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| number = ML17206A060 | | number = ML17206A060 | ||
| issue date = 12/31/2016 | | issue date = 12/31/2016 | ||
| title = | | title = Revised Updated Final Safety Analysis Report, Rev. 23, Chapter 4, Reactor | ||
| author name = | | author name = | ||
| author affiliation = Pacific Gas & Electric Co | | author affiliation = Pacific Gas & Electric Co | ||
| Line 20: | Line 20: | ||
2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title | 2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title | ||
Page i Revision 23 December 2016 4.1 SUMMARY DESCRIPTION 4.1-1 4. | Page i Revision 23 December 2016 4.1 | ||
==SUMMARY== | |||
DESCRIPTION 4.1-1 4. | |||
==1.1 REFERENCES== | ==1.1 REFERENCES== | ||
4.1-3 4.2 MECHANICAL DESIGN 4.2-1 4.2.1 FUEL 4.2-2 4.2.1.1 Design Bases 4.2-3 4.2.1.2 Fuel Rods 4.2-3 4.2.1.3 Fuel Assembly Structure 4.2-14 4.2.1.4 Operational Experience 4.2-24 4.2.1.5 Safety Evaluation 4.2-24 4.2.1.6 Tests and Inspections 4.2-25 4.2.2 REACTOR VESS EL INTERNALS 4.2-26 4.2.2.1 Design Bases 4.2-26 4.2.2.2 Acceptance Criteria 4.2-27 4.2.2.3 Reactor Vessel Internals Description 4.2-28 4.2.2.4 Reactor Vessel Internals Design Evaluation 4.2-32 4.2.2.5 Safety Evaluation 4.2-34 4.2.3 REACTIVITY CONTROL SYSTEM 4.2-36 4.2.3.1 Design Bases 4.2-36 4.2.3.2 Reactivity Control System Acceptance Criteria 4.2-37 4.2.3.3 Reactivity Control System Description 4.2-39 4.2.3.4 Reactivity Control System Design Evaluation 4.2-47 4.2.3.5 Safety Evaluation 4.2-54 4.2.3.6 Tests and Inspections 4.2-56 4.2.3.7 Instrumentation Applications 4.2-57 4. | 4.1-3 | ||
===4.2 MECHANICAL=== | |||
DESIGN 4.2-1 4.2.1 FUEL 4.2-2 4.2.1.1 Design Bases 4.2-3 4.2.1.2 Fuel Rods 4.2-3 4.2.1.3 Fuel Assembly Structure 4.2-14 4.2.1.4 Operational Experience 4.2-24 4.2.1.5 Safety Evaluation 4.2-24 4.2.1.6 Tests and Inspections 4.2-25 | |||
====4.2.2 REACTOR==== | |||
VESS EL INTERNALS 4.2-26 4.2.2.1 Design Bases 4.2-26 4.2.2.2 Acceptance Criteria 4.2-27 4.2.2.3 Reactor Vessel Internals Description 4.2-28 4.2.2.4 Reactor Vessel Internals Design Evaluation 4.2-32 4.2.2.5 Safety Evaluation 4.2-34 | |||
====4.2.3 REACTIVITY==== | |||
CONTROL SYSTEM 4.2-36 4.2.3.1 Design Bases 4.2-36 4.2.3.2 Reactivity Control System Acceptance Criteria 4.2-37 4.2.3.3 Reactivity Control System Description 4.2-39 4.2.3.4 Reactivity Control System Design Evaluation 4.2-47 4.2.3.5 Safety Evaluation 4.2-54 4.2.3.6 Tests and Inspections 4.2-56 4.2.3.7 Instrumentation Applications 4.2-57 4. | |||
==2.4 REFERENCES== | ==2.4 REFERENCES== | ||
4.2-58 4.3 NUCLEAR DESIGN 4.3-1 4.3.1 DESIGN BASES 4.3-2 4.3.1.1 General Design Criterion 10, 1971 - Reactor Design 4.3-2 4.3.1.2 General Design Criterion 11, 1971 - Reactor Inherent | 4.2-58 | ||
===4.3 NUCLEAR=== | |||
DESIGN 4.3-1 | |||
====4.3.1 DESIGN==== | |||
BASES 4.3-2 4.3.1.1 General Design Criterion 10, 1971 - Reactor Design 4.3-2 4.3.1.2 General Design Criterion 11, 1971 - Reactor Inherent | |||
Protection 4.3-2 4.3.1.3 General Design Criterion 12, 1971 - Suppression of DCPP UNITS 1 & | Protection 4.3-2 4.3.1.3 General Design Criterion 12, 1971 - Suppression of DCPP UNITS 1 & | ||
| Line 39: | Line 60: | ||
System Redundancy and Capability 4.3-2 4.3.1.6 General Design Criterion 28, 1971 - Reactivity Limits 4.3-2 | System Redundancy and Capability 4.3-2 4.3.1.6 General Design Criterion 28, 1971 - Reactivity Limits 4.3-2 | ||
4.3.2 NUCLEAR DESIGN ACCEPTANCE CRITERIA 4.3-3 4.3.2.1 Fuel Burnup 4.3-3 4.3.2.2 Control of Power Distribution 4.3-3 4.3.2.3 Negative Reactivity Feedbacks (Reactivity Coefficients) 4.3-3 4.3.2.4 Stability 4.3-4 4.3.2.5 Maximum Controlled Reactivity Insertion Rate 4.3-4 4.3.2.6 Shutdown Margins 4.3-4 4.3.3 DESCRIPTION 4.3-4 4.3.3.1 Nuclear Design Description 4.3-4 4.3.3.2 Power Distribution 4.3-6 4.3.3.3 Reactivity Coefficients 4.3-16 4.3.3.4 Control Requirements 4.3-19 4.3.3.5 Control 4.3-22 4.3.3.6 Control Rod Patterns and Reactivity Worths 4.3-24 4.3.3.7 Criticality of Fuel Assemblies 4.3-25 4.3.3.8 Stability 4.3-26 4.3.3.9 Vessel Irradiation 4.3-29 4.3.3.10 Analytical Methods 4.3-30 4.3.4 SAFETY EVALUATION 4.3-34 4.3.4.1 General Design Criterion 10, 1971 - Reactor Design 4.3-34 4.3.4.2 General Design Criterion 11, 1971 - Reactor Inherent | ====4.3.2 NUCLEAR==== | ||
DESIGN ACCEPTANCE CRITERIA 4.3-3 4.3.2.1 Fuel Burnup 4.3-3 4.3.2.2 Control of Power Distribution 4.3-3 4.3.2.3 Negative Reactivity Feedbacks (Reactivity Coefficients) 4.3-3 4.3.2.4 Stability 4.3-4 4.3.2.5 Maximum Controlled Reactivity Insertion Rate 4.3-4 4.3.2.6 Shutdown Margins 4.3-4 4. | |||
==3.3 DESCRIPTION== | |||
4.3-4 4.3.3.1 Nuclear Design Description 4.3-4 4.3.3.2 Power Distribution 4.3-6 4.3.3.3 Reactivity Coefficients 4.3-16 4.3.3.4 Control Requirements 4.3-19 4.3.3.5 Control 4.3-22 4.3.3.6 Control Rod Patterns and Reactivity Worths 4.3-24 4.3.3.7 Criticality of Fuel Assemblies 4.3-25 4.3.3.8 Stability 4.3-26 4.3.3.9 Vessel Irradiation 4.3-29 4.3.3.10 Analytical Methods 4.3-30 4.3.4 SAFETY EVALUATION 4.3-34 4.3.4.1 General Design Criterion 10, 1971 - Reactor Design 4.3-34 4.3.4.2 General Design Criterion 11, 1971 - Reactor Inherent | |||
Protection 4.3-35 4.3.4.3 General Design Criterion 12, 1971 - Suppression of Reactor | Protection 4.3-35 4.3.4.3 General Design Criterion 12, 1971 - Suppression of Reactor | ||
| Line 53: | Line 79: | ||
4.3-38 | 4.3-38 | ||
4.4 THERMAL AND HYDRAULIC DESIGN 4.4-1 | ===4.4 THERMAL=== | ||
AND HYDRAULIC DESIGN 4.4-1 | |||
4.4.1 DESIGN BASES 4.4-1 4.4.1.1 General Design Criterion 10, 1971 - Reactor Design 4.4-1 4.4.1.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations 4.4-1 | ====4.4.1 DESIGN==== | ||
BASES 4.4-1 4.4.1.1 General Design Criterion 10, 1971 - Reactor Design 4.4-1 4.4.1.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations 4.4-1 | |||
4.4.2 THERMAL AND HYDRAULIC DESIGN ACCEPTANCE CRITERIA 4.4-2 4.4.2.1 Departure from Nucleate Boiling Acceptance Criteria 4.4-2 4.4.2.2 Fuel Temperature Acceptance Criteria 4.4-2 4.4.2.3 Core Flow Acceptance Criteria 4.4-2 4.4.2.4 Hydrodynamic Stability Acceptance Criteria 4.4-2 | ====4.4.2 THERMAL==== | ||
AND HYDRAULIC DESIGN ACCEPTANCE CRITERIA 4.4-2 4.4.2.1 Departure from Nucleate Boiling Acceptance Criteria 4.4-2 4.4.2.2 Fuel Temperature Acceptance Criteria 4.4-2 4.4.2.3 Core Flow Acceptance Criteria 4.4-2 4.4.2.4 Hydrodynamic Stability Acceptance Criteria 4.4-2 | |||
4.4.3 SYSTEM DESCRIPTION 4.4-2 4.4.3.1 Summary Comparison 4.4-2 4.4.3.2 Fuel Cladding Temperatures 4.4-2 4.4.3.3 Departure from Nucleate Boiling Ratio 4.4-6 4.4.3.4 Flux Tilt Considerations 4.4-12 4.4.3.5 Void Fraction Distribution 4.4-13 4.4.3.6 Core Coolant Flow Distribution 4.4-13 4.4.3.7 Core Pressure Drops and Hydraulic Loads 4.4-13 4.4.3.8 Correlation and Physical Data 4.4-14 4.4.3.9 Thermal Effects of Operation Transients 4.4-16 4.4.3.10 Uncertainties in Estimates 4.4-16 4.4.3.11 Plant Configuration Data 4.4-18 4.4.3.12 Core Hydraulics 4.4-19 4.4.3.13 Influence of Power Distribution 4.4-21 4.4.3.14 Core Thermal Response 4.4-22 4.4.3.15 Analytical Techniques 4.4-22 4.4.3.16 Hydrodynamic and Flow-Power Coupled Instability 4.4-26 4.4.3.17 Temperature Transient Effects Analysis 4.4-27 4.4.3.18 Potentially Damaging Temperature Effects During Transients 4.4-28 4.4.3.19 Energy Release During Fuel Element Burnout 4.4-29 4.4.3.20 Energy Release During Rupture of Waterlogged Fuel Elements 4.4-29 DCPP UNITS 1 & | ====4.4.3 SYSTEM==== | ||
DESCRIPTION 4.4-2 4.4.3.1 Summary Comparison 4.4-2 4.4.3.2 Fuel Cladding Temperatures 4.4-2 4.4.3.3 Departure from Nucleate Boiling Ratio 4.4-6 4.4.3.4 Flux Tilt Considerations 4.4-12 4.4.3.5 Void Fraction Distribution 4.4-13 4.4.3.6 Core Coolant Flow Distribution 4.4-13 4.4.3.7 Core Pressure Drops and Hydraulic Loads 4.4-13 4.4.3.8 Correlation and Physical Data 4.4-14 4.4.3.9 Thermal Effects of Operation Transients 4.4-16 4.4.3.10 Uncertainties in Estimates 4.4-16 4.4.3.11 Plant Configuration Data 4.4-18 4.4.3.12 Core Hydraulics 4.4-19 4.4.3.13 Influence of Power Distribution 4.4-21 4.4.3.14 Core Thermal Response 4.4-22 4.4.3.15 Analytical Techniques 4.4-22 4.4.3.16 Hydrodynamic and Flow-Power Coupled Instability 4.4-26 4.4.3.17 Temperature Transient Effects Analysis 4.4-27 4.4.3.18 Potentially Damaging Temperature Effects During Transients 4.4-28 4.4.3.19 Energy Release During Fuel Element Burnout 4.4-29 4.4.3.20 Energy Release During Rupture of Waterlogged Fuel Elements 4.4-29 DCPP UNITS 1 & | |||
2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title | 2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title | ||
Page iv Revision 23 December 2016 4.4.3.21 Fuel Rod Behavior Effects from Coolant Flow Blockage 4.4-29 | Page iv Revision 23 December 2016 4.4.3.21 Fuel Rod Behavior Effects from Coolant Flow Blockage 4.4-29 | ||
4.4.4 THERMAL AND HYDRAULIC DESIGN EVALUATION 4.4-30 4.4.4.1 Departure from Nucleate Boiling 4.4-30 4.4.4.2 Fuel Temperature 4.4-31 4.4.4.3 Core Flow 4.4-32 4.4.4.4 Hydrodynamic Stability 4.4-32 | ====4.4.4 THERMAL==== | ||
AND HYDRAULIC DESIGN EVALUATION 4.4-30 4.4.4.1 Departure from Nucleate Boiling 4.4-30 4.4.4.2 Fuel Temperature 4.4-31 4.4.4.3 Core Flow 4.4-32 4.4.4.4 Hydrodynamic Stability 4.4-32 | |||
4.4.5 SAFETY EVALUATION 4.4-32 4.4.5.1 General Design Criterion 10, 1971 - Reactor Design 4.4-32 4.4.5.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations 4.4-32 | ====4.4.5 SAFETY==== | ||
EVALUATION 4.4-32 4.4.5.1 General Design Criterion 10, 1971 - Reactor Design 4.4-32 4.4.5.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations 4.4-32 | |||
4.4.6 TESTS AND INSPECTIONS 4.4-33 4.4.6.1 Testing Prior to Initial Criticality 4.4-33 4.4.6.2 Initial Power Plant Operation 4.4-33 4.4.6.3 Component and Fuel Inspections 4.4-33 | ====4.4.6 TESTS==== | ||
AND INSPECTIONS 4.4-33 4.4.6.1 Testing Prior to Initial Criticality 4.4-33 4.4.6.2 Initial Power Plant Operation 4.4-33 4.4.6.3 Component and Fuel Inspections 4.4-33 | |||
4.4.7 INSTRUMENTATION APPLICATIONS 4.4-33 4.4.7.1 Incore Instrumentation 4.4-33 4.4.7.2 Overtemperature and Overpower T Instrumentation 4.4-34 4.4.7.3 Instrumentation to Limit Maximum Power Output 4.4-34 | ====4.4.7 INSTRUMENTATION==== | ||
APPLICATIONS 4.4-33 4.4.7.1 Incore Instrumentation 4.4-33 4.4.7.2 Overtemperature and Overpower T Instrumentation 4.4-34 4.4.7.3 Instrumentation to Limit Maximum Power Output 4.4-34 | |||
4. | 4. | ||
| Line 113: | Line 147: | ||
4.4-4 Non-LOCA DNB Analysis Method DCPP UNITS 1 & | 4.4-4 Non-LOCA DNB Analysis Method DCPP UNITS 1 & | ||
2 FSAR UPDATE Chapter 4 FIGURES Figure Title vi Revision 23 December 2016 4.2-1 Fuel Assembly Cross Section | 2 FSAR UPDATE Chapter 4 FIGURES Figure Title vi Revision 23 December 2016 4.2-1 Fuel Assembly Cross Section | ||
4.2-2 Fuel Assembly Outline (LOPAR) | 4.2-2 Fuel Assembly Outline (LOPAR) | ||
| Line 150: | Line 184: | ||
4.2-18 Deleted in Revision 23 DCPP UNITS 1 & | 4.2-18 Deleted in Revision 23 DCPP UNITS 1 & | ||
2 FSAR UPDATE Chapter 4 FIGURES Figure Title vii Revision 23 December 2016 4.2-18A Wet Annular Burnable Absorber | 2 FSAR UPDATE Chapter 4 FIGURES Figure Title vii Revision 23 December 2016 4.2-18A Wet Annular Burnable Absorber | ||
4.2-19 Deleted in Revision 23 | 4.2-19 Deleted in Revision 23 | ||
| Line 182: | Line 216: | ||
4.3-4 Burnable Absorber Rod Arrangement Within an Assembly | 4.3-4 Burnable Absorber Rod Arrangement Within an Assembly | ||
4.3-5 Typical Integral Fuel Burnable Absorber Rod Arrangement Within an Assembly | 4.3-5 Typical Integral Fuel Burnable Absorber Rod Arrangement Within an Assembly 4.3-6 Burnable Absorber Loading Pattern | ||
4.3-6 Burnable Absorber Loading Pattern | |||
4.3-7 Normalized Power Density Distribution Near Beginning of Life (BOL), | 4.3-7 Normalized Power Density Distribution Near Beginning of Life (BOL), Unrodded Core, Hot Full Power, No Xenon | ||
Unrodded Core, Hot Full Power, No Xenon | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE Chapter 4 FIGURES Figure Title viii Revision 23 December 2016 4.3-8 Normalized Power Density Distribution Near BOL, Unrodded Core, Hot Full Power, Equilibrium Xenon | 2 FSAR UPDATE Chapter 4 FIGURES Figure Title viii Revision 23 December 2016 4.3-8 Normalized Power Density Distribution Near BOL, Unrodded Core, Hot Full Power, Equilibrium Xenon | ||
4.3-9 Unit 1 - Normalized Power Density Distribution Near BOL, Group D at Insertion Limit, Hot Full Power, Equilibrium Xenon | 4.3-9 Unit 1 - Normalized Power Density Distribution Near BOL, Group D at Insertion Limit, Hot Full Power, Equilibrium Xenon | ||
| Line 196: | Line 227: | ||
4.3-10 Unit 2 - Normalized Power Density Distribution Near BOL, Group D at Insertion Limit, Hot Full Power, Equilibrium Xenon | 4.3-10 Unit 2 - Normalized Power Density Distribution Near BOL, Group D at Insertion Limit, Hot Full Power, Equilibrium Xenon | ||
4.3-11 Normalized Power Density Distribution Near Middle of Life (MOL), | 4.3-11 Normalized Power Density Distribution Near Middle of Life (MOL), Unrodded Core, Hot Full Power, Equilibrium Xenon | ||
Unrodded Core, Hot Full Power, Equilibrium Xenon | |||
4.3-12 Normalized Power Density Distribution Near End of Life (EOL), | 4.3-12 Normalized Power Density Distribution Near End of Life (EOL), Unrodded Core, Hot Full Power, Equilibrium Xenon | ||
Unrodded Core, Hot Full Power, Equilibrium Xenon | |||
4.3-13 Rodwise Power Distribution in a Typical Assembly (G-10) Near BOL, Hot Full Power, Equilibrium Xenon, Unrodded Core 4.3-14 Rodwise Power Distribution in a Typical Assembly (G-10) Near EOL, Hot Full Power, Equilibrium Xenon, Unrodded Core 4.3-15 Possible Axial Power Shapes at BOL Due to Adverse Xenon Distributions | 4.3-13 Rodwise Power Distribution in a Typical Assembly (G-10) Near BOL, Hot Full Power, Equilibrium Xenon, Unrodded Core 4.3-14 Rodwise Power Distribution in a Typical Assembly (G-10) Near EOL, Hot Full Power, Equilibrium Xenon, Unrodded Core 4.3-15 Possible Axial Power Shapes at BOL Due to Adverse Xenon Distributions | ||
| Line 219: | Line 248: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE Chapter 4 FIGURES Figure Title ix Revision 23 December 2016 4.3-23 Maximum | 2 FSAR UPDATE Chapter 4 FIGURES Figure Title ix Revision 23 December 2016 4.3-23 Maximum Fx Q T Power vs. Axial Height During Normal Operations | ||
4.3-24 Deleted in Revision 23 | 4.3-24 Deleted in Revision 23 | ||
| Line 227: | Line 256: | ||
4.3-26 Comparison of Calculated and Measured Axial Shape | 4.3-26 Comparison of Calculated and Measured Axial Shape | ||
4.3-27 Measured Values of | 4.3-27 Measured Values of F Q T for Full Power Rod Configurations 4.3-28 Doppler Temperature Coefficient at BOL and EOL | ||
4.3-29 Doppler Only Power Coefficient at BOL and EOL | 4.3-29 Doppler Only Power Coefficient at BOL and EOL | ||
| Line 252: | Line 281: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE Chapter 4 FIGURES Figure Title x Revision 23 December 2016 4.3-41 Normalized Rod Worth vs. Percent Insertion, All Rods But One | 2 FSAR UPDATE Chapter 4 FIGURES Figure Title x Revision 23 December 2016 4.3-41 Normalized Rod Worth vs. Percent Insertion, All Rods But One | ||
4.3-42 Axial Offset vs. Time, PWR Core with a 12-ft Core Height and 121 Assemblies | 4.3-42 Axial Offset vs. Time, PWR Core with a 12-ft Core Height and 121 Assemblies | ||
| Line 269: | Line 298: | ||
4.4-2 Peak Fuel Centerline Temperature During Fuel Rod Lifetime vs. Linear Power Density | 4.4-2 Peak Fuel Centerline Temperature During Fuel Rod Lifetime vs. Linear Power Density | ||
4.4-3 Thermal Conductivity of UO 2 (Data Corrected to 95% Theoretical Density) | 4.4-3 Thermal Conductivity of UO 2 (Data Corrected to 95% Theoretical Density) 4.4-4 Axial Variation of Average Clad Temperature for Rod Operating at 5.43 kW/ft | ||
4.4-4 Axial Variation of Average Clad Temperature for Rod Operating at 5.43 kW/ft | |||
4.4-5 Probability Curves for W-3 and R Grid DNB Correlations | 4.4-5 Probability Curves for W-3 and R Grid DNB Correlations | ||
| Line 282: | Line 309: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE Chapter 4 FIGURES Figure Title xi Revision 23 December 2016 4.4-9 Normalized Radial Flow and Enthalpy Distribution at 12-ft Elevation Core Exit 4.4-10 Void Fraction vs. Thermodynamic Quality H-H SAT/ | 2 FSAR UPDATE Chapter 4 FIGURES Figure Title xi Revision 23 December 2016 4.4-9 Normalized Radial Flow and Enthalpy Distribution at 12-ft Elevation Core Exit 4.4-10 Void Fraction vs. Thermodynamic Quality H-H SAT/H G-HSAT 4.4-11 PWR Natural Circulation Test | ||
4.4-12 Comparison of a Representative W Two-loop Reactor Incore Thermocouple Measurements with THINC-IV Predictions | 4.4-12 Comparison of a Representative W Two-loop Reactor Incore Thermocouple Measurements with THINC-IV Predictions | ||
| Line 303: | Line 330: | ||
2 FSAR UPDATE 4.1-1 Revision 23 December 2016 Chapter 4 REACTOR This chapter describes the design for the reactors at Diablo Canyon Power Plant (DCPP) Unit 1 and Unit 2, and evaluates their capabilities to function safely under all operating modes expected during their lifetimes. | 2 FSAR UPDATE 4.1-1 Revision 23 December 2016 Chapter 4 REACTOR This chapter describes the design for the reactors at Diablo Canyon Power Plant (DCPP) Unit 1 and Unit 2, and evaluates their capabilities to function safely under all operating modes expected during their lifetimes. | ||
4.1 SUMMARY DESCRIPTION This chapter describes the following subjects: (a) the mechanical components of the reactor and reactor core, including the fuel rods and fuel assemblies, reactor vessel internals, and the control rod drive mechanisms (CRDMs), (b) the nuclear design, and (c) the thermal-hydraulic design. | 4.1 | ||
==SUMMARY== | |||
DESCRIPTION This chapter describes the following subjects: (a) the mechanical components of the reactor and reactor core, including the fuel rods and fuel assemblies, reactor vessel internals, and the control rod drive mechanisms (CRDMs), (b) the nuclear design, and (c) the thermal-hydraulic design. | |||
The reactor core of each unit consists of VANTAGE+ fuel assemblies. | The reactor core of each unit consists of VANTAGE+ fuel assemblies. | ||
| Line 385: | Line 415: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-1 Revision 23 December 2016 4.2 MECHANICAL DESIGN For design purposes, the DCPP conditions are divided into four categories, in accordance with their anticipated frequency of occurrence and risk to the public, as | 2 FSAR UPDATE 4.2-1 Revision 23 December 2016 | ||
===4.2 MECHANICAL=== | |||
DESIGN For design purposes, the DCPP conditions are divided into four categories, in accordance with their anticipated frequency of occurrence and risk to the public, as | |||
follows: | follows: | ||
(1) Condition I - Normal Operation (2) Condition II - Incidents of Moderate Frequency (3) Condition III - Infrequent Faults (4) Condition IV - Limiting Faults | (1) Condition I - Normal Operation (2) Condition II - Incidents of Moderate Frequency (3) Condition III - Infrequent Faults (4) Condition IV - Limiting Faults | ||
| Line 415: | Line 447: | ||
safety criteria: | safety criteria: | ||
(1) The mechanical design of the reactor core components and their physical arrangement, together with corrective actions by the reactor control, | (1) The mechanical design of the reactor core components and their physical arrangement, together with corrective actions by the reactor control, protection, and emergency cooling systems (when applicable) ensure that: | ||
protection, and emergency cooling systems ( | |||
when applicable) ensure that: | |||
(a) Fuel damage is not expected duri ng Conditions I and II events, although a very small number of fuel rod failures is anticipated. This | (a) Fuel damage is not expected duri ng Conditions I and II events, although a very small number of fuel rod failures is anticipated. This | ||
| Line 472: | Line 501: | ||
also limited so that extensive departure from nucleate boiling (DNB) | also limited so that extensive departure from nucleate boiling (DNB) | ||
propagation does not occur during normal operation and accident events | propagation does not occur during normal operation and accident events (Reference 14). Also, cladding fla ttening (Reference 15) will not occur during the fuel rod incore life. | ||
(Reference 14). Also, cladding fla ttening (Reference 15) will not occur during the fuel rod incore life. | |||
(3) Cladding Stress and Strain - The design limit for the fuel rod clad strain is the total plastic tensile creep strain due to: | (3) Cladding Stress and Strain - The design limit for the fuel rod clad strain is the total plastic tensile creep strain due to: | ||
* uniform clad creep, | * uniform clad creep, | ||
| Line 482: | Line 509: | ||
* pellet thermal expansion, | * pellet thermal expansion, | ||
* pellet swelling and uniform clad creep, and | * pellet swelling and uniform clad creep, and | ||
* pressure differences is less than the ZIRLO 0.2% offset yield stress, with due consideration to temperature and irradiation effects under Condition I and Condition ll events. | * pressure differences is less than the ZIRLO 0.2% offset yield stress, with due consideration to temperature and irradiation effects under Condition I and Condition ll events. While the clad has some capability for accommodating plastic strain, the yield stress has been established as a conservative design limit. | ||
While the clad has some capability for accommodating plastic strain, the yield stress has been established as a conservative design limit. | |||
(4) Cladding Tensile Strain - The total tensile strain due to uniform cylindrical pellet thermal expansion during a transient is less than 1% from the pre-transient value. | (4) Cladding Tensile Strain - The total tensile strain due to uniform cylindrical pellet thermal expansion during a transient is less than 1% from the pre-transient value. | ||
(5) Strain Fatigue - The fuel system will not be damaged due to excessive clad fatigue. The fatigue life usage factor is limited to less than 1.0 to prevent reaching the material fatigue limit. | (5) Strain Fatigue - The fuel system will not be damaged due to excessive clad fatigue. The fatigue life usage factor is limited to less than 1.0 to prevent reaching the material fatigue limit. | ||
| Line 556: | Line 582: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-11 Revision 23 December 2016 The evaluation of the fatigue life usage factor for extended burnup operation conservatively assumes daily load follow operation over the life of the fuel rod, plus ten (10) cold shutdowns per cycle. The Westinghouse fuel performance code, PAD 4.0, (Reference 34) is used to determine the strain range for the fatigue life usage analysis. | 2 FSAR UPDATE 4.2-11 Revision 23 December 2016 The evaluation of the fatigue life usage factor for extended burnup operation conservatively assumes daily load follow operation over the life of the fuel rod, plus ten (10) cold shutdowns per cycle. The Westinghouse fuel performance code, PAD 4.0, (Reference 34) is used to determine the strain range for the fatigue life usage analysis. | ||
PAD 4.0, is used to determine the strain range for the fatigue usage analysis of the VANTAGE+ fuel design. The Langer-O'Donnell fatigue model is used with the calculated strains from PAD 4.0 to assure that the above criterion is met for VANTAGE+. | PAD 4.0, is used to determine the strain range for the fatigue usage analysis of the VANTAGE+ fuel design. The Langer-O'Donnell fatigue model is used with the calculated strains from PAD 4.0 to assure that the above criterion is met for VANTAGE+. The Westinghouse analytical approach to strain fatigue results from evaluating several strain-fatigue models and the results of the Westingho use experimental programs. In conclusion, the approach defined by Langer-O'Donnell (Reference 12) was retained, and the empirical factors of their correlation were modified to conservatively bound the results of the Westinghouse testing program. | ||
The Westinghouse analytical approach to strain fatigue results from evaluating several strain-fatigue models and the results of the Westingho use experimental programs. In conclusion, the approach defined by Langer-O'Donnell (Reference 12) was retained, and the empirical factors of their correlation were modified to conservatively bound the results of the Westinghouse testing program. | |||
The Langer-O'Donnell empirical correlation has the following form: | The Langer-O'Donnell empirical correlation has the following form: | ||
e SRA100 100 ln 4 f N E a S+= (4.2-1) where: S a = 1/2 E = pseudo-stress amplitude that causes failure in N f cycles, lb/in 2 = total strain range, in./in E = Young's Modulus, lb/in 2 N f = number of cycles to failure RA = reduction in area at fracture in a uniaxial tensile test, % | |||
S e = endurance limit, lb/in 2 Both RA and S e are empirical constants that depend on the type of material, the temperature, and the irradiation. | |||
The results of the Westinghouse test programs provided information on different cladding conditions, including the effect of irradiation, hydrogen level, and temperature. | The results of the Westinghouse test programs provided information on different cladding conditions, including the effect of irradiation, hydrogen level, and temperature. | ||
The Westinghouse design equations followed the concept for the fatigue design criterion according to the ASME BPVC Section III, namely: | The Westinghouse design equations followed the concept for the fatigue design criterion according to the ASME BPVC Section III, namely: | ||
| Line 568: | Line 593: | ||
2 FSAR UPDATE 4.2-12 Revision 23 December 2016 (2) The allowable cycles for a given Sa are 5 percent of Nf or a safety factor of 20 on cycles. | 2 FSAR UPDATE 4.2-12 Revision 23 December 2016 (2) The allowable cycles for a given Sa are 5 percent of Nf or a safety factor of 20 on cycles. | ||
The lesser of the two allowable n umbers of cycles is selected. The cumulative fatigue life fraction is then computed as: | The lesser of the two allowable n umbers of cycles is selected. The cumulative fatigue life fraction is then computed as: | ||
k fk k N n 1 1 (4.2-2) where: n k = number of diurnal cycles of mode k 4.2.1.2.3 Fuel Rod Design Evaluation | |||
The fuel rod design ensures that the design bases are satisfied. | The fuel rod design ensures that the design bases are satisfied. | ||
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(3) Cladding Stress and Strain - Radial, tangential, and axial stress components due to pressure differential and fuel cladding contact pressure are combined into an effective stress using the maximum-distortion-energy theory. The von Mises criterion (Reference | (3) Cladding Stress and Strain - Radial, tangential, and axial stress components due to pressure differential and fuel cladding contact pressure are combined into an effective stress using the maximum-distortion-energy theory. The von Mises criterion (Reference | ||
: 22) is used to evaluate whether or not the yield strength has been exceeded. The criterion states that an isotropic material under multiaxial DCPP UNITS 1 & | : 22) is used to evaluate whether or not the yield strength has been exceeded. The criterion states that an isotropic material under multiaxial DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-13 Revision 23 December 2016 stress will begin to yield plastically when the effective stress (i.e., | 2 FSAR UPDATE 4.2-13 Revision 23 December 2016 stress will begin to yield plastically when the effective stress (i.e., combined stress using maximum-distortion-energy theory) becomes equal to the material yield stress in simple tension, as determined by a uniaxial tensile test. Since general yielding is prohibited, the volume average effective stress determined by integrating across the cladding thickness is increased by an allowance for local nonuniformity effects before the stress is compared to the yield strength. The yield strength correlation is appropriate for irradiated cladding since the irradiated properties are attained at low exposure, whereas the fuel/cladding interaction conditions, which can lead to minimum margin to the design basis limit, always occur at much higher exposures. The clad stresses in the VANTAGE+ fuel rod clad caused by power transients are evaluated (refer to Section 4.2.1.2.2.5). These evaluations show that the clad stresses and clad strains for VANTAGE+ fuel rod designs (IFBA and non-IFBA) meet the design limits. | ||
combined stress using maximum-distortion-energy theory) becomes equal to the material yield stress in simple tension, as determined by a uniaxial tensile test. Since general yielding is prohibited, the volume average effective stress determined by integrating across the cladding thickness is increased by an allowance for local nonuniformity effects before the stress is compared to the yield strength. The yield strength correlation is appropriate for irradiated cladding since the irradiated properties are attained at low exposure, whereas the fuel/cladding interaction conditions, which can lead to minimum margin to the design basis limit, always occur at much higher exposures. The clad stresses in the VANTAGE+ fuel rod clad caused by power transients are evaluated (refer to Section 4.2.1.2.2.5). These evaluations show that the clad stresses and clad strains for VANTAGE+ fuel rod designs (IFBA and non-IFBA) meet the design limits. | |||
(4) Cladding Tensile Strain - | (4) Cladding Tensile Strain - | ||
Section 4.2.1.2.2.5 shows that the cladding tensile strain stresses for the VANTAGE+ fuel rod designs meet the design limits. | Section 4.2.1.2.2.5 shows that the cladding tensile strain stresses for the VANTAGE+ fuel rod designs meet the design limits. | ||
(5) Strain Fatigue - Clad fatigue for the VANTAGE+ fuel rod design is evaluated by the same methods as are used for other Westinghouse fuel designs. Computer modeling of the fuel rod simulates a daily load follow cycling scheme 100-15-100% power and 12-3-6-3 hour intervals for residence times of more than 60 months. | (5) Strain Fatigue - Clad fatigue for the VANTAGE+ fuel rod design is evaluated by the same methods as are used for other Westinghouse fuel designs. Computer modeling of the fuel rod simulates a daily load follow cycling scheme 100-15-100% power and 12-3-6-3 hour intervals for residence times of more than 60 months. | ||
Design evaluations have shown that the cumulative fatigue usage factor for the VANTAGE+ fuel rod will meet the design criterion. Details regarding this evaluation are presented in Reference 29, Section B.2.3. | Design evaluations have shown that the cumulative fatigue usage factor for the VANTAGE+ fuel rod will meet the design criterion. Details regarding this evaluation are presented in Reference 29, Section B.2.3. | ||
(6) Fuel Clad Oxidation and Hydriding - The clad surface temperature and hydriding of the VANTAGE+ fuel rod is evaluated by the same methods as are used for other Westinghouse fuel designs. The coolant temperature rise over the length of the fuel rod and temperature rise through the film, crud and oxide layer are calculated and the temperature at the metal-oxide interface is determined. Calculations show that the clad surface temperature and hydriding of the VANTAGE+ fuel rod meet the design limits. | (6) Fuel Clad Oxidation and Hydriding - The clad surface temperature and hydriding of the VANTAGE+ fuel rod is evaluated by the same methods as are used for other Westinghouse fuel designs. The coolant temperature rise over the length of the fuel rod and temperature rise through the film, crud and oxide layer are calculated and the temperature at the metal-oxide interface is determined. Calculations show that the clad surface temperature and hydriding of the VANTAGE+ fuel rod meet the design limits. (7) Fuel Clad Wear - The design criteria with regard to clad fretting wear are met for VANTAGE+ to its design burnup. Details regarding this evaluation are presented in Reference 29, Section B.2.5.1. | ||
(8) Fuel Clad Flattening - Calculations for VANTAGE+ fuel show that predicted clad flattening time exceeds residence times expected for extended burnup fuel management. | (8) Fuel Clad Flattening - Calculations for VANTAGE+ fuel show that predicted clad flattening time exceeds residence times expected for extended burnup fuel management. | ||
The evaluation is discussed in detail in Reference 29, Section B.2.4. | The evaluation is discussed in detail in Reference 29, Section B.2.4. | ||
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2 FSAR UPDATE 4.2-14 Revision 23 December 2016 (9) Fuel Rod Axial Growth - The fuel assembly design is sized to provide sufficient fuel-rod-to-nozzle gaps, as discussed in Reference 29, Section 2.3.1.1. Sufficient top and bottom nozzle-to-fuel rod gaps are provided to assure that fuel rod growth is accommodated during the fuel design lifetime. | 2 FSAR UPDATE 4.2-14 Revision 23 December 2016 (9) Fuel Rod Axial Growth - The fuel assembly design is sized to provide sufficient fuel-rod-to-nozzle gaps, as discussed in Reference 29, Section 2.3.1.1. Sufficient top and bottom nozzle-to-fuel rod gaps are provided to assure that fuel rod growth is accommodated during the fuel design lifetime. | ||
4.2.1.3 Fuel Assembly Structure 4.2.1.3.1 Fuel Assembly Structure Acceptance Criteria 4.2.1.3.1.1 Fuel Assembly Structural Integrity The VANTAGE+ fuel assembly must maintain its structural integrity in response to seismic and LOCA loads (refer to Sections 3.7.3.15.2 and 4.2.1.5.4). The stresses and deformations due to various loads on the fuel assemblies are discussed in Section 4.2.1.3.2.5, including the effects of Seismic/LOCA loads.. | 4.2.1.3 Fuel Assembly Structure 4.2.1.3.1 Fuel Assembly Structure Acceptance Criteria 4.2.1.3.1.1 Fuel Assembly Structural Integrity The VANTAGE+ fuel assembly must maintain its structural integrity in response to seismic and LOCA loads (refer to Sections 3.7.3.15.2 and 4.2.1.5.4). The stresses and deformations due to various loads on the fuel assemblies are discussed in Section 4.2.1.3.2.5, including the effects of Seismic/LOCA loads.. | ||
4.2.1.3.1.2 Fuel Assembly Shipping and Handling Loads The design acceleration limit for the fuel assembly handling and shipping loads is 4g's minimum. | 4.2.1.3.1.2 Fuel Assembly Shipping and Handling Loads The design acceleration limit for the fuel assembly handling and shipping loads is 4g's minimum. 4.2.1.3.1.3 Top Nozzle The top nozzle is required to transmit 4g shipping and handling loads without permanent deformation. The joints must transmit the same loads and be capable of disconnecting using a special disassembly tool. | ||
4.2.1.3.1.3 Top Nozzle The top nozzle is required to transmit 4g shipping and handling loads without permanent deformation. The joints must transmit the same loads and be capable of disconnecting using a special disassembly tool. | 4.2.1.3.1.4 Fuel Assembly Holddown Springs The fuel assembly holddown springs, Figure 4.2-2, are designed to keep the fuel assemblies resting on the lower core plate under transients associated with Condition I and Condition II events with the exception of the turbine overspeed transient associated with a loss of external load. The holddown springs are designed to tolerate the possibility of a deflection associated with fuel assembly liftoff for this case and provide contact between the fuel assembly and the lower core plate following this transient. . 4.2.1.3.2 Fuel Assembly Structure Description The fuel assembly structure consists of a bottom nozzle, top nozzle, guide thimbles, and | ||
4.2.1.3.1.4 Fuel Assembly Holddown Springs The fuel assembly holddown springs, Figure 4.2-2, are designed to keep the fuel assemblies resting on the lower core plate under transients associated with Condition I and Condition II events with the exception of the turbine overspeed transient associated with a loss of external load. The holddown springs are designed to tolerate the possibility of a deflection associated with fuel assembly liftoff for this case and provide contact between the fuel assembly and the lower core plate following this transient. | |||
. 4.2.1.3.2 Fuel Assembly Structure Description The fuel assembly structure consists of a bottom nozzle, top nozzle, guide thimbles, and | |||
grids, as shown in Figure 4.2-2. | grids, as shown in Figure 4.2-2. | ||
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(b) One-third of the tensile strength or 90 percent of the yield strength, at temperature, but not to exceed two-thirds of the specified minimum yield strength at room temperature. | (b) One-third of the tensile strength or 90 percent of the yield strength, at temperature, but not to exceed two-thirds of the specified minimum yield strength at room temperature. | ||
The stress intensity limits for the austenitic steel components are: | The stress intensity limits for the austenitic steel components are: | ||
Stress Intensity Limits Categories Limit General Primary Membrane Stress Intensity 1.0 | Stress Intensity Limits Categories Limit General Primary Membrane Stress Intensity 1.0 S m Local Primary Membrane Stress Intensity 1.5 S m Primary Membrane plus Bending Stress Intensity 1.5 S m Total Primary plus Secondary Stress Intensity Range 3.0 S m where S m is the membrane stress. | ||
(3) Abnormal Loads during Conditions II I or IV - Worst cases are represented by combined seismic and blowdown loads. However, with NRC approval of the DCPP leak-before-break (LBB) analysis (Reference 30) and Amendments 221 and 223, to perform the fuel assembly structural analyses based on postulated pipe break locations that consider the application of LBB (Reference 32), the blowdown loads resulting from pipe rupture events in the main reactor coolant loop piping no longer have to be considered in the structural design basis analysis. Only the much smaller blowdown loads from RCS branch line breaks have to be considered (see Section 3.6.2.1.1.1). | (3) Abnormal Loads during Conditions II I or IV - Worst cases are represented by combined seismic and blowdown loads. However, with NRC approval of the DCPP leak-before-break (LBB) analysis (Reference 30) and Amendments 221 and 223, to perform the fuel assembly structural analyses based on postulated pipe break locations that consider the application of LBB (Reference 32), the blowdown loads resulting from pipe rupture events in the main reactor coolant loop piping no longer have to be considered in the structural design basis analysis. Only the much smaller blowdown loads from RCS branch line breaks have to be considered (see Section 3.6.2.1.1.1). | ||
(a) Deflections of components cannot interfere with reactor shutdown or emergency cooling of fuel rods. | (a) Deflections of components cannot interfere with reactor shutdown or emergency cooling of fuel rods. | ||
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stress range associated with deflections of such small magnitude is insignificant and has no effect on the structural integrity of the fuel rod. | stress range associated with deflections of such small magnitude is insignificant and has no effect on the structural integrity of the fuel rod. | ||
The conclusion that the effect of flow-in duced vibrations on the fuel assembly and fuel rod is minimal is based on test results and analysis documented in WCAP-8279 | The conclusion that the effect of flow-in duced vibrations on the fuel assembly and fuel rod is minimal is based on test results and analysis documented in WCAP-8279 (Reference 13), which considered conditions normally encountered in reactor operation. | ||
(Reference 13), which considered conditions normally encountered in reactor operation. | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
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As part of a continuing Westinghouse fuel performance evaluation program, one surveillance fuel assembly containing 88 rem ovable fuel rods was included in Region 3 of the initial DCPP Unit 1 and Unit 2 core loading. The objective of this program was to facilitate interim and EOL fuel evaluation as a function of exposure. The rods could be removed, nondestructively examined, and reinserted at the end of intermediate fuel cycles. The rods could be removed easily and subjected to a destructive examination at EOL. | As part of a continuing Westinghouse fuel performance evaluation program, one surveillance fuel assembly containing 88 rem ovable fuel rods was included in Region 3 of the initial DCPP Unit 1 and Unit 2 core loading. The objective of this program was to facilitate interim and EOL fuel evaluation as a function of exposure. The rods could be removed, nondestructively examined, and reinserted at the end of intermediate fuel cycles. The rods could be removed easily and subjected to a destructive examination at EOL. | ||
The overall dimensions, rod pitch | The overall dimensions, rod pitch , number of rods, and material are the same as for other Region 3 assemblies. These fuel rods were fabricated in parallel with the regular Region 3 rods using selected Region 3 cladding and pellets fabricated to the same DCPP UNITS 1 & | ||
, number of rods, and material are the same as for other Region 3 assemblies. These fuel rods were fabricated in parallel with the regular Region 3 rods using selected Region 3 cladding and pellets fabricated to the same DCPP UNITS 1 & | |||
2 FSAR UPDATE 4.2-26 Revision 23 December 2016 manufacturing tolerance limits. Mechanically, the special assemblies differ from other Region 3 assemblies only in those features that facilitate removal and reinsertion. | 2 FSAR UPDATE 4.2-26 Revision 23 December 2016 manufacturing tolerance limits. Mechanically, the special assemblies differ from other Region 3 assemblies only in those features that facilitate removal and reinsertion. | ||
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Figure 4.2-7 shows the removable rod fuel asse mbly, the modified upper nozzle adapter plate, and thimble plug assembly; it may be compared to the standard assembly shown in Figure 4.2-2. The location of the removable rods within the fuel assembly is shown in | Figure 4.2-7 shows the removable rod fuel asse mbly, the modified upper nozzle adapter plate, and thimble plug assembly; it may be compared to the standard assembly shown in Figure 4.2-2. The location of the removable rods within the fuel assembly is shown in | ||
Figure 4.2-8. Fuel handling with removable fuel rods has been done routinely and without difficulty in many operating plants. | Figure 4.2-8. Fuel handling with removable fuel rods has been done routinely and without difficulty in many operating plants. | ||
4.2.2 REACTOR VESS EL INTERNALS 4.2.2.1 Design Bases 4.2.2.1.1 General Design Criterion 2, 1967 - Performance Standards The reactor internals are designed to withstand the effects of, or are protected against, natural phenomena such as earthquakes. | |||
====4.2.2 REACTOR==== | |||
VESS EL INTERNALS 4.2.2.1 Design Bases 4.2.2.1.1 General Design Criterion 2, 1967 - Performance Standards The reactor internals are designed to withstand the effects of, or are protected against, natural phenomena such as earthquakes. | |||
4.2.2.1.2 General Design Criterion 4, 1987 | 4.2.2.1.2 General Design Criterion 4, 1987 | ||
- Environmental and Dynamic Effects Design Bases Consideration of the dynamic effects associated with main reactor coolant loop (RCL) piping postulated pipe ruptures are excluded from the DCPP design basis with the approval of leak-before-break (LBB) methodology by demonstrating that the probability of fluid system piping rupture is extremely low under conditions consistent with the design basis for the piping. | - Environmental and Dynamic Effects Design Bases Consideration of the dynamic effects associated with main reactor coolant loop (RCL) piping postulated pipe ruptures are excluded from the DCPP design basis with the approval of leak-before-break (LBB) methodology by demonstrating that the probability of fluid system piping rupture is extremely low under conditions consistent with the design basis for the piping. | ||
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HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | ||
With respect to previous plants, there is no change in the design configuration of reactor vessel internals and the reactor vessel internals core support structures. Moreover, since their mechanical properties (e.g., | With respect to previous plants, there is no change in the design configuration of reactor vessel internals and the reactor vessel internals core support structures. Moreover, since their mechanical properties (e.g., fuel assembly weight, beam stiffness) are virtually the same, the response of the reactor vessel internals core support structure will not change. | ||
fuel assembly weight, beam stiffness) are virtually the same, the response of the reactor vessel internals core support structure will not change. | The qualification of identical plants by the first-of-a-kind analysis is further verified by the Internals Vibration Assurance Program discussed in Section 3.9.2.1. | ||
The qualification of identical plants by the first-of-a | |||
-kind analysis is further verified by the Internals Vibration Assurance Program discussed in Section 3.9.2.1. | |||
4.2.2.3.1 Lower Core Support Structure The reactor vessel internals support member is the lower core support structure shown in Figures 4.2-9 and 4.2-10 for DCPP Unit 1 and Unit 2, respectively. This support structure assembly consists of the core barrel, the core baffle, the lower core plate and support columns, the thermal shield on Unit 1, and the neutron shield pad assembly on Unit 2 (the transition from a thermal shield to neutron shield pad assembly is explained in WCAP-7870 {Reference 7}), and the core support, which is welded to the core barrel. | 4.2.2.3.1 Lower Core Support Structure The reactor vessel internals support member is the lower core support structure shown in Figures 4.2-9 and 4.2-10 for DCPP Unit 1 and Unit 2, respectively. This support structure assembly consists of the core barrel, the core baffle, the lower core plate and support columns, the thermal shield on Unit 1, and the neutron shield pad assembly on Unit 2 (the transition from a thermal shield to neutron shield pad assembly is explained in WCAP-7870 {Reference 7}), and the core support, which is welded to the core barrel. | ||
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On Unit 1, the one-piece thermal shield is fix ed to the core barrel at the top with rigid bolted connections. The bottom of the thermal shield is connected to the core barrel by means of axial flexures. Rectangular specimen guides in which material samples can | On Unit 1, the one-piece thermal shield is fix ed to the core barrel at the top with rigid bolted connections. The bottom of the thermal shield is connected to the core barrel by means of axial flexures. Rectangular specimen guides in which material samples can | ||
be inserted, held by a preloaded spring device, and irradiated during reactor operation, | be inserted, held by a preloaded spring device, and irradiated during reactor operation, are welded to the thermal shield. | ||
are welded to the thermal shield. | |||
On Unit 2, the neutron shield pad assembly, shown in Figure 4.2-11, consists of four | On Unit 2, the neutron shield pad assembly, shown in Figure 4.2-11, consists of four | ||
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pins that are welded into the core barrel. | pins that are welded into the core barrel. | ||
The radial support system of the core barrel is accomplished by "key" and "keyway" | The radial support system of the core barrel is accomplished by "key" and "keyway" joints to the reactor vessel wall. At six equally spaced points around the circumference, an Inconel clevis block is welded to the vessel inner diameter. An Inconel insert block is bolted to each of these clevis blocks, and has a keyway geometry. Opposite each of | ||
joints to the reactor vessel wall. At six equally spaced points around the circumference, an Inconel clevis block is welded to the vessel inner diameter. An Inconel insert block is bolted to each of these clevis blocks, and has a keyway geometry. Opposite each of | |||
these is a key that is welded to the lower core support. During assembly, as the | these is a key that is welded to the lower core support. During assembly, as the | ||
| Line 1,016: | Line 1,030: | ||
4.2.2.3.3 Incore Instrumentation Support Structures The incore instrumentation support structures consist of an upper system to convey and support thermocouples penetrating the vessel through the head, and a lower system to | 4.2.2.3.3 Incore Instrumentation Support Structures The incore instrumentation support structures consist of an upper system to convey and support thermocouples penetrating the vessel through the head, and a lower system to | ||
convey and support flux thimbles penetrating the vessel through the bottom | convey and support flux thimbles penetrating the vessel through the bottom (Figure 7.7-9 shows the basic flux-mapping system). | ||
(Figure 7.7-9 shows the basic flux-mapping system). | |||
The upper system utilizes the reactor vessel head penetrations. Instrumentation port | The upper system utilizes the reactor vessel head penetrations. Instrumentation port | ||
| Line 1,098: | Line 1,110: | ||
The scope and methodology of the stress analysis problem is discussed in Section | The scope and methodology of the stress analysis problem is discussed in Section | ||
3.9.2.3. | 3.9.2.3. | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-34 Revision 23 December 2016 4.2.2.4.3 Allowable Deflections For normal operating conditions, downward vertical deflection of the lower core support plate is negligible. | 2 FSAR UPDATE 4.2-34 Revision 23 December 2016 4.2.2.4.3 Allowable Deflections For normal operating conditions, downward vertical deflection of the lower core support plate is negligible. | ||
Limiting deflection values from the LOCA plus the earthquake (larger of the DDE or HE), | Limiting deflection values from the LOCA plus the earthquake (larger of the DDE or HE), and for the deflection criteria of critical internal structures, are given in Section 3.9.2.3 and Table 3.9-10. | ||
and for the deflection criteria of critical internal structures, are given in Section 3.9.2.3 and Table 3.9-10. | |||
The criteria for the core drop accident are based on determining the total downward | The criteria for the core drop accident are based on determining the total downward | ||
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DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-36 Revision 23 December 2016 The reactor vessel internals have provisions to install material test specimens for the reactor vessel material surveillance program (refer to Section 5.2.2.4.4). | 2 FSAR UPDATE 4.2-36 Revision 23 December 2016 The reactor vessel internals have provisions to install material test specimens for the reactor vessel material surveillance program (refer to Section 5.2.2.4.4). | ||
(3) Incore Instrumentation The reactor vessel internals have provisions to install incore instrumentation. The incore instrumentation support structure is designed for adequate support of instrumentation during reactor operation (refer to Section 4.2.2.3.3). | (3) Incore Instrumentation The reactor vessel internals have provisions to install incore instrumentation. The incore instrumentation support structure is designed for adequate support of instrumentation during reactor operation (refer to Section 4.2.2.3.3). | ||
4.2.3 REACTIVITY CONTROL SYSTEM 4.2.3.1 Design Bases 4.2.3.1.1 General Design Criterion 2, 1967 - Performance Standards The CRDMs are designed to withstand the effects of, or are protected against, natural phenomena, such as earthquakes. | |||
====4.2.3 REACTIVITY==== | |||
CONTROL SYSTEM 4.2.3.1 Design Bases 4.2.3.1.1 General Design Criterion 2, 1967 - Performance Standards The CRDMs are designed to withstand the effects of, or are protected against, natural phenomena, such as earthquakes. | |||
4.2.3.1.2 General Design Criterion 4, 1987 | 4.2.3.1.2 General Design Criterion 4, 1987 | ||
- Environmental and Dynamic Effects Design Bases Consideration of the dynamic effects associated with main RCL piping postulated pipe ruptures are excluded from the DCPP des ign basis with the approval of LBB methodology by demonstrating that the probability of fluid system piping rupture is extremely low under conditions consistent with the design basis for the piping. | - Environmental and Dynamic Effects Design Bases Consideration of the dynamic effects associated with main RCL piping postulated pipe ruptures are excluded from the DCPP des ign basis with the approval of LBB methodology by demonstrating that the probability of fluid system piping rupture is extremely low under conditions consistent with the design basis for the piping. | ||
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fuel rods. | fuel rods. | ||
The structural elements of the burnable absorber rod are designed to maintain absorber geometry. The rods are designed so that the Al | The structural elements of the burnable absorber rod are designed to maintain absorber geometry. The rods are designed so that the Al 2 O 3-B 4 C material is below 1200°F during normal operation or overpower transients. | ||
4.2.3.2.5 Neutron Source Rods Acceptance Criteria The neutron source rods are designed to withstand: | 4.2.3.2.5 Neutron Source Rods Acceptance Criteria The neutron source rods are designed to withstand: | ||
| Line 1,230: | Line 1,242: | ||
The most effective reactivity control component is the RCCA and its corresponding drive | The most effective reactivity control component is the RCCA and its corresponding drive | ||
rod assemblies. Figure 4.2-15 identifies the rod cluster control and drive rod assembly, | rod assemblies. Figure 4.2-15 identifies the rod cluster control and drive rod assembly, in addition to the interfacing fuel assembly, guide tubes, and CRDM. | ||
in addition to the interfacing fuel assembly, guide tubes, and CRDM. | |||
Guidance for the control rod cluster is provided by the guide tube, as shown in | Guidance for the control rod cluster is provided by the guide tube, as shown in | ||
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steel and the rod spring spacer which is Inconel 750. The absorber rods are fastened securely to the spider to ensure trouble-free service. | steel and the rod spring spacer which is Inconel 750. The absorber rods are fastened securely to the spider to ensure trouble-free service. | ||
The overall length is such that when the assembly is withdrawn through its full travel, | The overall length is such that when the assembly is withdrawn through its full travel, the tips of the absorber rods remain engaged in the guide thimbles so that alignment between rods and thimbles is always maintained. Because the rods are long and | ||
the tips of the absorber rods remain engaged in the guide thimbles so that alignment between rods and thimbles is always maintained. Because the rods are long and | |||
slender, they are relatively free to conform to any small misalignments with the guide | slender, they are relatively free to conform to any small misalignments with the guide | ||
thimble. | thimble. | ||
4.2.3.3.3 Burnable Absorber Assembly Description Each burnable absorber assembly consists of WABA burnable absorber rods attached to a hold down assembly. | 4.2.3.3.3 Burnable Absorber Assembly Description Each burnable absorber assembly consists of WABA burnable absorber rods attached to a hold down assembly. | ||
A WABA rod (refer to Figure 4.2-18a) consists of annular pellets of alumina-boron carbide (Al | A WABA rod (refer to Figure 4.2-18a) consists of annular pellets of alumina-boron carbide (Al 2 O 3-B 4 C) burnable absorber material contai ned within two concentric Zircaloy tubes. These Zircaloy tubes, which form the inner and outer cladding for the WABA rod, are plugged and welded at each end to encapsulate the annular stack of absorber material. The assembled rod is then internally pressurized to 650 psig and seal welded. | ||
are plugged and welded at each end to encapsulate the annular stack of absorber material. The assembled rod is then internally pressurized to 650 psig and seal welded. | |||
The absorber stack lengths are positioned axially within the WABA rods by the use of | The absorber stack lengths are positioned axially within the WABA rods by the use of | ||
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During core loading, it is verified that active source assemblies provide the responding | During core loading, it is verified that active source assemblies provide the responding | ||
source range detectors with a sufficient count rate. For normal source range detectors | source range detectors with a sufficient count rate. For normal source range detectors (N-31 and N-32), and for alternate source ra nge detectors (N-51 and N-52), the following count rate requirements must be met after an installed active source is | ||
(N-31 and N-32), and for alternate source ra nge detectors (N-51 and N-52), the following count rate requirements must be met after an installed active source is | |||
neutronically coupled to a detector: | neutronically coupled to a detector: | ||
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2 FSAR UPDATE 4.2-45 Revision 23 December 2016 4.2.3.3.6 Control Rod Drive Mechanism Description All parts exposed to reactor coolant are made of metals that resist the corrosive action | 2 FSAR UPDATE 4.2-45 Revision 23 December 2016 4.2.3.3.6 Control Rod Drive Mechanism Description All parts exposed to reactor coolant are made of metals that resist the corrosive action | ||
of the water. Three types of metals are used exclusively: stainless steels, nickel alloy, | of the water. Three types of metals are used exclusively: stainless steels, nickel alloy, and cobalt-based alloys. Wherever magnetic flux is carried by parts exposed to the main coolant, 400 series stainless steel is used. Cobalt-based alloys are used for the | ||
and cobalt-based alloys. Wherever magnetic flux is carried by parts exposed to the main coolant, 400 series stainless steel is used. Cobalt-based alloys are used for the | |||
pins and latch tips. Nickel alloy is used for the springs of the latch assemblies, and Type 304 stainless steel for all pressure-containing parts. Hard chrome plating provides | pins and latch tips. Nickel alloy is used for the springs of the latch assemblies, and Type 304 stainless steel for all pressure-containing parts. Hard chrome plating provides | ||
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control rods are withdrawn from the core. | control rods are withdrawn from the core. | ||
(2) The coil stack assembly includes the coil housings, an electrical conduit and connector, and three operating coils: (a) the stationary gripper coil, | (2) The coil stack assembly includes the coil housings, an electrical conduit and connector, and three operating coils: (a) the stationary gripper coil, (b) the movable gripper coil, and (c) the lift coil. | ||
(b) the movable gripper coil, and (c) the lift coil. | |||
Energizing the operation coils causes movement of the pole pieces and | Energizing the operation coils causes movement of the pole pieces and | ||
| Line 1,525: | Line 1,524: | ||
groove. The control rod falls by gravity into the core. The trip occurs as the magnetic | groove. The control rod falls by gravity into the core. The trip occurs as the magnetic | ||
field, holding the stationary gripper plunger half against the stationary gripper pole, | field, holding the stationary gripper plunger half against the stationary gripper pole, collapses, and the stationary gripper plunger half is forced down by the weight acting | ||
collapses, and the stationary gripper plunger half is forced down by the weight acting | |||
upon the latches. After the drive r od assembly is released by the mechanism, it falls freely until the control rods enter the buffer section of their guide tubes. | upon the latches. After the drive r od assembly is released by the mechanism, it falls freely until the control rods enter the buffer section of their guide tubes. | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-47 Revision 23 December 2016 4.2.3.4 Reactivity Control System Design Evaluation 4.2.3.4.1 Reactivity Control Components Design Evaluation The components are analyzed for loads corresponding to normal, upset, emergency, | 2 FSAR UPDATE 4.2-47 Revision 23 December 2016 4.2.3.4 Reactivity Control System Design Evaluation 4.2.3.4.1 Reactivity Control Components Design Evaluation The components are analyzed for loads corresponding to normal, upset, emergency, and faulted conditions. The analysis performed depends on the mode of operation | ||
and faulted conditions. The analysis performed depends on the mode of operation | |||
under consideration. | under consideration. | ||
| Line 1,568: | Line 1,563: | ||
Section 4.2.1.2.3. The stress analysis for the WABA rods assumed a maximum 30 percent gas release, consistent with Reference 28. | Section 4.2.1.2.3. The stress analysis for the WABA rods assumed a maximum 30 percent gas release, consistent with Reference 28. | ||
The WABA rod cladding and rod initial intern al pressure have been designed so that the clad will not rely upon the pellets for support under all Condition I and Condition II events. Rodlet pre-pressurization will support the outer clad against irradiation induced creep collapse in the event of 0% gas release (worst case) from the Al | The WABA rod cladding and rod initial intern al pressure have been designed so that the clad will not rely upon the pellets for support under all Condition I and Condition II events. Rodlet pre-pressurization will support the outer clad against irradiation induced creep collapse in the event of 0% gas release (worst case) from the Al 2 O 3-B 4 C for the design life. Calculations also verify the clad integrity under Condition I and Condition II events with a conservative maximum gas release. | ||
Thermal analyses have shown that the maximum absorber temperature is less than 1200°F for both normal operation (Condition I) and for Condition II upset events. This provides assurance that the He gas release will not exceed limits for the WABA rod's mechanical design life of 18,000 EFPH. This also assures that the Zircaloy clad strain limit is satisfied. A conservatively large heating rate was used in the thermal analyses. | Thermal analyses have shown that the maximum absorber temperature is less than 1200°F for both normal operation (Condition I) and for Condition II upset events. This provides assurance that the He gas release will not exceed limits for the WABA rod's mechanical design life of 18,000 EFPH. This also assures that the Zircaloy clad strain limit is satisfied. A conservatively large heating rate was used in the thermal analyses. | ||
The actual heating rate would be less for the reference design due to the lower B 10 loading. | The actual heating rate would be less for the reference design due to the lower B 10 loading. | ||
An evaluation of the WABA rod design is given in Reference 28. | An evaluation of the WABA rod design is given in Reference 28. | ||
| Line 1,593: | Line 1,587: | ||
quite low, and proper control of Cl | quite low, and proper control of Cl | ||
- and | - and O 2 in the coolant prevents stress corrosion. All of the austenitic stainless steel base material used is processed and fabricated to | ||
preclude sensitization. | preclude sensitization. | ||
| Line 1,657: | Line 1,651: | ||
individual rod into the core. | individual rod into the core. | ||
(5) The Westinghouse RCCA and EP | (5) The Westinghouse RCCA and EP-RCCA models radial vanes are brazed to the spider body and guidance of the RCCA is accomplished by the inner fingers of these vanes. They are therefore the most susceptible to | ||
-RCCA models radial vanes are brazed to the spider body and guidance of the RCCA is accomplished by the inner fingers of these vanes. They are therefore the most susceptible to | |||
mechanical damage. For the Framatome RCCA, the radial vanes are | mechanical damage. For the Framatome RCCA, the radial vanes are | ||
| Line 1,717: | Line 1,710: | ||
borne by this component. | borne by this component. | ||
The burnable absorber rods are clad with either stainless steel or Zircaloy 4. The burnable absorber is Al | The burnable absorber rods are clad with either stainless steel or Zircaloy 4. The burnable absorber is Al 2 O 3-B 4 C annular pellets contain ed within two concentric Zircaloy tubes. Burnable absorber rods are placed in static assemblies and are not subjected to motion which might damage the rods. Further, the guide thimble tubes of the fuel | ||
assembly afford additional protection from damage. | assembly afford additional protection from damage. | ||
| Line 1,723: | Line 1,716: | ||
During the accumulated thousands of years of burnable absorber rodlet operating experience, only one instance of penetration of the stainless steel burnable absorber cladding has been observed. The consequences of cladding breach are also small. It | During the accumulated thousands of years of burnable absorber rodlet operating experience, only one instance of penetration of the stainless steel burnable absorber cladding has been observed. The consequences of cladding breach are also small. It | ||
is anticipated that upon cladding breach, the B | is anticipated that upon cladding breach, the B 4 C would be leached by the coolant water and that localized power peaking of a few percent would occur; no design criteria would be violated. Additional information on the consequences of postulated WABA rod | ||
failures is presented in Reference 28. | failures is presented in Reference 28. | ||
| Line 1,809: | Line 1,802: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.2-54 Revision 23 December 2016 (4) Coil Fit in Coil Housing | 2 FSAR UPDATE 4.2-54 Revision 23 December 2016 (4) Coil Fit in Coil Housing - CRDM and coil housing clearances are selected so that coil heatup results in a close or tight fit. This facilitates thermal transfer and coil cooling in a hot CRDM. | ||
- CRDM and coil housing clearances are selected so that coil heatup results in a close or tight fit. This facilitates thermal transfer and coil cooling in a hot CRDM. | |||
4.2.3.5 Safety Evaluation 4.2.3.5.1 General Design Criterion 2, 1967 - Performance Standards A dynamic seismic analysis is performed on the CRDMs to confirm their ability to trip under a postulated seismic disturbance while maintaining resulting stresses under allowable values (refer to Section 5.2.2.1.15.7). | 4.2.3.5 Safety Evaluation 4.2.3.5.1 General Design Criterion 2, 1967 - Performance Standards A dynamic seismic analysis is performed on the CRDMs to confirm their ability to trip under a postulated seismic disturbance while maintaining resulting stresses under allowable values (refer to Section 5.2.2.1.15.7). | ||
| Line 1,917: | Line 1,909: | ||
==2.4 REFERENCES== | ==2.4 REFERENCES== | ||
: 1. J. A. Christensen, et al, Melting Point of Irradiated UO 2, WCAP-6065, February 1965. | : 1. J. A. Christensen, et al, Melting Point of Irradiated UO 2 , WCAP-6065, February 1965. | ||
: 2. J. Cohen, Development and Properties of Silver-Based Alloys as Control Rod Materials for Pressurized Water Reactors, WAPD-214, December 1959. | : 2. J. Cohen, Development and Properties of Silver-Based Alloys as Control Rod Materials for Pressurized Water Reactors, WAPD-214, December 1959. | ||
: 3. Deleted in Revision 23. | : 3. Deleted in Revision 23. | ||
| Line 1,959: | Line 1,951: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-1 Revision 23 December 2016 4.3 NUCLEAR DESIGN The nuclear design of the reactors for DCPP Unit 1 and Unit 2, including fuel and reactivity control systems, is described in this section; the analytical methods used in | 2 FSAR UPDATE 4.3-1 Revision 23 December 2016 | ||
===4.3 NUCLEAR=== | |||
DESIGN The nuclear design of the reactors for DCPP Unit 1 and Unit 2, including fuel and reactivity control systems, is described in this section; the analytical methods used in | |||
reactor design and evaluation are also discussed. | reactor design and evaluation are also discussed. | ||
| Line 1,991: | Line 1,986: | ||
occurrences through conservative design, and maintained by the action of the control | occurrences through conservative design, and maintained by the action of the control | ||
system. The requirements for Condition II occurrences are met by providing an adequate protection system that monitors reactor parameters. The control and protection systems are described in Chapter 7 and the consequences of Conditions II, | system. The requirements for Condition II occurrences are met by providing an adequate protection system that monitors reactor parameters. The control and protection systems are described in Chapter 7 and the consequences of Conditions II, III, and IV occurrences are discussed in Chapter 15. | ||
DCPP UNITS 1 & | |||
2 FSAR UPDATE 4.3-2 Revision 23 December 2016 | |||
====4.3.1 DESIGN==== | |||
BASES The design bases and functional requirements for the nuclear design of the fuel and | |||
reactivity control system, and the relationships of these design bases to the GDC of July 1971, are presented in this section. Where appropriate, supplemental criteria, such | reactivity control system, and the relationships of these design bases to the GDC of July 1971, are presented in this section. Where appropriate, supplemental criteria, such | ||
| Line 2,009: | Line 2,005: | ||
4.3.1.6 General Design Criterion 28, 1971 - Reactivity Limits The reactivity control systems are designed to assure that the effects of postulated reactivity accidents neither result in damage to the reactor coolant pressure boundary greater than limited local yielding nor cause sufficient damage to significantly impair the capability to cool the core. | 4.3.1.6 General Design Criterion 28, 1971 - Reactivity Limits The reactivity control systems are designed to assure that the effects of postulated reactivity accidents neither result in damage to the reactor coolant pressure boundary greater than limited local yielding nor cause sufficient damage to significantly impair the capability to cool the core. | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-3 Revision 23 December 2016 4.3.2 | 2 FSAR UPDATE 4.3-3 Revision 23 December 2016 | ||
====4.3.2 NUCLEAR==== | |||
DESIGN ACCEPTANCE CRITERIA 4.3.2.1 Fuel Burnup Sufficient reactivity should be incorporated in the fuel to attain a desired region average discharge burnup. | |||
4.3.2.2 Control of Power Distribution The nuclear design basis, with at least a 95 percent confidence level, is as follows: | 4.3.2.2 Control of Power Distribution The nuclear design basis, with at least a 95 percent confidence level, is as follows: | ||
(1) The fuel will not be operated at greater than 14.3 kW/ft under normal operating conditions, including an allowance of 2 percent for calorimetric error and not including the power spike factor due to densification effects | (1) The fuel will not be operated at greater than 14.3 kW/ft under normal operating conditions, including an allowance of 2 percent for calorimetric error and not including the power spike factor due to densification effects (Reference 31). | ||
(Reference 31). | |||
(2) Under abnormal conditions, including the maximum overpower condition, the fuel peak power will not cause melting as defined in Section 4.4.2.2. | (2) Under abnormal conditions, including the maximum overpower condition, the fuel peak power will not cause melting as defined in Section 4.4.2.2. | ||
(3) The fuel will not operate with a power distribution that violates the DNB design basis (i.e., the departure from nucleate boiling ratio {DNBR} shall not be less than the design limit DNBR, as discussed in Section 4.4.2) under Conditions I and II events, including the maximum overpower | (3) The fuel will not operate with a power distribution that violates the DNB design basis (i.e., the departure from nucleate boiling ratio {DNBR} shall not be less than the design limit DNBR, as discussed in Section 4.4.2) under Conditions I and II events, including the maximum overpower | ||
| Line 2,032: | Line 2,029: | ||
they occur, can be reliably and readily detected and suppressed. | they occur, can be reliably and readily detected and suppressed. | ||
4.3.2.5 Maximum Controlled Reactivity Insertion Rate The maximum reactivity insertion rate due to withdrawal of RCCAs, or by boron dilution, is limited. This limit, expressed as a maximum reactivity change rate (75 pcm/sec) is set such that the peak heat generation rate does not exceed the maximum allowable, | 4.3.2.5 Maximum Controlled Reactivity Insertion Rate The maximum reactivity insertion rate due to withdrawal of RCCAs, or by boron dilution, is limited. This limit, expressed as a maximum reactivity change rate (75 pcm/sec) is set such that the peak heat generation rate does not exceed the maximum allowable, and DNBR is not below the minimum allowable at overpower conditions (refer to Note (b) of Table 4.3-1). | ||
and DNBR is not below the minimum allowable at overpower conditions (refer to Note (b) of Table 4.3-1). | |||
4.3.2.6 Shutdown Margins | 4.3.2.6 Shutdown Margins | ||
| Line 2,041: | Line 2,036: | ||
remain untripped in its full-out position (stuck rod criterion). | remain untripped in its full-out position (stuck rod criterion). | ||
4.3.3 DESCRIPTION 4.3.3.1 Nuclear Design Description The reactor core consists of 193 fuel assemblies arranged in a pattern that approximates a right circular cylinder. Each fuel assembly contains a 17 x 17 rod array composed of 264 fuel rods, 24 RCCA guide tubes, and an incore instrumentation | 4. | ||
==3.3 DESCRIPTION== | |||
4.3.3.1 Nuclear Design Description The reactor core consists of 193 fuel assemblies arranged in a pattern that approximates a right circular cylinder. Each fuel assembly contains a 17 x 17 rod array composed of 264 fuel rods, 24 RCCA guide tubes, and an incore instrumentation | |||
thimble. Each rod is held in place by spacer grids and top and bottom nozzles. The | thimble. Each rod is held in place by spacer grids and top and bottom nozzles. The | ||
| Line 2,083: | Line 2,082: | ||
for long-term reactivity requirements, such as those due to fuel burnup, fission product | for long-term reactivity requirements, such as those due to fuel burnup, fission product | ||
poisoning, including xenon and samarium, burnable absorber material depletion, and the cold-to-operating moderator temperature change. Using its normal makeup path, | poisoning, including xenon and samarium, burnable absorber material depletion, and the cold-to-operating moderator temperature change. Using its normal makeup path, the CVCS is capable of inserting negative reactivity at a rate of approximately 30 pcm/min when the reactor coolant boron concentration is 100 ppm. In an emergency, the CVCS can insert negative reactivity at approximately 65 pcm/min when | ||
the CVCS is capable of inserting negative reactivity at a rate of approximately 30 pcm/min when the reactor coolant boron concentration is 100 ppm. In an emergency, the CVCS can insert negative reactivity at approximately 65 pcm/min when | |||
the reactor coolant concentration is 1000 ppm, and 75 pcm/min when the reactor | the reactor coolant concentration is 1000 ppm, and 75 pcm/min when the reactor | ||
coolant boron concentration is 100 ppm. The peak xenon burnout rate is 25 pcm/min | coolant boron concentration is 100 ppm. The peak xenon burnout rate is 25 pcm/min (Section 9.3.4 discusses the capability of the CVCS to counteract xenon decay). Rapid | ||
(Section 9.3.4 discusses the capability of the CVCS to counteract xenon decay). Rapid | |||
transient reactivity requirements and safe shutdown requirements are met with control | transient reactivity requirements and safe shutdown requirements are met with control | ||
| Line 2,112: | Line 2,107: | ||
Tables 4.1-1, and 4.3-1 through 4.3-3, summarize the reactor core design parameters | Tables 4.1-1, and 4.3-1 through 4.3-3, summarize the reactor core design parameters | ||
for a typical reload fuel cycle, including reactivity coefficients, delayed neutron fraction, | for a typical reload fuel cycle, including reactivity coefficients, delayed neutron fraction, and neutron lifetimes. | ||
and neutron lifetimes. | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
| Line 2,168: | Line 2,161: | ||
Local heat flux is the heat flux at the surface of the cladding (Btu ft | Local heat flux is the heat flux at the surface of the cladding (Btu ft | ||
- | -2 hr-1). For nominal fuel rod parameters, this differs from linear power density by a constant factor. | ||
Rod power or rod integral power is the linear power density in one rod integrated over | Rod power or rod integral power is the linear power density in one rod integrated over | ||
| Line 2,179: | Line 2,172: | ||
defined as follows: | defined as follows: | ||
F T Q , heat flux hot channel factor , is defined as the maximum local heat flux on the surface of a fuel rod divided by the average fuel rod heat flux, allowing for manufacturing tolerances on fuel pellets and rods. | |||
, is defined as the maximum local heat flux on the surface of a fuel rod divided by the average fuel rod heat flux, allowing for manufacturing tolerances on fuel pellets and rods. | |||
F N Q , nuclear heat flux hot channel factor , is defined as the maximum local fuel rod linear power density divided by the average fuel rod linear power density, assuming nominal | |||
, is defined as the maximum local fuel rod linear power density divided by the average fuel rod linear power density, assuming nominal | |||
fuel pellet and rod parameters. (No densification effects included.) | fuel pellet and rod parameters. (No densification effects included.) | ||
F E Q , engineering heat flux hot channel factor , is the allowance on heat flux required for manufacturing tolerances. The engineering factor allows for local variations in | |||
, is the allowance on heat flux required for manufacturing tolerances. The engineering factor allows for local variations in | |||
enrichment, pellet density and diameter, surface area of the fuel rod, and eccentricity of the gap between pellet and clad. | enrichment, pellet density and diameter, surface area of the fuel rod, and eccentricity of the gap between pellet and clad. | ||
Combined statistically, the net effect is a factor of 1.03 to be applied to the fuel rod surface heat flux. | Combined statistically, the net effect is a factor of 1.03 to be applied to the fuel rod surface heat flux. | ||
F N H, nuclear enthalpy rise hot channel factor , is defined as the ratio of the integral of linear power along the rod with the highest integrated power to the average rod power. | |||
, is defined as the ratio of the integral of linear power along the rod with the highest integrated power to the average rod power. | |||
Manufacturing tolerances, hot channel powe r distribution, and surrounding channel power distributions are treated explicitly in the calculation of DNBR described in Section 4.4. | Manufacturing tolerances, hot channel powe r distribution, and surrounding channel power distributions are treated explicitly in the calculation of DNBR described in Section 4.4. | ||
For the purposes of discussion, it is convenient to define subfactors of | For the purposes of discussion, it is convenient to define subfactors of F T Q; design limits are set, however, in terms of the total peaking factor: | ||
F T Q factor channel hotflux heat or factor peaking Total | |||
= | = | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-8 Revision 23 December 2016 kW/ft AveragekW/ft Maximum | 2 FSAR UPDATE 4.3-8 Revision 23 December 2016 kW/ft AveragekW/ft Maximum | ||
= (4.3-1) without densification effects. | = (4.3-1) without densification effects. | ||
F T Q = F N Qx F E Q = max [F N XY (z) x P(z)] x F N U x F E Q (4.3-2) where: F N Q and F E Q are defined above. | |||
F N U = the measurement uncertainty associated with a full core flux map with movable detectors or PDMS F N XY(z) = ratio of peak power density to average power density in the horizontal plane of peak local power P(z) = ratio of the power per unit core height in the horizontal plane at elevation Z to the average value of power per unit core height 4.3.3.2.2 Radial Power Distributions | |||
The power shape in horizontal sections of the core at full power is a function of the fuel and burnable absorber loading patterns, and the presence or absence of a single bank | The power shape in horizontal sections of the core at full power is a function of the fuel and burnable absorber loading patterns, and the presence or absence of a single bank | ||
| Line 2,224: | Line 2,213: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-9 Revision 23 December 2016 Since hot channel location varies from time to time, a single reference radial design power distribution is selected for DNB calculations. This reference power distribution, | 2 FSAR UPDATE 4.3-9 Revision 23 December 2016 Since hot channel location varies from time to time, a single reference radial design power distribution is selected for DNB calculations. This reference power distribution, normalized to core average power, is chosen conservatively to concentrate power in | ||
normalized to core average power, is chosen conservatively to concentrate power in | |||
one area of the core, minimizing the benefits of flow redistribution. | one area of the core, minimizing the benefits of flow redistribution. | ||
| Line 2,239: | Line 2,226: | ||
Since the detailed power distribution surrounding the hot channel varies from time to | Since the detailed power distribution surrounding the hot channel varies from time to | ||
time, a conservatively flat assembly power distribution is assumed in the DNB analysis, | time, a conservatively flat assembly power distribution is assumed in the DNB analysis, described in Section 4.4, with the rod of maximum integrated power artificially raised to the design value of F N H. The nuclear design considers all fuel cycles and all operating conditions to ensure that a flatter assembly power distribution does not occur with | ||
limiting values of F N H. 4.3.3.2.4 Axial Power Distributions The shape of the power profile in the axial direction is largely under the control of the | |||
limiting values of F | |||
operator through the manual operation of the control rods or the automatic motion of the control rods responding to manual operation of the CVCS. Nuclear effects that cause variations in the axial power shape include moderator density, Doppler effect on | operator through the manual operation of the control rods or the automatic motion of the control rods responding to manual operation of the CVCS. Nuclear effects that cause variations in the axial power shape include moderator density, Doppler effect on | ||
| Line 2,256: | Line 2,241: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-10 Revision 23 December 2016 Representative axial power shapes for BOL, MOL | 2 FSAR UPDATE 4.3-10 Revision 23 December 2016 Representative axial power shapes for BOL, MOL , and EOL conditions covering a wide range, including power shape changes achieved by skewing xenon distributions, are shown in Figures 4.3-15 through 4.3-17. | ||
, and EOL conditions covering a wide range, including power shape changes achieved by skewing xenon distributions, are shown in Figures 4.3-15 through 4.3-17. | |||
4.3.3.2.5 Local Power Peaking Fuel densification causes fuel pellets to shrin k both axially and radially. Pellet shrinkage combined with random hang-up of fuel pellets results in gaps in the fuel column when | 4.3.3.2.5 Local Power Peaking Fuel densification causes fuel pellets to shrin k both axially and radially. Pellet shrinkage combined with random hang-up of fuel pellets results in gaps in the fuel column when | ||
| Line 2,308: | Line 2,292: | ||
Westinghouse PWR, on the defined operating procedures, and on the measures taken to preclude exceeding design limits is presented in References 23, 29, and 30. | Westinghouse PWR, on the defined operating procedures, and on the measures taken to preclude exceeding design limits is presented in References 23, 29, and 30. | ||
The upper bound on peaking factors, F | The upper bound on peaking factors, F T Q and F N H, includes all of the nuclear effects that influence the radial and/or axial power distributions throughout core life for various modes of operation, including load follow, reduced power operation, and axial xenon | ||
transients. | transients. | ||
| Line 2,376: | Line 2,360: | ||
on the radial peak of xenon redistribution tha t occur, following the withdrawal of a control bank (or banks) from a rodded region, are obtained from three-dimensional calculations. The factor to be applied to the radial peak is obtained from calculations in DCPP UNITS 1 & | on the radial peak of xenon redistribution tha t occur, following the withdrawal of a control bank (or banks) from a rodded region, are obtained from three-dimensional calculations. The factor to be applied to the radial peak is obtained from calculations in DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-13 Revision 23 December 2016 which the xenon distribution is preconditioned by the presence of control rods and then allowed to redistribute for several hours. A d etailed discussion of this effect may be found in References 23 and 29. In addition to the 1.05 conservatism factor, the calculated values are increased by a factor of 1.03 for the engineering factor F | 2 FSAR UPDATE 4.3-13 Revision 23 December 2016 which the xenon distribution is preconditioned by the presence of control rods and then allowed to redistribute for several hours. A d etailed discussion of this effect may be found in References 23 and 29. In addition to the 1.05 conservatism factor, the calculated values are increased by a factor of 1.03 for the engineering factor F E Q. | ||
The envelope drawn over the calculated (max F | The envelope drawn over the calculated (max F T Q x Power) points, as shown in Figure 4.3-23 is an example of an upper bound envelope on local power density versus elevation in the core. | ||
Cycle-specific values are calculated each cycle. | Cycle-specific values are calculated each cycle. | ||
Finally, this upper bound envelope is based on operation within an allowed range of axial flux difference limits. These limits are detailed in the Core Operating Limits Reports and rely only on excore surveillance supplemented by the required normal | Finally, this upper bound envelope is based on operation within an allowed range of axial flux difference limits. These limits are detailed in the Core Operating Limits Reports and rely only on excore surveillance supplemented by the required normal | ||
| Line 2,389: | Line 2,373: | ||
14.3 kW/ft at 102 percent power. | 14.3 kW/ft at 102 percent power. | ||
To determine reactor protection system setpoints, with respect to power distributions, | To determine reactor protection system setpoints, with respect to power distributions, three categories of events are considered: rod control equipment malfunctions, operator errors of commission, and operator errors of omission. In evaluating these three categories, the core is assumed to be operating within the four constraints | ||
three categories of events are considered: rod control equipment malfunctions, | |||
operator errors of commission, and operator errors of omission. In evaluating these three categories, the core is assumed to be operating within the four constraints | |||
described above. | described above. | ||
| Line 2,421: | Line 2,401: | ||
conditions not included in normal operating conditions. | conditions not included in normal operating conditions. | ||
The third category assumes that the operator fails to take action to correct a flux difference violation. The results shown in Figure 4.3-22 are F | The third category assumes that the operator fails to take action to correct a flux difference violation. The results shown in Figure 4.3-22 are F T Q multiplied by 102 percent power, including an allowance for calorimetric error. The peak linear power DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-14 Revision 23 December 2016 does not exceed 22.0 kW/ft, provided the operator's error does not continue for a period which is long compared to the xenon time constant. It should be noted that a reactor | 2 FSAR UPDATE 4.3-14 Revision 23 December 2016 does not exceed 22.0 kW/ft, provided the operator's error does not continue for a period which is long compared to the xenon time constant. It should be noted that a reactor | ||
| Line 2,428: | Line 2,408: | ||
error. Additional detailed discussion of these analyses is presented in Reference 23. | error. Additional detailed discussion of these analyses is presented in Reference 23. | ||
Analyses of possible operating power shapes for the DCPP reactor show that the appropriate hot channel factors F | Analyses of possible operating power shapes for the DCPP reactor show that the appropriate hot channel factors F T Q and F N H for peak local power density, and for DNB analysis at full power, are the values given in Table 4.3-1 and addressed in the Technical Specifications. | ||
The maximum allowable F | The maximum allowable F T Q can increase with decreasing power, as shown in the Technical Specifications. Increasing F N H with decreasing power is permitted by the DNB protection setpoints and allows radial power shape changes with rod insertion to the insertion limits, as described in Section 4.4.3.13. | ||
The allowances for increased F | The allowances for increased F N H permitted is: | ||
F N H = 1.65 [1 + 0.3 (1-P)] for VANTAGE+ fuel (4.3-5) This becomes a design basis criterion, which is used for establishing acceptable control rod patterns and control bank sequencing. | |||
Likewise, fuel loading patterns for each cycle are selected with consideration of this design criterion. The worst values of F | Likewise, fuel loading patterns for each cycle are selected with consideration of this design criterion. The worst values of F N H for possible rod configurations occurring in normal operation are used in verifying that this criterion is met. Typical radial factors and radial power distributions are shown in | ||
Figures 4.3-7 through 4.3-12. The worst values generally occur when the rods are | Figures 4.3-7 through 4.3-12. The worst values generally occur when the rods are | ||
| Line 2,453: | Line 2,433: | ||
4.3.3.2.7 Experimental Verification of Power Distribution Analysis This subject, which is discussed in depth in Reference 1, is summarized here. | 4.3.3.2.7 Experimental Verification of Power Distribution Analysis This subject, which is discussed in depth in Reference 1, is summarized here. | ||
To measure the peak local power density, F | To measure the peak local power density, F T Q , with the movable detector system described in Sections 4.4.7 and 7.7.2.9.2, the following uncertainties are considered: | ||
(1) Reproducibility of the measured signal | (1) Reproducibility of the measured signal | ||
| Line 2,467: | Line 2,447: | ||
simulated guide thimbles, control rods, burnable poisons, etc. | simulated guide thimbles, control rods, burnable poisons, etc. | ||
Reference 1 concludes that the uncertainty associated with the peak nuclear heat flux factor, F | Reference 1 concludes that the uncertainty associated with the peak nuclear heat flux factor, F T Q , is 4.58 percent at the 95 percent confidence level with only 5 percent of the measurements greater than the inferred value. | ||
In comparing measured power distributions (or detector currents) against the | In comparing measured power distributions (or detector currents) against the | ||
| Line 2,477: | Line 2,457: | ||
Figure 4.3-25 for one of the maps of Reference 1, which is similar to hundreds of maps | Figure 4.3-25 for one of the maps of Reference 1, which is similar to hundreds of maps | ||
taken since then on various reactors, confirming the adequacy of the 5 percent uncertainty allowance on F | taken since then on various reactors, confirming the adequacy of the 5 percent uncertainty allowance on F T Q. A similar analysis for the uncertainty in F N H (rod integral power) measurements results in an allowance of 3.68 percent at the equivalent of a 2 confidence level. For historical reasons, an 8 percent uncertainty factor is allowed in the nuclear design basis; that is, the predicted rod integrals at full power must not exceed the design F N H less 8 percent. | ||
the predicted rod integrals at full power must not exceed the design F | |||
This 8 percent may be reduced in final design to 4 percent to allow a wider range of acceptable axial power distributions in the DNB analysis and still meet the acceptance criteria of Section 4.3.2.2. | This 8 percent may be reduced in final design to 4 percent to allow a wider range of acceptable axial power distributions in the DNB analysis and still meet the acceptance criteria of Section 4.3.2.2. | ||
| Line 2,494: | Line 2,472: | ||
2 FSAR UPDATE 4.3-16 Revision 23 December 2016 (2) Data with unusual values of AO are obtained as part of the excore detector calibration exercise which is performed monthly. | 2 FSAR UPDATE 4.3-16 Revision 23 December 2016 (2) Data with unusual values of AO are obtained as part of the excore detector calibration exercise which is performed monthly. | ||
(3) Special tests have been performed in load follow and other transient xenon conditions which have yielded useful information on power distributions. | (3) Special tests have been performed in load follow and other transient xenon conditions which have yielded useful information on power distributions. | ||
These data are presented in detail in Reference 3. Figure 4.3-27 contains a summary of measured values of F | These data are presented in detail in Reference 3. Figure 4.3-27 contains a summary of measured values of F T Q as a function of AO for five plants from that report. | ||
4.3.3.2.8 Testing An extensive series of physics tests is performed on first cores. These tests and the | 4.3.3.2.8 Testing An extensive series of physics tests is performed on first cores. These tests and the | ||
| Line 2,576: | Line 2,554: | ||
2 FSAR UPDATE 4.3-18 Revision 23 December 2016 hardened spectrum also causes a decrease in the fission to capture ratio in U-235 and Pu-239. Both of these effects make the MTC more negative. Since water density decreases as temperature increases, the MTC (density) becomes more negative with increasing temperature. | 2 FSAR UPDATE 4.3-18 Revision 23 December 2016 hardened spectrum also causes a decrease in the fission to capture ratio in U-235 and Pu-239. Both of these effects make the MTC more negative. Since water density decreases as temperature increases, the MTC (density) becomes more negative with increasing temperature. | ||
The soluble boron also affects the MTC (density) since its density, like that of water, | The soluble boron also affects the MTC (density) since its density, like that of water, also decreases when the coolant temperature rises. Therefore, a decrease in the | ||
also decreases when the coolant temperature rises. Therefore, a decrease in the | |||
soluble poison concentration introduces a positive component into the moderator | soluble poison concentration introduces a positive component into the moderator | ||
| Line 2,588: | Line 2,564: | ||
initial hot boron concentration is sufficiently low, making the MTC negative at full power | initial hot boron concentration is sufficiently low, making the MTC negative at full power | ||
operating temperatures. The effect of control rods is to make the moderator coefficient more negative by reducing the required soluble boron concentration and by increasing | operating temperatures. The effect of control rods is to make the moderator coefficient more negative by reducing the required soluble boron concentration and by increasing "leakage" from the core. | ||
"leakage" from the core. | |||
With burnup, the MTC normally becomes more negative primarily as a result of boric | With burnup, the MTC normally becomes more negative primarily as a result of boric | ||
| Line 2,635: | Line 2,609: | ||
power level changes is called the total power coefficient, and is expressed in terms of | power level changes is called the total power coefficient, and is expressed in terms of | ||
reactivity change per percent power change. The power coefficient at BOL, MOL, and EOL conditions is given in Figure 4.3-35. It becomes more negative with burnup, | reactivity change per percent power change. The power coefficient at BOL, MOL, and EOL conditions is given in Figure 4.3-35. It becomes more negative with burnup, reflecting the combined effect on moderator and fuel temperature coefficients of burnup. | ||
reflecting the combined effect on moderator and fuel temperature coefficients of burnup. | |||
The power defect (integral reactivity effect) at BOL, MOL, and EOL is given in Figure 4.3-36. | The power defect (integral reactivity effect) at BOL, MOL, and EOL is given in Figure 4.3-36. | ||
| Line 2,693: | Line 2,665: | ||
requirement at EOL. | requirement at EOL. | ||
4.3.3.4.3 Redistribution During full power operation, the coolant density decreases with core height and this, | 4.3.3.4.3 Redistribution During full power operation, the coolant density decreases with core height and this, together with partial insertion of control rods, results in less fuel depletion near the top of | ||
together with partial insertion of control rods, results in less fuel depletion near the top of | |||
the core. Under steady state conditions, the relative power distribution will be slightly | the core. Under steady state conditions, the relative power distribution will be slightly | ||
| Line 2,801: | Line 2,771: | ||
4.3.3.5.4 Peak Xenon Startup Peak xenon buildup is compensated by the boron control system. Startup from the peak xenon condition is accomplished with a combination of rod motion and boron | 4.3.3.5.4 Peak Xenon Startup Peak xenon buildup is compensated by the boron control system. Startup from the peak xenon condition is accomplished with a combination of rod motion and boron | ||
dilution. Boron dilution may be made at any time, including the shutdown period, | dilution. Boron dilution may be made at any time, including the shutdown period, provided the SDM is maintained. | ||
provided the SDM is maintained. | |||
4.3.3.5.5 Load Follow Con trol and Xenon Control The DCPP units are usually base loaded; however, it is expected that during certain | 4.3.3.5.5 Load Follow Con trol and Xenon Control The DCPP units are usually base loaded; however, it is expected that during certain | ||
| Line 2,826: | Line 2,794: | ||
describe a particular grouping of control assemblies. The RCCA patterns are displayed | describe a particular grouping of control assemblies. The RCCA patterns are displayed | ||
in Figures 4.3-37 and 4.3-38 for Unit 1 and Unit 2, respectively. These patterns are not expected to change during the life of the units. The control banks are labeled A, B, C, | in Figures 4.3-37 and 4.3-38 for Unit 1 and Unit 2, respectively. These patterns are not expected to change during the life of the units. The control banks are labeled A, B, C, and D, and the shutdown banks are labeled SA, SB, SC and SD. | ||
The two criteria used to select the control groups are: (a) the total reactivity worth must be adequate to meet the requirements specified in Tables 4.3-2 and 4.3-3, and (b) because these rods may be partially inserted at power operation, the total power | |||
The two criteria used to select the control groups are: (a) the total reactivity worth must be adequate to meet the requirements specified in Tables 4.3-2 and 4.3-3, and | |||
(b) because these rods may be partially inserted at power operation, the total power | |||
peaking factor should be low enough to ensure that power capability requirements are | peaking factor should be low enough to ensure that power capability requirements are | ||
| Line 2,859: | Line 2,823: | ||
2 FSAR UPDATE 4.3-25 Revision 23 December 2016 Allowable deviations due to misaligned control rods are discussed in the Technical Specifications. | 2 FSAR UPDATE 4.3-25 Revision 23 December 2016 Allowable deviations due to misaligned control rods are discussed in the Technical Specifications. | ||
A representative calculation for two banks of control rods withdrawn simultaneously | A representative calculation for two banks of control rods withdrawn simultaneously (rod withdrawal accident) at EOL is shown in Figure 4.3-39. Calculation of control rod reactivity worth versus time following reactor trip involves both control rod velocity and | ||
(rod withdrawal accident) at EOL is shown in Figure 4.3-39. Calculation of control rod reactivity worth versus time following reactor trip involves both control rod velocity and | |||
differential reactivity worth. Rod position versus time of travel after rod release is shown | differential reactivity worth. Rod position versus time of travel after rod release is shown | ||
| Line 2,915: | Line 2,877: | ||
direction or in the X-Y plane, as: | direction or in the X-Y plane, as: | ||
();1i, | ();1i,icb 2=+= (4.3-6) where b is defined as the stability index and T = 2/c as the oscillation period of the first harmonic. The time-dependence of the first harmonic in the power distribution can now be represented as: | ||
()ctcosaeeAtbtt== (4.3-7) where A and a are constants. The stability i ndex can also be obtained approximately by: | ()ctcosaeeAtbtt== (4.3-7) where A and a are constants. The stability i ndex can also be obtained approximately by: | ||
+ | +n A1n A ln T 1 = b (4.3-8) where A n , A n+1 are the successive peak amplitudes of the oscillation, and T is the time period between the successive peaks. | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
| Line 2,935: | Line 2,897: | ||
(b) The reactor core becomes less stable as fuel burnup progresses, and the axial stability index was essentially zero at 12,000 | (b) The reactor core becomes less stable as fuel burnup progresses, and the axial stability index was essentially zero at 12,000 | ||
MWD/MTU. | MWD/MTU. (2) Measurements in the X-Y Plane Two X-Y xenon oscillation tests were performed at a PWR plant with a | ||
(2) Measurements in the X-Y Plane Two X-Y xenon oscillation tests were performed at a PWR plant with a | |||
core height of 12 feet and 157 fuel asse mblies. This plant had the highest power output of any Westinghouse PWR ope rating in 1972. The first test was conducted at a core average burnup of 1540 MWD/MTU and the | core height of 12 feet and 157 fuel asse mblies. This plant had the highest power output of any Westinghouse PWR ope rating in 1972. The first test was conducted at a core average burnup of 1540 MWD/MTU and the | ||
| Line 2,979: | Line 2,940: | ||
An analytical simulation of the first X-Y xenon oscillation test shows a calculated stability index of -0.081 hr | An analytical simulation of the first X-Y xenon oscillation test shows a calculated stability index of -0.081 hr | ||
-1, in good agreement with the measured value of -0.076 hr | -1 , in good agreement with the measured value of -0.076 hr | ||
-1. As indicated earlier, the second X-Y xenon test showed that the core had become more | -1. As indicated earlier, the second X-Y xenon test showed that the core had become more | ||
| Line 3,011: | Line 2,972: | ||
this core, as discussed in Sections 4.3.3.8.4 and 4.3.3.8.5, make it very unlikely that a sustained X-Y oscillation can occur in a core with 193 | this core, as discussed in Sections 4.3.3.8.4 and 4.3.3.8.5, make it very unlikely that a sustained X-Y oscillation can occur in a core with 193 | ||
assemblies. In the unlikely event that X-Y oscillations occur, backup actions are possible and would be implemented, if necessary, to increase the natural stability of the core until tests demonstrate a suitable stability, | assemblies. In the unlikely event that X-Y oscillations occur, backup actions are possible and would be implemented, if necessary, to increase the natural stability of the core until tests demonstrate a suitable stability, by making the MTC more negative. | ||
by making the MTC more negative. | |||
A more detailed discussion of the power distribution control in PWR cores | A more detailed discussion of the power distribution control in PWR cores | ||
| Line 3,103: | Line 3,062: | ||
Westinghouse version of the LEOPARD and CINDER codes, which are linked internally and provide burnup-dependent cross-sections. Normally, a simplified approximation of the main fuel chains is used; however, where needed, a complete solution for all the | Westinghouse version of the LEOPARD and CINDER codes, which are linked internally and provide burnup-dependent cross-sections. Normally, a simplified approximation of the main fuel chains is used; however, where needed, a complete solution for all the | ||
significant isotopes in the fuel chains from Th-232 to Cm-244 is available | significant isotopes in the fuel chains from Th-232 to Cm-244 is available (Reference 17). Cross-section library tapes contain microscopic cross-sections from the ENDF/B (Reference 18) library, with a few exceptions, where other data provide better agreement with critical experiments, isotopic measurements, and plant critical | ||
(Reference 17). Cross-section library tapes contain microscopic cross-sections from the ENDF/B (Reference 18) library, with a few exceptions, where other data provide better agreement with critical experiments, isotopic measurements, and plant critical | |||
boron values. | boron values. | ||
| Line 3,126: | Line 3,083: | ||
Baffle group constants are calculated from an average of core and radial reflector microscopic group constants for stainless steel. | Baffle group constants are calculated from an average of core and radial reflector microscopic group constants for stainless steel. | ||
Group constants for control rods are calculated in a linked version of the HAMMER | Group constants for control rods are calculated in a linked version of the HAMMER (Reference 19) and AIM (Reference 20) codes to provide an improved treatment of self- | ||
(Reference 19) and AIM (Reference 20) codes to provide an improved treatment of self- | |||
shielding in the broad resonance structure of the appropriate isotopes at epithermal | shielding in the broad resonance structure of the appropriate isotopes at epithermal | ||
| Line 3,147: | Line 3,102: | ||
Validation of the cross-section method is based on analysis of critical experiments (refer to Table 4.3-7), isotopic data (refer to Table 4.3-8), plant critical boron (C B) values at hot DCPP UNITS 1 & | Validation of the cross-section method is based on analysis of critical experiments (refer to Table 4.3-7), isotopic data (refer to Table 4.3-8), plant critical boron (C B) values at hot DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.3-33 Revision 23 December 2016 zero power (HZP), BOL (refer to Table 4.3-9), | 2 FSAR UPDATE 4.3-33 Revision 23 December 2016 zero power (HZP), BOL (refer to Table 4.3-9), and at HFP as a function of burnup (refer to Figures 4.3-45 through 4.3-47). Control rod worth measurements are shown in Table 4.3-10. Confirmatory critical experiments on burnable absorbers are described in Reference 21. | ||
and at HFP as a function of burnup (refer to Figures 4.3-45 through 4.3-47). Control rod worth measurements are shown in Table 4.3-10. Confirmatory critical experiments on burnable absorbers are described in Reference 21. | |||
The PHOENIX-P computer code is a two-dimensional, multi-group, transport based | The PHOENIX-P computer code is a two-dimensional, multi-group, transport based | ||
| Line 3,186: | Line 3,140: | ||
Reactor cores. | Reactor cores. | ||
Group constants for burnable absorber cells, guide thimbles, instrument thimbles, | Group constants for burnable absorber cells, guide thimbles, instrument thimbles, control rod cells and other non-fuel cells can be obtained directly from PHOENIX-P | ||
control rod cells and other non-fuel cells can be obtained directly from PHOENIX-P | |||
without any adjustments such as those required in the cell or 1D lattice codes. | without any adjustments such as those required in the cell or 1D lattice codes. | ||
| Line 3,207: | Line 3,159: | ||
The agreement in the PHOENIX-P methodology and PHOENIX-P/ANC core model qualification demonstrates the high accuracy of the PHOENIX-P/ANC advanced design system for multidimensional nucl ear analysis of PWR cores. This qualification data base demonstrates the performance of this system for a wide range of applications performed in the design, safety, licensing and operational follow of PWR cores. Refer to Reference 27 for additional details on experimental verification. | The agreement in the PHOENIX-P methodology and PHOENIX-P/ANC core model qualification demonstrates the high accuracy of the PHOENIX-P/ANC advanced design system for multidimensional nucl ear analysis of PWR cores. This qualification data base demonstrates the performance of this system for a wide range of applications performed in the design, safety, licensing and operational follow of PWR cores. Refer to Reference 27 for additional details on experimental verification. | ||
The accuracy of APOLLO predictions for reactivity and axial power shapes is comparable to that for 3D ANC-based calculations (References 26 and 27). | The accuracy of APOLLO predictions for reactivity and axial power shapes is comparable to that for 3D ANC-based calculations (References 26 and 27). | ||
4.3.4 SAFETY EVALUATION 4.3.4.1 General Design Criterion 10, 1971 - Reactor Design The reactor core and associated coolant, control, and protection systems are designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation, including the effects of anticipated operational occurrences. | |||
====4.3.4 SAFETY==== | |||
EVALUATION 4.3.4.1 General Design Criterion 10, 1971 - Reactor Design The reactor core and associated coolant, control, and protection systems are designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation, including the effects of anticipated operational occurrences. | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
| Line 3,223: | Line 3,177: | ||
equilibrium xenon, samarium, and other fission products present. The end of design | equilibrium xenon, samarium, and other fission products present. The end of design | ||
cycle life is defined to occur when the chemical shim concentration is essentially zero, | cycle life is defined to occur when the chemical shim concentration is essentially zero, with control rods present to the degree neces sary for operational requirements (e.g., the controlling bank at the "bite" position). In terms of chemical shim boron concentration, this represents approximately 10 ppm with no control rod insertion. | ||
with control rods present to the degree neces sary for operational requirements (e.g., the controlling bank at the "bite" position). In terms of chemical shim boron concentration, | |||
this represents approximately 10 ppm with no control rod insertion. | |||
4.3.4.1.2 Control of Power Distribution | 4.3.4.1.2 Control of Power Distribution | ||
| Line 3,258: | Line 3,208: | ||
Burnable absorber content (quantity and distribution) is not stated as a design basis | Burnable absorber content (quantity and distribution) is not stated as a design basis | ||
other than as it relates to achieving a nonpositive MTC at power operating conditions, | other than as it relates to achieving a nonpositive MTC at power operating conditions, as discussed above. | ||
as discussed above. | |||
4.3.4.3 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations The reactor core and associated coolant, control, and protection systems are designed to assure that power oscillations which can result in conditions exceeding SAFDLs are not possible or can be reliably and readily detected and suppressed. | 4.3.4.3 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations The reactor core and associated coolant, control, and protection systems are designed to assure that power oscillations which can result in conditions exceeding SAFDLs are not possible or can be reliably and readily detected and suppressed. | ||
| Line 3,381: | Line 3,329: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-1 Revision 23 December 2016 4.4 THERMAL AND HYDRAULIC DESIGN This section discusses the thermal and hydraulic design of the DCPP reactors. | 2 FSAR UPDATE 4.4-1 Revision 23 December 2016 | ||
===4.4 THERMAL=== | |||
AND HYDRAULIC DESIGN This section discusses the thermal and hydraulic design of the DCPP reactors. | |||
The objective of the thermal and hydraulic design of the reactor core is to provide | The objective of the thermal and hydraulic design of the reactor core is to provide | ||
| Line 3,401: | Line 3,352: | ||
arising from Condition IV events. | arising from Condition IV events. | ||
Note that fuel damage as used here is defined as penetration of the fission product barrier (i.e., the fuel rod cladding). | Note that fuel damage as used here is defined as penetration of the fission product barrier (i.e., the fuel rod cladding). | ||
4.4.1 DESIGN BASES | |||
====4.4.1 DESIGN==== | |||
BASES | |||
4.4.1.1 General Design Criterion 10, 1971 - Reactor Design The reactor core is designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation or anticipated operational occurrences. | 4.4.1.1 General Design Criterion 10, 1971 - Reactor Design The reactor core is designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation or anticipated operational occurrences. | ||
| Line 3,408: | Line 3,361: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-2 Revision 23 December 2016 4.4.2 THERMAL AND HYDRAULIC DESIGN ACCEPTANCE CRITERIA 4.4.2.1 Departure from Nucleate Boiling Acceptance Criteria There will be at least a 95 percent probability that DNB will not occur on the limiting fuel rods during normal operation and operational transients and any transient conditions arising from faults of moderate frequency (Conditio ns I and II events) at a 95 percent confidence level. | 2 FSAR UPDATE 4.4-2 Revision 23 December 2016 | ||
====4.4.2 THERMAL==== | |||
AND HYDRAULIC DESIGN ACCEPTANCE CRITERIA 4.4.2.1 Departure from Nucleate Boiling Acceptance Criteria There will be at least a 95 percent probability that DNB will not occur on the limiting fuel rods during normal operation and operational transients and any transient conditions arising from faults of moderate frequency (Conditio ns I and II events) at a 95 percent confidence level. | |||
4.4.2.2 Fuel Temperature Acceptance Criteria During Condition I and Condition II events, the maximum fuel temperature shall be less than the melting temperature of UO | 4.4.2.2 Fuel Temperature Acceptance Criteria During Condition I and Condition II events, the maximum fuel temperature shall be less than the melting temperature of UO | ||
| Line 3,417: | Line 3,373: | ||
4.4.2.4 Hydrodynamic Stability Acceptance Criteria Modes of operation associated with Condition I and Condition II events shall not lead to hydrodynamic instability. | 4.4.2.4 Hydrodynamic Stability Acceptance Criteria Modes of operation associated with Condition I and Condition II events shall not lead to hydrodynamic instability. | ||
4.4.3 SYSTEM DESCRIPTION 4.4.3.1 Summary Comparison The core design parameters of the DCPP Unit 1 and Unit 2 reactors are presented in Table 4.1-1. | ====4.4.3 SYSTEM==== | ||
DESCRIPTION 4.4.3.1 Summary Comparison The core design parameters of the DCPP Unit 1 and Unit 2 reactors are presented in Table 4.1-1. | |||
The reactor core is designed to a minimum DNBR greater than or equal to the design | The reactor core is designed to a minimum DNBR greater than or equal to the design | ||
| Line 3,430: | Line 3,387: | ||
below the melting point of UO 2 (refer to Section 4.4.2.2). To preclude center melting and establish overpower protection system setpoints, a calculated centerline fuel DCPP UNITS 1 & | below the melting point of UO 2 (refer to Section 4.4.2.2). To preclude center melting and establish overpower protection system setpoints, a calculated centerline fuel DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-3 Revision 23 December 2016 temperature of 4700°F has been selected as the overpower limit. The temperature distribution within the fuel pellet is predomina ntly a function of the local power density and | 2 FSAR UPDATE 4.4-3 Revision 23 December 2016 temperature of 4700°F has been selected as the overpower limit. The temperature distribution within the fuel pellet is predomina ntly a function of the local power density and UO 2 thermal conductivity. However, the computation of radial fuel temperature distributions combines crud, oxide, cladding, gap, and pellet conductances. The factors | ||
that influence these conductances, such as gap size (or contact pressure), internal gas | that influence these conductances, such as gap size (or contact pressure), internal gas | ||
pressure, gas composition, pellet density, and radial power distribution within the pellet, | pressure, gas composition, pellet density, and radial power distribution within the pellet, etc., have been combined into a semiempirical thermal model (refer to Section 4.4.3.2.4) with modifications for time-dependent fuel densification (Reference 68). The temperature predictions have been compared to incore fuel | ||
etc., have been combined into a semiempirical thermal model (refer to Section 4.4.3.2.4) with modifications for time-dependent fuel densification (Reference 68). The temperature predictions have been compared to incore fuel | |||
temperature measurements (References 3 through 9) and melt radius data (References | temperature measurements (References 3 through 9) and melt radius data (References | ||
| Line 3,446: | Line 3,401: | ||
This affects the fuel temperatures in the following ways: | This affects the fuel temperatures in the following ways: | ||
(1) Pellet radial shrinkage increases the pellet diametral gap that results in increased thermal resistance of the gap and thus higher fuel temperatures | (1) Pellet radial shrinkage increases the pellet diametral gap that results in increased thermal resistance of the gap and thus higher fuel temperatures (refer to Section 4.2.1.2.2). | ||
(2) Pellet axial shrinkage may produce pellet-to-pellet gaps that result in local power spikes, described in Section 4.3.3.2.1, and thus higher total heat flux hot channel factor, F T Q and local fuel temperatures. However, studies have shown that this penalty can be eliminated for the fuel type present in the DCPP Unit 1 and Unit 2 cores (refer to Section 4.3.3.2.5). | |||
(refer to Section 4.2.1.2.2). | |||
(2) Pellet axial shrinkage may produce pellet-to-pellet gaps that result in local power spikes, described in Section 4.3.3.2.1, and thus higher total heat flux hot channel factor, F | |||
(3) Pellet axial shrinkage results in a fuel stack height reduction and an increase in the linear power generation rate (kW/ft) for a constant core | (3) Pellet axial shrinkage results in a fuel stack height reduction and an increase in the linear power generation rate (kW/ft) for a constant core | ||
| Line 3,460: | Line 3,413: | ||
determined throughout its lifetime considering time-dependent densification. Maximum fuel average and surface temperatures, shown in Figure 4.4-1 as a function of linear | determined throughout its lifetime considering time-dependent densification. Maximum fuel average and surface temperatures, shown in Figure 4.4-1 as a function of linear | ||
power density (kW/ft), are peak values attained during the fuel lifetime. Similarly, | power density (kW/ft), are peak values attained during the fuel lifetime. Similarly, Figure 4.4-2 presents the peak value of fuel centerline temperature versus linear power | ||
Figure 4.4-2 presents the peak value of fuel centerline temperature versus linear power | |||
density, attained during its lifetime. | density, attained during its lifetime. | ||
| Line 3,475: | Line 3,426: | ||
conductivity to melt, which can be determined with more certainty. From an | conductivity to melt, which can be determined with more certainty. From an | ||
examination of the data, it has been conclud ed that the best estimate for the value of | examination of the data, it has been conclud ed that the best estimate for the value of kdTC2800 0 o is 93 watts/cm. This conclusion is based on the integral values reported in References 10 and 24 through 28. | ||
The design curve for the thermal conductivity is shown in Figure 4.4-3. The section of the curve at temperatures between 0 and 1300°C is in excellent agreement with the | The design curve for the thermal conductivity is shown in Figure 4.4-3. The section of the curve at temperatures between 0 and 1300°C is in excellent agreement with the | ||
| Line 3,483: | Line 3,434: | ||
Thermal conductivity for UO 2 at 95 percent theoretical density can be represented best by the following equation: | Thermal conductivity for UO 2 at 95 percent theoretical density can be represented best by the following equation: | ||
() | ()313T10 8.775 0.0238T 11.8 1 kx++= (4.4-1) where: | ||
k is in watts/cm-°C, and T is in °C 4.4.3.2.3 Radial Power Distribution in UO 2 Fuel Rods An accurate radial power distribution as a function of burnup is needed to determine the | k is in watts/cm-°C, and T is in °C 4.4.3.2.3 Radial Power Distribution in UO 2 Fuel Rods An accurate radial power distribution as a function of burnup is needed to determine the | ||
power level for incipient fuel melting and other important performance parameters, | power level for incipient fuel melting and other important performance parameters, e.g., pellet thermal expansion, fuel swel ling, and fission gas release rates. | ||
This UO 2 fuel rods radial power distribution as a function of core burnup is determined using a 3D ANC calculation (refer to Sections 4.3.3.10.3 and 15.1.2.4) or with the neutron transport theory LASER (Reference 81) code that has been validated by | |||
This | |||
comparing code predictions on radial burnup and isotopic distributions with measured | comparing code predictions on radial burnup and isotopic distributions with measured | ||
| Line 3,522: | Line 3,471: | ||
core thermal output. Figure 4.4-4 shows the axial variation of average cladding temperature for a representative average power rod both at BOL and EOL. | core thermal output. Figure 4.4-4 shows the axial variation of average cladding temperature for a representative average power rod both at BOL and EOL. | ||
4.4.3.2.7 Treatment of Peaking Factors The total heat flux hot channel factor, F | 4.4.3.2.7 Treatment of Peaking Factors The total heat flux hot channel factor, F T Q , is defined by the ratio of the maximum to core average heat flux. The design value of F T Q for normal operation is 2.58, allowing for fuel densification effects, as shown in Table 4.3-1. This results in a peak local linear power density of 14.3 kW/ft at full power. The corresponding peak local power at the maximum overpower trip point (118 percent total power) is 16.6 kW/ft. Centerline | ||
temperature at this kW/ft must be below the UO 2 melt temperature over the lifetime of the rod including allowances for uncertainties | temperature at this kW/ft must be below the UO 2 melt temperature over the lifetime of the rod including allowances for uncertainties. From Figure 4.4-2, the centerline temperature at the maximum overpower trip point is well below that required to produce melting. Fuel centerline and average temperature at rated (100 percent) power and at | ||
. From Figure 4.4-2, the centerline temperature at the maximum overpower trip point is well below that required to produce melting. Fuel centerline and average temperature at rated (100 percent) power and at | |||
the maximum overpower trip point for Unit 1 and Unit 2 are presented in Table 4.1-1. | the maximum overpower trip point for Unit 1 and Unit 2 are presented in Table 4.1-1. | ||
| Line 3,547: | Line 3,495: | ||
In several cases, the W-3 DNB correlation is used where the WRB-2 is not applicable. | In several cases, the W-3 DNB correlation is used where the WRB-2 is not applicable. | ||
For example, Section 15.2.14.1 uses the W-3 DNB correlation since the system pressure for the limiting statepoint is below 1,000 psia. | For example, Section 15.2.14.1 uses the W-3 DNB correlation since the system pressure for the limiting statepoint is below 1,000 psia. | ||
The W-3 DNB correlation, and several modifications, have been used in Westinghouse CHF calculations. The W-3 DNB was origin ally developed from single tube data (Reference 34), but was subsequently modified to apply to the 0.422 inch, OD rod low parasitic reinforced grid (R-grid) (References 35 and 92) and low parasitic grid (L-grid) | The W-3 DNB correlation, and several modifications, have been used in Westinghouse CHF calculations. The W-3 DNB was origin ally developed from single tube data (Reference 34), but was subsequently modified to apply to the 0.422 inch, OD rod low parasitic reinforced grid (R-grid) (References 35 and 92) and low parasitic grid (L-grid) (Reference 36), as well as the 0.374 inch OD (References 37 and 38) rod bundle data. | ||
(Reference 36), as well as the 0.374 inch OD (References 37 and 38) rod bundle data. | |||
These modifications to the W-3 DNB correlation have been demonstrated to be adequate for reactor rod bundle design. | These modifications to the W-3 DNB correlation have been demonstrated to be adequate for reactor rod bundle design. | ||
| Line 3,574: | Line 3,521: | ||
CHF tests which model the 17x17 optimized fuel assembly have been performed with the results described in detail in Reference 87. It was concluded that the CHF | CHF tests which model the 17x17 optimized fuel assembly have been performed with the results described in detail in Reference 87. It was concluded that the CHF | ||
characteristics of the 17x17 optimized fuel asse mbly design are not significantly different from those of 17x17 LOPAR design, and can be adequately described by the | characteristics of the 17x17 optimized fuel asse mbly design are not significantly different from those of 17x17 LOPAR design, and can be adequately described by the "R" grid form of the WRB-1 CHF correlation. Furthermore, the new data can be | ||
"R" grid form of the WRB-1 CHF correlation. Furthermore, the new data can be | |||
incorporated into the "R" grid data base such that the WRB-1 correlation can be applied | incorporated into the "R" grid data base such that the WRB-1 correlation can be applied | ||
| Line 3,582: | Line 3,527: | ||
to 17x17 LOPAR fuel design without changi ng the DNBR design criterion of 1.17. | to 17x17 LOPAR fuel design without changi ng the DNBR design criterion of 1.17. | ||
4.4.3.3.2 Definition of Departure from Nucleate Boiling Ratio The DNBR, as applied to this design for both typical and thimble cold wall cells is: | 4.4.3.3.2 Definition of Departure from Nucleate Boiling Ratio The DNBR, as applied to this design for both typical and thimble cold wall cells is: | ||
"actual"Predicted DNB, | " actual"Predicted DNB, q q DNBR= (4.4-5) For the W-3 DNB (R-Grid) correlation, FFq'""S3WEU, Predicted DNB, qx= (4.4-6) when all flow cell walls are heated and q" EU, W-3 is the uniform DNB heat flux as predicted by W-3 DNB correlation and F is the flux shape factor which accounts for non-uniform axial heat flux distributions (Reference 39) with the "C" term modified as in | ||
Reference 34. | Reference 34. | ||
| Line 3,590: | Line 3,535: | ||
TDC increase as axial grid spacing is decreased (References 35 and 40). | TDC increase as axial grid spacing is decreased (References 35 and 40). | ||
When a cold wall is present for the W-3 DNB correlation, | When a cold wall is present for the W-3 DNB correlation, 'F" q" q SCW3,WEU, Predicted DNB,x= (4.4-7) | ||
'F"q" | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-8 Revision 23 December 2016 where: | 2 FSAR UPDATE 4.4-8 Revision 23 December 2016 where: CWF F" q" qDh3,WEU,CW3,WEU,x= (4.4-7A) | ||
"Dh3,WEU,q is the uniform DNB heat flux as predicted by the W-3 DNB cold wall correlation (Reference 34) when not all flow cell walls are heated (thimble cold wall cell). | "Dh3,WEU, q is the uniform DNB heat flux as predicted by the W-3 DNB cold wall correlation (Reference 34) when not all flow cell walls are heated (thimble cold wall cell). | ||
The cold wall factor (CWF) is provided in References 34 and 39. For the WRB-2 correlation, | The cold wall factor (CWF) is provided in References 34 and 39. For the WRB-2 correlation, F q" q"2WRB Predicted DNB,= (4.4-8) | ||
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | ||
F q"1WRB Predicted DNB," q= for WRB1 correlation | |||
where: | where: | ||
| Line 3,662: | Line 3,606: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-10 Revision 23 December 2016 4.4.3.3.4.1 Heat Flux Engineering Hot Channel Factor, | 2 FSAR UPDATE 4.4-10 Revision 23 December 2016 4.4.3.3.4.1 Heat Flux Engineering Hot Channel Factor, F E Q The heat flux engineering hot channel factor is used to evaluate the maximum heat flux. | ||
This subfactor is determined by statistically combinin g the tolerances for the fuel pellet diameter, density, enrichment, eccentricity, and the fuel rod diameter, and has a value | This subfactor is determined by statistically combinin g the tolerances for the fuel pellet diameter, density, enrichment, eccentricity, and the fuel rod diameter, and has a value | ||
| Line 3,676: | Line 3,620: | ||
4.4.3.3.4.2 Enthalpy Rise Engineering Hot Channel Factor, F E The effect of variations in flow conditions and fabrication tolerances on the hot channel | 4.4.3.3.4.2 Enthalpy Rise Engineering Hot Channel Factor, F E The effect of variations in flow conditions and fabrication tolerances on the hot channel | ||
enthalpy rise is directly considered in the THINC core thermal subchannel analysis | enthalpy rise is directly considered in the THINC core thermal subchannel analysis (refer to Section 4.4.3.15.1) under any reacto r operating condition. The following items contribute to the enthalpy rise engineering hot channel factor: | ||
(refer to Section 4.4.3.15.1) under any reacto r operating condition. The following items contribute to the enthalpy rise engineering hot channel factor: | |||
(1) Pellet Diameter, Density and Enrichment, Fuel Rod Diameter, Pitch, and Bowing Design values employed in the THINC analysis are based on applicable limiting tolerances such that design values are met for 95 percent of the | (1) Pellet Diameter, Density and Enrichment, Fuel Rod Diameter, Pitch, and Bowing Design values employed in the THINC analysis are based on applicable limiting tolerances such that design values are met for 95 percent of the | ||
| Line 3,719: | Line 3,661: | ||
fuel assembly analysis utilizing the WRB-2 correlation. | fuel assembly analysis utilizing the WRB-2 correlation. | ||
However, for the upper assembly span of VANTAGE+ fuel where additional restraint is provided with the IFM grids, the grid-to-grid s pacing in DNB limiting span is approximately 10 inches . Using the rod bow topical report methods (Reference 79), | However, for the upper assembly span of VANTAGE+ fuel where additional restraint is provided with the IFM grids, the grid-to-grid s pacing in DNB limiting span is approximately 10 inches . Using the rod bow topical report methods (Reference 79), and scaling with the NRC approved factor results in predicted channel closure in the limiting spans of less than 50 percent closure; no rod bow DNBR penalty is required in the 10 inch spans in the VANTAGE+ safety analyses. | ||
and scaling with the NRC approved factor results in predicted channel closure in the limiting spans of less than 50 percent closure; no rod bow DNBR penalty is required in the 10 inch spans in the VANTAGE+ safety analyses. | |||
VANTAGE+ Design Limit Typical Cell 1.34 Thimble Cell 1.32 | VANTAGE+ Design Limit Typical Cell 1.34 Thimble Cell 1.32 | ||
| Line 3,728: | Line 3,669: | ||
on an assembly average burnup of 24,000 MWD/MTU based on Reference 100. At burnups greater than 24,000 MWD/MTU, credit is taken for the effect of F N burndown. | on an assembly average burnup of 24,000 MWD/MTU based on Reference 100. At burnups greater than 24,000 MWD/MTU, credit is taken for the effect of F N burndown. | ||
Due to the decrease in fissionable isotopes and the buildup of fission product inventory, | Due to the decrease in fissionable isotopes and the buildup of fission product inventory, no additional rod bow penalty is required. | ||
no additional rod bow penalty is required. | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
| Line 3,768: | Line 3,707: | ||
of the power distribution measurements, the quadrant power tilt alarms and related | of the power distribution measurements, the quadrant power tilt alarms and related | ||
instrumentation are adjusted to indicate zero quadrant tilt, 1.00 quadrant power tilt ratio, | instrumentation are adjusted to indicate zero quadrant tilt, 1.00 quadrant power tilt ratio, as the final step in the calibration process. Proper functioning of the quadrant power tilt | ||
as the final step in the calibration process. Proper functioning of the quadrant power tilt | |||
alarm is significant because no allowances are made in the design for increased hot | alarm is significant because no allowances are made in the design for increased hot | ||
| Line 3,792: | Line 3,729: | ||
4.4.3.6 Core Coolant Flow Distribution Coolant enthalpy rise and flow distributions are shown for the 4-foot elevation | 4.4.3.6 Core Coolant Flow Distribution Coolant enthalpy rise and flow distributions are shown for the 4-foot elevation | ||
(1/3 of core height) in Figure 4.4-7, 8-foot elevation (2/3 of core height) in Figure 4.4-8, | (1/3 of core height) in Figure 4.4-7, 8-foot elevation (2/3 of core height) in Figure 4.4-8, and at the core exit in Figure 4.4-9. These distributions correspond to a representative | ||
and at the core exit in Figure 4.4-9. These distributions correspond to a representative | |||
Westinghouse 4-loop plant. The THINC code analysis for this case utilized a uniform | Westinghouse 4-loop plant. The THINC code analysis for this case utilized a uniform | ||
| Line 3,804: | Line 3,739: | ||
4.4.3.7.1 Core Pressure Drops The analytical model and experimental data used to calculate the pressure drops, for | 4.4.3.7.1 Core Pressure Drops The analytical model and experimental data used to calculate the pressure drops, for | ||
the full power conditions given in Table 4.1-1 | the full power conditions given in Table 4.1-1 , are described in Section 4.4.3.8.2. The core pressure drop consists of the fuel assembly, lower core plate, and upper core plate | ||
, are described in Section 4.4.3.8.2. The core pressure drop consists of the fuel assembly, lower core plate, and upper core plate | |||
pressure drops. These pressure drops are based on the best estimate flow, as | pressure drops. These pressure drops are based on the best estimate flow, as | ||
| Line 3,834: | Line 3,768: | ||
correlation (Reference 49), with the properties evaluated at bulk fluid conditions: | correlation (Reference 49), with the properties evaluated at bulk fluid conditions: | ||
0. | 0.4 kµp C 0.8 G e D 0.023 k e hD=µ (4.4-10) where: | ||
h = heat transfer coefficient, Btu/hr-ft 2-°F | h = heat transfer coefficient, Btu/hr-ft 2-°F D e = equivalent diameter, ft k = thermal conductivity, Btu/hr-ft-°F G = mass velocity, lbm/hr-ft 2 µ = dynamic viscosity, lbm/ft-hr Cp = heat capacity, Btu/lbm-°F | ||
This correlation has been shown to be conservative (Reference 50) for rod bundle | This correlation has been shown to be conservative (Reference 50) for rod bundle | ||
| Line 3,846: | Line 3,780: | ||
: 51) correlation. After this occurrence, the outer cladding wall temperature is determined by: | : 51) correlation. After this occurrence, the outer cladding wall temperature is determined by: | ||
T sat = [0.072 exp (-P/1260)] (q") | |||
0.5 (4.4-11) where: | 0.5 (4.4-11) where: | ||
TSAT = wall superheat, T w - Tsat, °F q" = wall heat flux, Btu/hr-ft 2 P = pressure, psia | TSAT = wall superheat, T w - Tsat , °F q" = wall heat flux, Btu/hr-ft 2 P = pressure, psia | ||
single-phase water. Two-phase consideratio ns are neglected in the vessel pressure DCPP UNITS 1 & | T w = outer cladding wall temperature, °F T SAT = saturation temperature of coolant at P, °F 4.4.3.8.2 Total Core and Vessel Pressure Drop Pressure losses occur as a result of viscous drag (friction) and/or geometry changes (form) in the fluid flowpath. The flow field is assumed to be incompressible, turbulent, single-phase water. Two-phase consideratio ns are neglected in the vessel pressure DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-15 Revision 23 December 2016 drop evaluation because the core average void is negligible (refer to Section 4.4.3.5 and Tables 4.4-1 and 4.4-2). | 2 FSAR UPDATE 4.4-15 Revision 23 December 2016 drop evaluation because the core average void is negligible (refer to Section 4.4.3.5 and Tables 4.4-1 and 4.4-2). | ||
Two-phase flow considerations in the core thermal subchannel analyses are considered and the models are discussed in Section 4.4.3.12.3. Core and vessel pressure losses are calculated by equations of the form: | Two-phase flow considerations in the core thermal subchannel analyses are considered and the models are discussed in Section 4.4.3.12.3. Core and vessel pressure losses are calculated by equations of the form: | ||
(144) | (144)c 2g 2 e D FL K L+= (4.4-12) where: P L = pressure drop, lb f/in 2 = fluid density, lbm/ft 3 L = length, ft D e = equivalent diameter, ft V = fluid velocity, ft/sec g c = 2 sec f 1b ft m 1b 32.174 K = form loss coefficient, dimensionless F = friction loss coefficient, dimensionless | ||
Fluid density is assumed to be constant at an appropriate value for each component in | Fluid density is assumed to be constant at an appropriate value for each component in | ||
| Line 3,863: | Line 3,795: | ||
the core and vessel. Because of the complex core and vessel flow geometry, precise | the core and vessel. Because of the complex core and vessel flow geometry, precise | ||
analytical values for the form and friction loss coefficients are not available. Therefore, | analytical values for the form and friction loss coefficients are not available. Therefore, experimental values for these coefficients are obtained from geometrically similar | ||
experimental values for these coefficients are obtained from geometrically similar | |||
models. | models. | ||
| Line 3,883: | Line 3,813: | ||
Figure 4.4-10. They are the wall void region (no bubble detachment), the subcooled | Figure 4.4-10. They are the wall void region (no bubble detachment), the subcooled | ||
boiling region (bubble detachment), | boiling region (bubble detachment), and the bulk boiling region. | ||
and the bulk boiling region. | |||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
| Line 3,971: | Line 3,900: | ||
the best estimate loop flow (by approximately 4 percent). In addition, another | the best estimate loop flow (by approximately 4 percent). In addition, another | ||
7.5 percent (Unit 1) and 9.0 percent (Unit 2) of the thermal design flow is assumed to be ineffective for core heat removal capability because it bypasses the core through the | ===7.5 percent=== | ||
(Unit 1) and 9.0 percent (Unit 2) of the thermal design flow is assumed to be ineffective for core heat removal capability because it bypasses the core through the | |||
various available flowpaths described in Section 4.4.3.12.1. | various available flowpaths described in Section 4.4.3.12.1. | ||
| Line 3,995: | Line 3,925: | ||
(4) The height of fluid in each component of the RCS may be determined from the physical data and data provided in Table 5.1-1. The RCS components are water-filled during power operation with the pressurizer being approximately 60 percent water-filled. | (4) The height of fluid in each component of the RCS may be determined from the physical data and data provided in Table 5.1-1. The RCS components are water-filled during power operation with the pressurizer being approximately 60 percent water-filled. | ||
(5) ECCS components are located to meet the criteria for net positive suction head described in Section 6.3. | (5) ECCS components are located to meet the criteria for net positive suction head described in Section 6.3. | ||
(6) Line lengths and sizes for the safety injection system are determined so as to guarantee a total system resistance that will provide, as a minimum, | (6) Line lengths and sizes for the safety injection system are determined so as to guarantee a total system resistance that will provide, as a minimum, the fluid delivery rates assumed in the safety analyses described in Chapter 15. | ||
(7) The design data for RCS components, including volumes (diameter), flows, and pressure and temperature, are presented in Section 5.5. | |||
the fluid delivery rates assumed in the safety analyses described in Chapter 15. | |||
(7) The design data for RCS components, including volumes (diameter), | |||
flows, and pressure and temperature, are presented in Section 5.5. | |||
(8) RCS steady state pressure and temperature distribution are presented in Table 5.1-1. | (8) RCS steady state pressure and temperature distribution are presented in Table 5.1-1. | ||
4.4.3.12 Core Hydraulics | 4.4.3.12 Core Hydraulics | ||
| Line 4,010: | Line 3,937: | ||
2 FSAR UPDATE 4.4-20 Revision 23 December 2016 The above contributions are evaluated to confirm that the design basis value of | 2 FSAR UPDATE 4.4-20 Revision 23 December 2016 The above contributions are evaluated to confirm that the design basis value of | ||
7.5 percent (Unit 1) and 9.0 percent (Unit 2) core bypass flow is met. | ===7.5 percent=== | ||
(Unit 1) and 9.0 percent (Unit 2) core bypass flow is met. | |||
4.4.3.12.2 Inlet Flow Distribution Data from several 1/7 scale hydraulic reactor model tests (References 52, 53, and 60) | 4.4.3.12.2 Inlet Flow Distribution Data from several 1/7 scale hydraulic reactor model tests (References 52, 53, and 60) | ||
| Line 4,030: | Line 3,958: | ||
inlet velocity distribution with reduced flowrate. | inlet velocity distribution with reduced flowrate. | ||
4.4.3.12.3 Empirical Friction Factor Correlations, F | 4.4.3.12.3 Empirical Friction Factor Correlations, F E Q Two empirical friction factor correlations are used in the THINC-IV computer code (refer to Section 4.4.3.15.1). | ||
The friction factor in the axial direction, parallel to the fuel rod axis, uses the | The friction factor in the axial direction, parallel to the fuel rod axis, uses the | ||
| Line 4,050: | Line 3,978: | ||
large tube bank. Thus, the lateral friction factor proposed by Idel'chik (Reference 54) is applicable. This correlation is of the form: | large tube bank. Thus, the lateral friction factor proposed by Idel'chik (Reference 54) is applicable. This correlation is of the form: | ||
0. | 0.2ReAF L L= (4.4-13) | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-21 Revision 23 December 2016 where: A is a function of the rod pitch and diameter as given in Reference 54 | 2 FSAR UPDATE 4.4-21 Revision 23 December 2016 where: A is a function of the rod pitch and diameter as given in Reference 54 | ||
Re L is the lateral Reynolds number based on rod diameter | |||
Extensive comparisons of THINC-IV predictions using these correlations to | Extensive comparisons of THINC-IV predictions using these correlations to | ||
| Line 4,061: | Line 3,988: | ||
experimental data are given in Reference 59, and verify the applicability of these correlations in PWR design. | experimental data are given in Reference 59, and verify the applicability of these correlations in PWR design. | ||
4.4.3.13 Influence of Power Distribution The core power distribution, which at BOL is largely established by fuel enrichment, | 4.4.3.13 Influence of Power Distribution The core power distribution, which at BOL is largely established by fuel enrichment, loading pattern, and core power level, is also a function of variables such as control rod worth and position and fuel depletion throughout lifetime. Although radial power | ||
loading pattern, and core power level, is also a function of variables such as control rod worth and position and fuel depletion throughout lifetime. Although radial power | |||
distributions in various planes of the core are often illustrated for general interest, the | distributions in various planes of the core are often illustrated for general interest, the | ||
| Line 4,069: | Line 3,994: | ||
core radial enthalpy rise distribution, as determined by the integral of power over each | core radial enthalpy rise distribution, as determined by the integral of power over each | ||
channel, is of greater importance for DNB analyses. These radial power distributions, characterized by | channel, is of greater importance for DNB analyses. These radial power distributions, characterized by F N (defined in Section 4.3.3.2.2), as well as axial heat flux profiles, are discussed in the following two sections. | ||
4.4.3.13.1 Nuclear Enthalpy Rise Hot Channel Factor, F N Given the local power density q' (kW/ft) at a point x, y, z in a core with N fuel rods and | 4.4.3.13.1 Nuclear Enthalpy Rise Hot Channel Factor, F N Given the local power density q' (kW/ft) at a point x, y, z in a core with N fuel rods and | ||
height H: | height H: | ||
()dzz)y,(x,q' | ()dzz)y,(x,q' N ldzz,y,xq'Maxpower rod averagepower rod hot H o rods alloo H o N F== (4.4-14) | ||
The location of minimum DNBR depends on the axial profile and its magnitude depends on the enthalpy rise up to that point. The maximum value of the rod integral is used to identify the most likely rod for minimum DNBR. An axial power profile is obtained which, when normalized to the design value of F N, recreates the axial heat flux along the limiting rod. The surrounding rods are assumed to have the same axial profile with rod average powers that are typical of distributions found in hot assemblies. In this | The location of minimum DNBR depends on the axial profile and its magnitude depends on the enthalpy rise up to that point. The maximum value of the rod integral is used to identify the most likely rod for minimum DNBR. An axial power profile is obtained which, when normalized to the design value of F N , recreates the axial heat flux along the limiting rod. The surrounding rods are assumed to have the same axial profile with rod average powers that are typical of distributions found in hot assemblies. In this | ||
manner, worst case axial profiles can be combined with worst case radial distributions | manner, worst case axial profiles can be combined with worst case radial distributions | ||
| Line 4,089: | Line 4,014: | ||
For operation at a fraction P of full power, the design F N is given by: | For operation at a fraction P of full power, the design F N is given by: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-22 Revision 23 December 2016 | 2 FSAR UPDATE 4.4-22 Revision 23 December 2016 F N = 1.59 [1 + 0.3 (1-P)] (VANTAGE+) (4.4-15) | ||
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | ||
F N = 1.56 [1 + 0.3 (1-P)] (LOPAR) | |||
The permitted relaxation of F N is included in the DNB protection setpoints and allows radial power shape changes with rod insertion to the insertion limits (Reference 64), | The permitted relaxation of F N is included in the DNB protection setpoints and allows radial power shape changes with rod insertion to the insertion limits (Reference 64), thus allowing greater flexib ility in the nuclear design. | ||
thus allowing greater flexib ility in the nuclear design. | |||
4.4.3.13.2 Axial Heat Flux Distributions As discussed in Section 4.3.3.2, the axial he at flux distribution can vary as a result of rod motion, power change, or due to spatial xenon transients that may occur in the axial | 4.4.3.13.2 Axial Heat Flux Distributions As discussed in Section 4.3.3.2, the axial he at flux distribution can vary as a result of rod motion, power change, or due to spatial xenon transients that may occur in the axial | ||
| Line 4,102: | Line 4,026: | ||
axial shape. | axial shape. | ||
The reference DNB design axial shape is a chopped cosine with a peak-to-average ratio of 1.55. | The reference DNB design axial shape is a chopped cosine with a peak-to-average ratio of 1.55. | ||
4.4.3.14 Core Thermal Response A general summary of the steady state the rmal-hydraulic design parameters including thermal output, flowrates, etc., is provided in Table 4.1-1. As stated in Section 4.4.2, the acceptance criteria are to prevent DNB and to prevent fuel melting for Conditions I and II events. The protective systems described in Chapter 7 (Instrumentation and Controls) are designed to meet these bases. The response of the core to Condition II | 4.4.3.14 Core Thermal Response A general summary of the steady state the rmal-hydraulic design parameters including thermal output, flowrates, etc., is provided in Table 4.1-1. As stated in Section 4.4.2, the acceptance criteria are to prevent DNB and to prevent fuel melting for Conditions I and II events. The protective systems described in Chapter 7 (Instrumentation and Controls) are designed to meet these bases. The response of the core to Condition II | ||
| Line 4,132: | Line 4,055: | ||
design evaluation. | design evaluation. | ||
4.4.3.15.1.1 Steady State Analysis The THINC-IV computer program determines coolant density, mass velocity, enthalpy, | 4.4.3.15.1.1 Steady State Analysis The THINC-IV computer program determines coolant density, mass velocity, enthalpy, vapor void, static pressure, and DNBR distributions al ong parallel flow channels within a reactor core under all expected operating conditions. The core region being studied is | ||
vapor void, static pressure, and DNBR distributions al ong parallel flow channels within a reactor core under all expected operating conditions. The core region being studied is | |||
made up of a number of contiguous elements in a rectangular array extending the full | made up of a number of contiguous elements in a rectangular array extending the full | ||
| Line 4,209: | Line 4,130: | ||
gaining flow, thereby creating significant inte r-assembly cross flow. Tests with significant cross flow are of more value in code verification. | gaining flow, thereby creating significant inte r-assembly cross flow. Tests with significant cross flow are of more value in code verification. | ||
Inter-assembly cross flow is caused by radial variations in pressure that are caused in turn by variations in the axial pressure drops in different assemblies. Under normal operating conditions (subcooled forced convection), | Inter-assembly cross flow is caused by radial variations in pressure that are caused in turn by variations in the axial pressure drops in different assemblies. Under normal operating conditions (subcooled forced convection), the axial pressure drop is due mainly to friction losses. Because all assemblies have the same geometry, all | ||
the axial pressure drop is due mainly to friction losses. Because all assemblies have the same geometry, all | |||
assemblies have nearly the same axial pressure drops, and cross flow velocities are | assemblies have nearly the same axial pressure drops, and cross flow velocities are | ||
| Line 4,246: | Line 4,166: | ||
The predicted assembly exit temperatures were compared with the measured exit | The predicted assembly exit temperatures were compared with the measured exit | ||
temperatures for each data run. The standa rd deviations of the measured and predicted assembly exit temperatures are compared for both THINC-IV and THINC-I, | temperatures for each data run. The standa rd deviations of the measured and predicted assembly exit temperatures are compared for both THINC-IV and THINC-I, and are given in Table 4.4-3. THI NC-IV generally fits the data somewhat more accurately than THINC-I. Both codes are conservative and predict exit temperatures | ||
and are given in Table 4.4-3. THI NC-IV generally fits the data somewhat more accurately than THINC-I. Both codes are conservative and predict exit temperatures | |||
higher than measured values for the high-powered assemblies. Experimental verification of the THINC-IV subchannel calculation has been obtained from exit | higher than measured values for the high-powered assemblies. Experimental verification of the THINC-IV subchannel calculation has been obtained from exit | ||
| Line 4,301: | Line 4,219: | ||
the modifications for the time-dependent densification given in Reference 68. | the modifications for the time-dependent densification given in Reference 68. | ||
4.4.3.16 Hydrodynamic and Flow-Power Coupled Instability Boiling flow may be susceptible to thermohydrodynamic instabilities (Reference 69). | 4.4.3.16 Hydrodynamic and Flow-Power Coupled Instability Boiling flow may be susceptible to thermohydrodynamic instabilities (Reference 69). | ||
These instabilities may cause a change in th ermo-hydraulic conditions that may lead to a reduction in the DNB heat flux relative to that observed during a steady flow condition, | These instabilities may cause a change in th ermo-hydraulic conditions that may lead to a reduction in the DNB heat flux relative to that observed during a steady flow condition, or to undesired forced vibrations of core components. Thus, the thermo-hydraulic design criterion states that operation during Condition I and Condition II events shall not lead to thermohydrodynamic instabilities. | ||
or to undesired forced vibrations of core components. Thus, the thermo-hydraulic design criterion states that operation during Condition I and Condition II events shall not lead to thermohydrodynamic instabilities. | |||
Two specific types of flow instabilities are considered by Westinghouse for PWR | Two specific types of flow instabilities are considered by Westinghouse for PWR | ||
| Line 4,310: | Line 4,226: | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-27 Revision 23 December 2016 A Ledinegg instability involves a sudden change in flowrate from one steady state to another. This instability occurs (Reference 69) when the slope of the RCS pressure drop-flowrate curve becomes algebraically smaller than the slope of the loop supply | 2 FSAR UPDATE 4.4-27 Revision 23 December 2016 A Ledinegg instability involves a sudden change in flowrate from one steady state to another. This instability occurs (Reference 69) when the slope of the RCS pressure drop-flowrate curve becomes algebraically smaller than the slope of the loop supply (pump head) pressure drop-flowrate curve. The Westinghouse pump head curve has a | ||
(pump head) pressure drop-flowrate curve. The Westinghouse pump head curve has a | |||
negative slope whereas the RCS pressure drop-flow curve has a positive slope over the | negative slope whereas the RCS pressure drop-flow curve has a positive slope over the | ||
| Line 4,353: | Line 4,267: | ||
are required for fuel failure. Normal operational transients are limited to about 40 cal/gm-min. (peak rod) while the Spert tests (Reference 76) indicate that 120 to 150 cal/gm is required to rupture the clad even wit h very short transients (5.5 msec. period). | are required for fuel failure. Normal operational transients are limited to about 40 cal/gm-min. (peak rod) while the Spert tests (Reference 76) indicate that 120 to 150 cal/gm is required to rupture the clad even wit h very short transients (5.5 msec. period). | ||
Release of the internal fuel rod pressure is expected to have a minimal effect on the DCPP UNITS 1 & | Release of the internal fuel rod pressure is expected to have a minimal effect on the DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-28 Revision 23 December 2016 RCS (Reference 76) and is not expected to result in failure of additional fuel rods (Reference 77). Ejection of fuel pellet fragments into the coolant stream is not expected | 2 FSAR UPDATE 4.4-28 Revision 23 December 2016 RCS (Reference 76) and is not expected to result in failure of additional fuel rods (Reference 77). Ejection of fuel pellet fragments into the coolant stream is not expected (References 76 and 77). A cladding breach due to waterlogging is thus expected to be similar to any fuel rod failure mechanism that exposes fuel pellets to the reactor coolant | ||
(References 76 and 77). A cladding breach due to waterlogging is thus expected to be similar to any fuel rod failure mechanism that exposes fuel pellets to the reactor coolant | |||
stream. Waterlogging has not been identified as the mechanism for cladding distortion | stream. Waterlogging has not been identified as the mechanism for cladding distortion | ||
| Line 4,417: | Line 4,329: | ||
of the relatively good film boiling heat transfer following DNB, the energy release from this reaction is insignificant compared to the power produced by the fuel. | of the relatively good film boiling heat transfer following DNB, the energy release from this reaction is insignificant compared to the power produced by the fuel. | ||
These results have been confirmed in DNB tests conducted by Westinghouse | These results have been confirmed in DNB tests conducted by Westinghouse (References 66 and 78). | ||
(References 66 and 78). | |||
4.4.3.20 Energy Release During Rupture of Waterlogged Fuel Elements | 4.4.3.20 Energy Release During Rupture of Waterlogged Fuel Elements | ||
| Line 4,467: | Line 4,377: | ||
turbulent pressure fluctuations. Fuel rod wear due to flow-induced vibration is | turbulent pressure fluctuations. Fuel rod wear due to flow-induced vibration is | ||
considered in the fuel rod fretting evaluati on (refer to Section 4.2.1.3.2.7). | considered in the fuel rod fretting evaluati on (refer to Section 4.2.1.3.2.7). | ||
4.4.4 THERMAL AND HYDRAULIC DESIGN EVALUATION 4.4.4.1 Departure from Nucleate Boiling DNB will not occur on at least 95 percent of the limiting fuel rods during normal operation and operational transients and any transient conditions arising from faults of moderate frequency (Condition I and Conditio n II events) at a 95 percent confidence level. | |||
====4.4.4 THERMAL==== | |||
AND HYDRAULIC DESIGN EVALUATION 4.4.4.1 Departure from Nucleate Boiling DNB will not occur on at least 95 percent of the limiting fuel rods during normal operation and operational transients and any transient conditions arising from faults of moderate frequency (Condition I and Conditio n II events) at a 95 percent confidence level. | |||
This criterion has been conservatively met by adhering to the following thermal design | This criterion has been conservatively met by adhering to the following thermal design | ||
| Line 4,540: | Line 4,452: | ||
4.4.4.4 Hydrodynamic Stability Operation during Condition I and Condition II events shall not lead to hydrodynamic instability. | 4.4.4.4 Hydrodynamic Stability Operation during Condition I and Condition II events shall not lead to hydrodynamic instability. | ||
4.4.5 SAFETY EVALUATION 4.4.5.1 General Design Criterion 10, 1971 - Reactor Design The preceding evaluations show that the SAFDLs are not exceeded during any condition of normal operation or anticipated operational occurrence. Specifically: | ====4.4.5 SAFETY==== | ||
EVALUATION 4.4.5.1 General Design Criterion 10, 1971 - Reactor Design The preceding evaluations show that the SAFDLs are not exceeded during any condition of normal operation or anticipated operational occurrence. Specifically: | |||
* Section 4.4.4.1 shows that the DNB limits are not exceeded; | * Section 4.4.4.1 shows that the DNB limits are not exceeded; | ||
* Section 4.4.4.2 shows that the maximum fuel temperature limits are not exceeded; and | * Section 4.4.4.2 shows that the maximum fuel temperature limits are not exceeded; and | ||
| Line 4,551: | Line 4,464: | ||
4.4.5.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations Thermo-hydrodynamic instabilities (i.e., oscillations) will not occur under Condition I and Condition II events for DCPP. A large power margin exists to predicted inception of DCPP UNITS 1 & | 4.4.5.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations Thermo-hydrodynamic instabilities (i.e., oscillations) will not occur under Condition I and Condition II events for DCPP. A large power margin exists to predicted inception of DCPP UNITS 1 & | ||
2 FSAR UPDATE 4.4-33 Revision 23 December 2016 such instabilities. Analyses have been performed and show that in Westinghouse reactor designs, parameters such as fuel assembly arrays, core power flow ratios, fuel assembly length, etc., do not result in gross deterioration of the above power margins (refer to Section 4.4.3.16). | 2 FSAR UPDATE 4.4-33 Revision 23 December 2016 such instabilities. Analyses have been performed and show that in Westinghouse reactor designs, parameters such as fuel assembly arrays, core power flow ratios, fuel assembly length, etc., do not result in gross deterioration of the above power margins (refer to Section 4.4.3.16). | ||
4.4.6 TESTS AND INSPECTIONS 4.4.6.1 Testing Prior to Initial Criticality Reactor coolant flow tests, as noted in Tests 3.9 and 3.10 of Table 14.1-2, are | |||
====4.4.6 TESTS==== | |||
AND INSPECTIONS 4.4.6.1 Testing Prior to Initial Criticality Reactor coolant flow tests, as noted in Tests 3.9 and 3.10 of Table 14.1-2, are | |||
performed following fuel loading, but prior to initial criticality. Coolant loop pressure drop data are obtained in this test. These data, in conjunction with coolant pump | performed following fuel loading, but prior to initial criticality. Coolant loop pressure drop data are obtained in this test. These data, in conjunction with coolant pump | ||
| Line 4,565: | Line 4,480: | ||
4.4.6.3 Component and Fuel Inspections Inspections performed on the manufactured fuel are delineated in Section 4.2.1.6. | 4.4.6.3 Component and Fuel Inspections Inspections performed on the manufactured fuel are delineated in Section 4.2.1.6. | ||
Fabrication measurements critical to thermal and hydraulic analysis are obtained to verify that the engineering hot channel factors employed in the design analyses (refer to Section 4.4.3.3.4) are met. | Fabrication measurements critical to thermal and hydraulic analysis are obtained to verify that the engineering hot channel factors employed in the design analyses (refer to Section 4.4.3.3.4) are met. | ||
4.4.7 INSTRUMENTATION APPLICATIONS | |||
====4.4.7 INSTRUMENTATION==== | |||
APPLICATIONS | |||
4.4.7.1 Incore Instrumentation Instrumentation is located in the core so that by correlating movable neutron detector | 4.4.7.1 Incore Instrumentation Instrumentation is located in the core so that by correlating movable neutron detector | ||
| Line 4,656: | Line 4,573: | ||
2 FSAR UPDATE 4.4-36 Revision 23 December 2016 | 2 FSAR UPDATE 4.4-36 Revision 23 December 2016 | ||
: 5. I. Cohen, et al, Measurement of t he Thermal Conductivity of Metal-Clad Uranium Oxide Rods during Irradiation, WAPD-228, 1960. | : 5. I. Cohen, et al, Measurement of t he Thermal Conductivity of Metal-Clad Uranium Oxide Rods during Irradiation, WAPD-228, 1960. | ||
: 6. D. J. Clough and J. B. Sayers, The Measurement of the Thermal Conductivity of | : 6. D. J. Clough and J. B. Sayers, The Measurement of the Thermal Conductivity of UO 2 under Irradiation in the Temperature Range 150°F-1600°C, AERE-R-4690, UKAEA Research Group, Harwell, December 1964. | ||
: 7. J. P. Stora, et al, Thermal Conductivity of Sintered Uranium Oxide Under In-Pile Conditions, EURAEC-1095, August 1964. | : 7. J. P. Stora, et al, Thermal Conductivity of Sintered Uranium Oxide Under In-Pile Conditions, EURAEC-1095, August 1964. | ||
: 8. I. Devold, A Study of the Temperature Distribution in UO 2 Reactor Fuel Elements, AE-318, Aktiebolaget Atomenergi, Stockholm, Sweden, 1968. | : 8. I. Devold, A Study of the Temperature Distribution in UO 2 Reactor Fuel Elements, AE-318, Aktiebolaget Atomenergi, Stockholm, Sweden, 1968. | ||
: 9. M. G. Balfour, et al, In-Pile Measurement of UO 2 Thermal Conductivity, WCAP-2923, March 1966. | : 9. M. G. Balfour, et al, In-Pile Measurement of UO 2 Thermal Conductivity, WCAP-2923, March 1966. | ||
: 10. R. N. Duncan, Rabbit Capsule Irradiation of UO 2, CVTR Project, CVNA-142, June 1962. | : 10. R. N. Duncan, Rabbit Capsule Irradiation of UO 2 , CVTR Project, CVNA-142, June 1962. | ||
: 11. R. C. Nelson, et al, Fission Gas Release from UO 2 Fuel Rods with Gross Central Melting, GEAP-4572, July 1964. | : 11. R. C. Nelson, et al, Fission Gas Release from UO 2 Fuel Rods with Gross Central Melting, GEAP-4572, July 1964. | ||
: 12. V. C. Howard and T. G. Gulvin, Thermal Conductivity Determinations on Uranium Dioxide by a Radial Flow Method, UKAEA IG-Report 51, November 1960. | : 12. V. C. Howard and T. G. Gulvin, Thermal Conductivity Determinations on Uranium Dioxide by a Radial Flow Method, UKAEA IG-Report 51, November 1960. | ||
: 13. C. F. Lucks and H. W. Deem, "Thermal Conductivity and Electrical Conductivity of | : 13. C. F. Lucks and H. W. Deem, "Thermal Conductivity and Electrical Conductivity of UO 2 ," in Progress Reports Relating to Civi lian Applications, BMI-1448 (Revision) for June 1960, BMI-1489 (Revision) for December 1960 and BMI-1518 (Revision) for May 1961. | ||
: 14. J. L. Daniel, et al, Thermal Conductivity of UO 2, HW-69945, September 1962. | : 14. J. L. Daniel, et al, Thermal Conductivity of UO 2 , HW-69945, September 1962. | ||
: 15. A. D. Feith, Thermal Conductivity of UO 2 by a Radial Heat Flow Method, TID-21668, 1962. | : 15. A. D. Feith, Thermal Conductivity of UO 2 by a Radial Heat Flow Method, TID-21668, 1962. | ||
: 16. J. Vogt, et al, Determination of the Thermal Conductivity of Unirradiated Uranium Dioxide, AB Atomenergi Report RMB-527, 1964, Quoted by IAEA Technical Report Series No. 59, "Thermal Conductivity of Uranium Dioxide." | : 16. J. Vogt, et al, Determination of the Thermal Conductivity of Unirradiated Uranium Dioxide, AB Atomenergi Report RMB-527, 1964, Quoted by IAEA Technical Report Series No. 59, "Thermal Conductivity of Uranium Dioxide." | ||
: 17. T. Nishijima, et al, "Thermal Conductivity of Sintered UO 2 and | : 17. T. Nishijima, et al, "Thermal Conductivity of Sintered UO 2 and Al 2 O 3 at High Temperatures," J. American Ceramic Socie ty, 48, 1965, pp. 31-34. | ||
: 18. J. B. Ainscough and M. J. Wheeler, "The Thermal Diffusivity and Thermal Conductivity of Sintered Uranium Dioxide," in Proceedings of the Seventh Conference on Thermal Conductivity, National Bureau of Standards, Washington, D.C., 1968, p. 467. | : 18. J. B. Ainscough and M. J. Wheeler, "The Thermal Diffusivity and Thermal Conductivity of Sintered Uranium Dioxide," in Proceedings of the Seventh Conference on Thermal Conductivity, National Bureau of Standards, Washington, D.C., 1968, p. 467. | ||
DCPP UNITS 1 & | DCPP UNITS 1 & | ||
| Line 4,679: | Line 4,596: | ||
: 25. M. F. Lyons, et al, UO 2 Powder and Pellet Thermal Conductivity During Irradiation, GEAP-5100-1, March 1966. | : 25. M. F. Lyons, et al, UO 2 Powder and Pellet Thermal Conductivity During Irradiation, GEAP-5100-1, March 1966. | ||
: 26. D. H. Coplin, et al, The Thermal Conductivity of UO 2 by Direct In-reactor Measurements, GEAP-5100-6, March 1968. | : 26. D. H. Coplin, et al, The Thermal Conductivity of UO 2 by Direct In-reactor Measurements, GEAP-5100-6, March 1968. | ||
: 27. A. S. Bain, "The Heat Rating Required to Produce Center Melting in Various UO 2 Fuels," ASTM Special Technical Publication | : 27. A. S. Bain, "The Heat Rating Required to Produce Center Melting in Various UO 2 Fuels," ASTM Special Technical Publication , No. 306, Philadelphia, 1962, pp. 30-46. | ||
, No. 306, Philadelphia, 1962, pp. 30-46. | : 28. J. P. Stora, "In-Reactor Measurements of the Integrated Thermal Conductivity of UO 2 - Effects of Porosity," Trans. ANS, 13, 1970, pp. 137-138. | ||
: 28. J. P. Stora, "In-Reactor Measurements of the Integrated Thermal Conductivity of | : 29. International Atomic Energy Agency, "Thermal Cond uctivity of Uranium Dioxide," Report of the Panel held in Vien na, April 1965, IAEA Technical Reports Series, No. 59, Vienna, The Agency, 1966. | ||
: 29. International Atomic Energy Agency, "Thermal Cond uctivity of Uranium Dioxide," | |||
Report of the Panel held in Vien na, April 1965, IAEA Technical Reports Series, No. 59, Vienna, The Agency, 1966. | |||
: 30. C. G. Poncelet, Burnup Physics of Heterogeneous Reactor Lattices, WCAP-6069, June 1965. | : 30. C. G. Poncelet, Burnup Physics of Heterogeneous Reactor Lattices, WCAP-6069, June 1965. | ||
: 31. R. J. Nodvick, Saxton Core II Fuel Performance Evaluation, WCAP-3385-56, Part II, Evaluation of Mass Spectrometric and Radiochemical Analyses of Irradiated Saxton Plutonium Fuel, July 1970. | : 31. R. J. Nodvick, Saxton Core II Fuel Performance Evaluation, WCAP-3385-56, Part II, Evaluation of Mass Spectrometric and Radiochemical Analyses of Irradiated Saxton Plutonium Fuel, July 1970. | ||
| Line 4,692: | Line 4,607: | ||
: 33. A. M. Ross and R. L. Stoute, Heat Transfer Coefficient Between UO 2 and Zircacloy-2, AECL-1552, June 1962. | : 33. A. M. Ross and R. L. Stoute, Heat Transfer Coefficient Between UO 2 and Zircacloy-2, AECL-1552, June 1962. | ||
: 34. L. S. Tong, Boiling Crisis and Critical Heat Flux, AEC Critical Review Series, TID-25887, 1972. | : 34. L. S. Tong, Boiling Crisis and Critical Heat Flux, AEC Critical Review Series, TID-25887, 1972. | ||
: 35. F. E. Motley and F. F. Cadek, DNB Tests Results for New Mixing Vane Grids (R), | : 35. F. E. Motley and F. F. Cadek, DNB Tests Results for New Mixing Vane Grids (R), WCAP-7695 -P-A, January 1975 (Westingho use Proprietary) and WCAP-7958-A, January 1975. | ||
WCAP-7695 -P-A, January 1975 (Westingho use Proprietary) and WCAP-7958-A, January 1975. | |||
: 36. F. E. Motley, and F. F. Cadek, Application of Modified Spacer Factor to L. grid Typical and Cold Wall Cell DNB, WCAP-7988-P-A, January 1975 (Westinghouse Proprietary) and WCAP-8030-A, January 1975. | : 36. F. E. Motley, and F. F. Cadek, Application of Modified Spacer Factor to L. grid Typical and Cold Wall Cell DNB, WCAP-7988-P-A, January 1975 (Westinghouse Proprietary) and WCAP-8030-A, January 1975. | ||
: 37. F. E. Motley, et al, Critical Heat Flux Testing of 17 x 17 Fuel Assembly Geometry with 22-Inch Grid Spacing, WCAP-8536, May 1975 (Westinghouse Proprietary) and WCAP-8537, May 1975. | : 37. F. E. Motley, et al, Critical Heat Flux Testing of 17 x 17 Fuel Assembly Geometry with 22-Inch Grid Spacing, WCAP-8536, May 1975 (Westinghouse Proprietary) and WCAP-8537, May 1975. | ||
| Line 4,710: | Line 4,624: | ||
: 48. S. Nakazato and E. E. DeMario, Hydraulic Flow Test of the 17 x 17 Fuel Assembly, WCAP-8279, February 1974. | : 48. S. Nakazato and E. E. DeMario, Hydraulic Flow Test of the 17 x 17 Fuel Assembly, WCAP-8279, February 1974. | ||
: 49. F. W. Dittus and L. M. K. Boelter, "Heat Transfer in Automobile Radiators of the Tubular Type," Calif. Univ. Publication in Eng., 2, No. 13, 1930, pp. 443-461. | : 49. F. W. Dittus and L. M. K. Boelter, "Heat Transfer in Automobile Radiators of the Tubular Type," Calif. Univ. Publication in Eng., 2, No. 13, 1930, pp. 443-461. | ||
: 50. J. Weisman, "Heat Transfer to Water Flowing Parallel to Tube Bundles," | : 50. J. Weisman, "Heat Transfer to Water Flowing Parallel to Tube Bundles," Nucl. Sci. Eng., 6, 1959, pp. 78-79. | ||
Nucl. Sci. Eng., 6, 1959, pp. 78-79. | |||
: 51. J. R. S. Thom, et al, "Boiling in Sub-cooled Water During Flowup Heated Tubes or Annuli," Proc. Instn. Mech. Engrs., 180, Pt. C, 1965-66, pp. 226-46. | : 51. J. R. S. Thom, et al, "Boiling in Sub-cooled Water During Flowup Heated Tubes or Annuli," Proc. Instn. Mech. Engrs., 180, Pt. C, 1965-66, pp. 226-46. | ||
: 52. G. Hetsroni, Hydraulic Tests of the San Onofre Reactor Model, WCAP-3269-8, June 1964. | : 52. G. Hetsroni, Hydraulic Tests of the San Onofre Reactor Model, WCAP-3269-8, June 1964. | ||
| Line 4,732: | Line 4,645: | ||
: 66. J. Weisman, et al, "Experimental Determination of the Departure from Nucleate Boiling in Large Rod Bundles at High Pressures," Chem. Eng. Prog. Symp. | : 66. J. Weisman, et al, "Experimental Determination of the Departure from Nucleate Boiling in Large Rod Bundles at High Pressures," Chem. Eng. Prog. Symp. | ||
Ser. 64, No. 82, 1968, pp. 114-125. | Ser. 64, No. 82, 1968, pp. 114-125. | ||
: 67. Supplemental information on fuel design transmitted from R. Salvatori, Westinghouse NES, to D. Knuth, AEC, as attachments to Letters NS-SL-518 (12/22/72), NS-SL-521 (1/4/73), | : 67. Supplemental information on fuel design transmitted from R. Salvatori, Westinghouse NES, to D. Knuth, AEC, as attachments to Letters NS-SL-518 (12/22/72), NS-SL-521 (1/4/73), NS-SL-524 (1/4/73), and NS-SL-543 (1/12/73) (Westinghouse Proprietary), and supplemental information on fuel design transmitted from R. Salvatori, Westinghouse NES, to D. Knuth, AEC, as attachments to Letters NS-SL-527 (1/4/73), and NS-SL-544 (1/12/73). | ||
NS-SL-524 (1/4/73), and NS-SL-543 (1/12/73) (Westinghouse Proprietary), and supplemental information on fuel design transmitted from R. Salvatori, Westinghouse NES, to D. Knuth, AEC, as attachments to Letters NS-SL-527 (1/4/73), and NS-SL-544 (1/12/73). | |||
: 68. J. M. Hellman (ed), Fuel Densific ation Experimental Results and Model for Reactor Application, WCAP-8218-P-A, March 1975 (Westinghouse Proprietary) and WCAP-8219-A, March 1975. | : 68. J. M. Hellman (ed), Fuel Densific ation Experimental Results and Model for Reactor Application, WCAP-8218-P-A, March 1975 (Westinghouse Proprietary) and WCAP-8219-A, March 1975. | ||
: 69. J. A. Boure, et al, Review of Two-Phase Flow Instability, ASME Paper 71-HT-42, August 1971. | : 69. J. A. Boure, et al, Review of Two-Phase Flow Instability, ASME Paper 71-HT-42, August 1971. | ||
| Line 4,743: | Line 4,655: | ||
2 FSAR UPDATE 4.4-41 Revision 23 December 2016 | 2 FSAR UPDATE 4.4-41 Revision 23 December 2016 | ||
: 74. South Texas FSAR, Docket #50-498. | : 74. South Texas FSAR, Docket #50-498. | ||
: 75. H. S. Kao, et al., "Prediction of Flow Oscillation in Reactor Core Channel," | : 75. H. S. Kao, et al., "Prediction of Flow Oscillation in Reactor Core Channel," Trans. ANS. Vol. 16, 1973, pp. 212-213. | ||
Trans. ANS. Vol. 16, 1973, pp. 212-213. | |||
: 76. L. A. Stephan, The Effects of Cladding Material and Heat Treatment on the Response of Waterlogged UO 2 Fuel Rods to Power Bursts, IN-ITR-111, January 1970. | : 76. L. A. Stephan, The Effects of Cladding Material and Heat Treatment on the Response of Waterlogged UO 2 Fuel Rods to Power Bursts, IN-ITR-111, January 1970. | ||
: 77. Western New York Nuclear Research Center Correspondence with the AEC on February 11 and August 27, 1971, Docket 50-57. | : 77. Western New York Nuclear Research Center Correspondence with the AEC on February 11 and August 27, 1971, Docket 50-57. | ||
| Line 4,750: | Line 4,661: | ||
: 34. | : 34. | ||
: 79. J. Skaritka, (Ed.), Fuel Rod Bow Evaluati on, WCAP-8691, Revision 1 July 1979. | : 79. J. Skaritka, (Ed.), Fuel Rod Bow Evaluati on, WCAP-8691, Revision 1 July 1979. | ||
: 80. "Partial Response to Request Number 1 for Additional Information on WCAP-8691, Revision 1" Letter, E. P. Rahe, Jr., (Westinghouse) to J. R. Miller (NRC), NS-EPR-2515, dated October 1981; "Remaining Response to Request Number 1 for Additional Information on WCAP-8691, Revision 1" Letter, | : 80. "Partial Response to Request Number 1 for Additional Information on WCAP-8691, Revision 1" Letter, E. P. Rahe, Jr., (Westinghouse) to J. R. Miller (NRC), NS-EPR-2515, dated October 1981; "Remaining Response to Request Number 1 for Additional Information on WCAP-8691, Revision 1" Letter, E. P. Rahe, Jr., (Westinghouse) to J.R. Miller (NRC), NS-EPR-2572, dated March 1982. | ||
E. P. Rahe, Jr., (Westinghouse) to J.R. Miller (NRC), NS-EPR-2572, dated March 1982. | |||
: 81. C. G. Poncelet, LASER - A Depletion Program for Lattice Calculations Based on MUFT and THERMOS, WCAP-6073, April 1966. | : 81. C. G. Poncelet, LASER - A Depletion Program for Lattice Calculations Based on MUFT and THERMOS, WCAP-6073, April 1966. | ||
: 82. Technical Specifications, Diablo Canyon Power Plant Units 1 and 2, Appendix A to License Nos. DPR-80 and DPR-82, as amended. | : 82. Technical Specifications, Diablo Canyon Power Plant Units 1 and 2, Appendix A to License Nos. DPR-80 and DPR-82, as amended. | ||
| Line 4,778: | Line 4,687: | ||
101. J.P. Foster, et al., Westinghouse Improved Performance Analysis and Design Model (PAD 4.0), WCAP-15063-P-A, Revision 1, with Errata, July 2000. | 101. J.P. Foster, et al., Westinghouse Improved Performance Analysis and Design Model (PAD 4.0), WCAP-15063-P-A, Revision 1, with Errata, July 2000. | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 1 of 7 Revision 23 December 2016 REACTOR DESIGN COMPARISON Thermal and Hydraulic Design Parameters Unit 1 Unit 2 (Using ITDP) | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 1 of 7 Revision 23 December 2016 REACTOR DESIGN COMPARISON Thermal and Hydraulic Design Parameters Unit 1 Unit 2 (Using ITDP)(a) Reactor Core Heat Output, MWt 3,411 3,411 Reactor Core Heat Output, 10 6 Btu/hr 11,639 11,639 Heat Generated in Fuel, % | ||
(a) Reactor Core Heat Output, MWt 3,411 3,411 Reactor Core Heat Output, 10 6 Btu/hr 11,639 11,639 Heat Generated in Fuel, % | 97.4 97.4 Reactor Coolant Pressure, psia 2,250 2,250 Fuel Type Vantage+ Vantage+ Design DNBR Limit Typical Cell 1.34 1.34 Thimble Cell 1.32 1.32 Safety Analysis DNBR Limit Typical Cell 1.71 1.71 Thimble Cell 1.68 1.68 DNB Correlation WRB-2 WRB-2 | ||
97.4 97.4 Reactor Coolant Pressure, psia 2,250 2,250 Fuel Type Vantage+ | |||
Vantage+ | |||
Design DNBR Limit Typical Cell 1.34 1.34 Thimble Cell 1.32 1.32 Safety Analysis DNBR Limit Typical Cell 1.71 1.71 Thimble Cell 1.68 1.68 DNB Correlation WRB-2 WRB-2 | |||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 2 of 7 Revision 23 December 2016 Unit 1 Unit 2 Vessel Minimum Measured Flow Rate (including Bypass) gpm 359,200 362,500 | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 2 of 7 Revision 23 December 2016 Unit 1 Unit 2 Vessel Minimum Measured Flow Rate (including Bypass) gpm 359,200 362,500 | ||
| Line 4,789: | Line 4,695: | ||
Thermal and Hydraulic Design Parameters (Based on Thermal Design Flow) | Thermal and Hydraulic Design Parameters (Based on Thermal Design Flow) | ||
Core Flow Rate (excluding Bypass) | Core Flow Rate (excluding Bypass) 10 6 lbm/hr 122.3 123.4 gpm 324,490 327,450 Effective Core Flow Area for Heat Transfer, ft 2 54.13 54.13 Average Velocity along Fuel (k) Rods, ft/sec 14.0 14.2 Core Inlet Mass Velocity, 10 6 lbm/hr-ft (V-5) 2.26 2.28 | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 3 of 7 Revision 23 December 2016 Unit 1 Unit 2 Nominal Vessel/Core Inlet Temperature, °F 531.7 - 544.5 531.9 -545.1 Vessel Average Temperature, °F 565.0 - 577.3 565.0 - 577.6 Core Average Temperature, °F 569.1 - 581.5 569.6 - 582.3 Vessel Outlet Temperature, °F 598.3 - 610.1 598.1 - 610.1 Average Temperature Rise in Vessel, °F 66.6 - 65.6 66.2 - 65.0 Average Temperature Rise in Core, °F 71.6 - 70.4 72.1 - 70.7 Heat Transfer Active Heat Transfer Surface Area, ft 2 57,505 57,505 Average Heat Flux, Btu/hr-ft 2 197,180 197,180 Maximum Heat Flux for Normal (h) Operation, Btu/hr-ft 2 508,720 508,720 Average Linear Power, kW/ft 5.445 5.445 Peak Linear Power for Normal Operation, (h) kW/ft 14.3 14.3 Peak Linear Power for Prevention of Centerline Melt, kW/ft 22.0(i) 22.0(i) Pressure Drop (j) Across Core, psi | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 3 of 7 Revision 23 December 2016 Unit 1 Unit 2 Nominal Vessel/Core Inlet Temperature, °F 531.7 - 544.5 531.9 -545.1 Vessel Average Temperature, °F 565.0 - 577.3 565.0 - 577.6 Core Average Temperature, °F 569.1 - 581.5 569.6 - 582.3 Vessel Outlet Temperature, °F 598.3 - 610.1 598.1 - 610.1 Average Temperature Rise in Vessel, °F 66.6 - 65.6 66.2 - 65.0 Average Temperature Rise in Core, °F 71.6 - 70.4 72.1 - 70.7 Heat Transfer Active Heat Transfer Surface Area, ft 2 57,505 57,505 Average Heat Flux, Btu/hr-ft 2 197,180 197,180 Maximum Heat Flux for Normal (h) Operation, Btu/hr-ft 2 508,720 508,720 Average Linear Power, kW/ft 5.445 5.445 Peak Linear Power for Normal Operation, (h) kW/ft 14.3 14.3 Peak Linear Power for Prevention of Centerline Melt, kW/ft 22.0 (i) 22.0 (i) Pressure Drop (j) Across Core, psi | ||
* 25.5 + 2.6 27.2 + 2.7 Across Vessel, (n) including nozzle, psi | * 25.5 + 2.6 27.2 + 2.7 Across Vessel, (n) including nozzle, psi | ||
* 52.8 + 5.3 48.2 + 4.8 Thermal and Hydraulic Design Parameters (Fuel Rod Design) | * 52.8 + 5.3 48.2 + 4.8 Thermal and Hydraulic Design Parameters (Fuel Rod Design) | ||
Heat Flux Hot Channel Factor, | Heat Flux Hot Channel Factor, F Q T 2.58 2.58 Temperature at Peak Linear Power for 4,700 4,700 Prevention of Centerline Melt, °F Fuel Centerline Temperature, °F Peak at 102% power | ||
<3,360 <3,360 Peak at maximum thermal output for maximum overpower DT trip point | <3,360 <3,360 Peak at maximum thermal output for maximum overpower DT trip point | ||
<3,770 <3,770 | <3,770 <3,770 | ||
* Pressure drop values for mechanical design flow and low inlet temperatures of 531.7°F and 531.9°F for Unit 1 and Unit 2. | * Pressure drop values for mechanical design flow and low inlet temperatures of 531.7°F and 531.9°F for Unit 1 and Unit 2. | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 4 of 7 Revision 23 December 2016 Core Mechanical Design Parameters Unit 1 Unit 2 Fuel Assemblies Design RCC Canless RCC Canless Number of fuel assemblies 193 193 Rod array 17 X 17 17 X 17 | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 4 of 7 Revision 23 December 2016 Core Mechanical Design Parameters Unit 1 Unit 2 Fuel Assemblies Design RCC Canless RCC Canless Number of fuel assemblies 193 193 Rod array 17 X 17 17 X 17 U0 2 rods per assembly 264 264 Rod pitch, in 0.496 0.496 Overall dimensions, in 8.424 x 8.424 8.424 x 8.424 Fuel weight (as UO | ||
: 2) lb 200,720/205,159 200,720/205,159 Zirconium alloy weight, lb 51,917 51,917 Number of grids per assembly 12 2 non-mixing vane type | : 2) lb 200,720/205,159 200,720/205,159 Zirconium alloy weight, lb 51,917 51,917 Number of grids per assembly 12 2 non-mixing vane type | ||
| Line 4,810: | Line 4,716: | ||
Upper part 0.442 x 0.474 0.442 x 0.474 Lower part 0.397 x 0.430 0.397 x 0.430 Diameter of instrument guide thimbles, in. | Upper part 0.442 x 0.474 0.442 x 0.474 Lower part 0.397 x 0.430 0.397 x 0.430 Diameter of instrument guide thimbles, in. | ||
0.442 x 0.474 0.442 x 0.474 DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 5 of 7 Revision 23 December 2016 Core Mechanical Design Parameters (Cont'd) | 0.442 x 0.474 0.442 x 0.474 DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 5 of 7 Revision 23 December 2016 Core Mechanical Design Parameters (Cont'd) | ||
Unit 1 Unit 2 Fuel Rods Number 50,952 50,952 Outside diameter, in 0.360 0.360 Diametral gap, in 0.0062 0.0062 Cladding thickness, in 0.0225 0.0225 Cladding material ZIRLO ZIRLO Gap material Helium Helium Fuel Pellets Material UO 2 sintered UO 2 sintered Density, % of theoretical 95 95 Diameter, in 0.3088 +/- 0.0005 0.3088 +/- | Unit 1 Unit 2 Fuel Rods Number 50,952 50,952 Outside diameter, in 0.360 0.360 Diametral gap, in 0.0062 0.0062 Cladding thickness, in 0.0225 0.0225 Cladding material ZIRLO ZIRLO Gap material Helium Helium Fuel Pellets Material UO 2 sintered UO 2 sintered Density, % of theoretical 95 95 Diameter, in 0.3088 +/- 0.0005 0.3088 +/- 0.0005 Length, in Enriched or IFBA Pellets 0.370 +/- 0.025 0.370 +/- 0.025 Axial Blanket Pellets (refer to Section 4.2.1.2.2) 0.500 +/- 0.025 0.500 +/- 0.025 Mass of UO 2 , lb/ft of fuel rod 0.334 0.334 Rod Cluster Control Assemblies Neutron absorber, Ag-In-Cd Ag-In-Cd Composition 80%, 15%, 5% 80%, 15%, 5% | ||
0.0005 Length, in Enriched or IFBA Pellets 0.370 +/- 0.025 0.370 +/- 0.025 Axial Blanket Pellets (refer to Section 4.2.1.2.2) 0.500 +/- 0.025 0.500 +/- 0.025 Mass of UO 2, lb/ft of fuel rod 0.334 0.334 Rod Cluster Control Assemblies Neutron absorber, Ag-In-Cd Ag-In-Cd Composition 80%, 15%, 5% 80%, 15%, 5% | |||
Diameter, in 0.341 +/- 0.001* | Diameter, in 0.341 +/- 0.001* | ||
0.341 +/- 0.001* Nominal length of absorber material, in. 142 142 Density, lb/in 3 0.367 0.367 Cladding material Framatome RCCAs Ion-nitrided, cold worked, Type 316L SS Ion-nitrided, cold worked, Type 316L SS Westinghouse RCCAs Chrome Plated, cold worked, Type 304 SS Chrome Plated, cold worked, Type 304 SS Cladding thickness, in 0.0185 0.0185 Number of RCCAs 53 53 Number of absorber rods per cluster 24 24 Core Structure Core barrel, ID/OD, in 148.0/152.5 148.0/152.5 Thermal shield, ID/OD, in 158.5/164.0 Neutron pad Design | 0.341 +/- 0.001* Nominal length of absorber material, in. 142 142 Density, lb/in 3 0.367 0.367 Cladding material Framatome RCCAs Ion-nitrided, cold worked, Type 316L SS Ion-nitrided, cold worked, Type 316L SS Westinghouse RCCAs Chrome Plated, cold worked, Type 304 SS Chrome Plated, cold worked, Type 304 SS Cladding thickness, in 0.0185 0.0185 Number of RCCAs 53 53 Number of absorber rods per cluster 24 24 Core Structure Core barrel, ID/OD, in 148.0/152.5 148.0/152.5 Thermal shield, ID/OD, in 158.5/164.0 Neutron pad Design | ||
| Line 4,820: | Line 4,725: | ||
~10 ~10 Bottom - water plus steel, in. | ~10 ~10 Bottom - water plus steel, in. | ||
~10 ~10 Side - water plus steel, in | ~10 ~10 Side - water plus steel, in | ||
~15 ~15 | ~15 ~15 H 2 O/U, cold molecular ratio lattice 2.73 2.73 Fuel Enrichment, Wt% | ||
Maximum feed enrichment 5.0 5.0 Burnable Absorbers Type IFBA IFBA Number (typical range) 2000 - 15000 2000 - 15000 | Maximum feed enrichment 5.0 5.0 Burnable Absorbers Type IFBA IFBA Number (typical range) 2000 - 15000 2000 - 15000 | ||
Material ZrB 2 | Material ZrB 2 ZrB 2 B10 Loading, mg/inch (typical) 2.25 2.25 | ||
(a) Includes the effect of fuel densification | (a) Includes the effect of fuel densification | ||
| Line 4,837: | Line 4,742: | ||
(f) Deleted | (f) Deleted | ||
(g) Deleted (h) This limit is associated with the value of | (g) Deleted (h) This limit is associated with the value of F Q T= 2.58 (i) Refer to Section 4.3.3.2.6 | ||
(j) Based on best estimate reactor flow rate(refer to Section 5.1) | (j) Based on best estimate reactor flow rate(refer to Section 5.1) | ||
| Line 4,847: | Line 4,752: | ||
(n) Deleted | (n) Deleted | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 1 of 3 Revision 23 December 2016 ANALYTICAL TECHNIQUES IN CORE DESIGN Analysis Technique Computer Code Section Referenced Mechanical Design of Core Internals Loads, deflections, and stress analysis Static and dynamic WECAN; ANSYS; MULTIFLEX 3.0; 3.7, 3.9 modeling BLODWN-2; LATFORC; WEGAP Fuel Rod Design Fuel performance characteristics Semiempirical thermal Westinghouse fuel rod 4.2.1.2.2.5 (temperature, internal pressure, model of fuel rod with design model; PAD 4.0 4.4.3.15.2 cladding stress, etc.) | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 1 of 3 Revision 23 December 2016 ANALYTICAL TECHNIQUES IN CORE DESIGN Analysis Technique Computer Code Section Referenced Mechanical Design of Core Internals Loads, deflections, and stress analysis Static and dynamic WECAN; ANSYS; MULTIFLEX 3.0; 3.7, 3.9 modeling BLODWN-2; LATFORC; WEGAP Fuel Rod Design Fuel performance characteristics Semiempirical thermal Westinghouse fuel rod 4.2.1.2.2.5 (temperature, internal pressure, model of fuel rod with design model; PAD 4.0 4.4.3.15.2 cladding stress, etc.) | ||
consideration of fuel density changes, heat transfer, fission gas release, etc. | consideration of fuel density changes, heat transfer, fission gas release, etc. | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 2 of 3 Revision 23 December 2016 Analysis Technique Computer Code Section Referenced Nuclear Design (1) Cross sections and group Microscopic data Modified ENDF/B library 4.3.3.10.2 constants Macroscopic constants for LEOPARD /CINDER type 4.3.3.10.2 homogenized core regions and PHOENIX-P | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 2 of 3 Revision 23 December 2016 Analysis Technique Computer Code Section Referenced Nuclear Design (1) Cross sections and group Microscopic data Modified ENDF/B library 4.3.3.10.2 constants Macroscopic constants for LEOPARD /CINDER type 4.3.3.10.2 homogenized core regions and PHOENIX-P | ||
Group constants for control rods with self-shielding HAMMER-AIM and PHOENIX-P/ANC 4.3.3.10.2 4.3.3.10.3 (2) X-Y power distributions, fuel 2-D, 2-group diffusion TURTLE and ANC 4.3.3.10.3 depletion, critical boron theory concentrations, X-Y xenon distributions, reactivity coefficients and control rod worths (3) X-Y-Z power distributions, fuel 3-D, 2-group diffusion 3D PALADON 4.3.3.10.3 depletion, critical boron theory and ANC concentrations, X-Y-Z xenon distributions, reactivity coefficients and control rod worths (4) Axial power distributions 1-D, 2-group diffusion PANDA/APOLLO 4.3.3.10.3 and axial xenon distributions theory (5) Fuel rod power Integral transport theory LASER / 3D ANC 4.4.3.2.3 (6) Effective resonance Radial weighting REPAD / FIGHTH 4.3.3.10.1 temperature function DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 3 of 3 Revision 23 December 2016 Analysis Technique Computer Code Section Referenced Thermal-Hydraulic Design (1) Steady state Subchannel analysis of THINC-IV 4.4.3.3 local fluid conditions in 4.4.3.5 rod bundles, including 4.4.3.10.5 inertial and crossflow 4.4.3.12 resistance terms, solution 4.4.3.13 progresses from core-wide 4.4.3.15 to hot assembly to hot 4.4.3.21 channel (2) Transient DNB analysis Subchannel analysis of THINC-III 4.4.3.15.1.3 local fluid conditions in rod bundles during transients by including accumulation terms in con-servation equations; solution progresses from core-wide to hot assembly to hot channel | Group constants for control rods with self-shielding HAMMER-AIM and PHOENIX-P/ANC 4.3.3.10.2 4.3.3.10.3 (2) X-Y power distributions, fuel 2-D, 2-group diffusion TURTLE and ANC 4.3.3.10.3 depletion, critical boron theory concentrations, X-Y xenon distributions, reactivity coefficients and control rod worths (3) X-Y-Z power distributions, fuel 3-D, 2-group diffusion 3D PALADON 4.3.3.10.3 depletion, critical boron theory and ANC concentrations, X-Y-Z xenon distributions, reactivity coefficients and control rod worths (4) Axial power distributions 1-D, 2-group diffusion PANDA/APOLLO 4.3.3.10.3 and axial xenon distributions theory (5) Fuel rod power Integral transport theory LASER / 3D ANC 4.4.3.2.3 (6) Effective resonance Radial weighting REPAD / FIGHTH 4.3.3.10.1 temperature function DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 3 of 3 Revision 23 December 2016 Analysis Technique Computer Code Section Referenced Thermal-Hydraulic Design (1) Steady state Subchannel analysis of THINC-IV 4.4.3.3 local fluid conditions in 4.4.3.5 rod bundles, including 4.4.3.10.5 inertial and crossflow 4.4.3.12 resistance terms, solution 4.4.3.13 progresses from core-wide 4.4.3.15 to hot assembly to hot 4.4.3.21 channel (2) Transient DNB analysis Subchannel analysis of THINC-III 4.4.3.15.1.3 local fluid conditions in rod bundles during transients by including accumulation terms in con-servation equations; solution progresses from core-wide to hot assembly to hot channel | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 12 September 1998 TABLE 4.1-3 DESIGN LOADING CONDITIONS FO R REACTOR CORE COMPONENTS (1) Fuel assembly weight (2) Fuel assembly spring forces (3) Internals weight (4) Control rod scram (equivalent static load) | DCPP UNITS 1 & 2 FSAR UPDATE Revision 12 September 1998 TABLE 4.1-3 DESIGN LOADING CONDITIONS FO R REACTOR CORE COMPONENTS (1) Fuel assembly weight (2) Fuel assembly spring forces (3) Internals weight (4) Control rod scram (equivalent static load) | ||
(5) Differential pressure (6) Spring preloads (7) Coolant flow forces (static) | (5) Differential pressure (6) Spring preloads (7) Coolant flow forces (static) | ||
(8) Temperature gradients (9) Differences in thermal expansions (a) Due to temperature differences (b) Due to expansion of different materials (10) Interference between components (11) Vibration (mechanically or hydraulically induced) (12) One or more loops out of service (13) All operational transi ents listed in Table 5.2-4 (14) Pump overspeed (15) Seismic loads (DE and DDE) | (8) Temperature gradients (9) Differences in thermal expansions (a) Due to temperature differences (b) Due to expansion of different materials (10) Interference between components (11) Vibration (mechanically or hydraulically induced) (12) One or more loops out of service (13) All operational transi ents listed in Table 5.2-4 (14) Pump overspeed (15) Seismic loads (DE and DDE) | ||
(16) Blowdown forces (due to RCS branch line breaks) | (16) Blowdown forces (due to RCS branch line breaks)(a) | ||
(a) | |||
(a) In the original analysis, the blowdown forces used were those resulting from breaks in the RCS cold and hot legs. However, with the acceptance of the DCPP leak-before-break analysis by the NRC, the blowdow n forces resulting from pipe rupture events in the main reactor coolant loop pi ping no longer have to be considered in the design basis structural analyses and included in the loading combinations. Only the | (a) In the original analysis, the blowdown forces used were those resulting from breaks in the RCS cold and hot legs. However, with the acceptance of the DCPP leak-before-break analysis by the NRC, the blowdow n forces resulting from pipe rupture events in the main reactor coolant loop pi ping no longer have to be considered in the design basis structural analyses and included in the loading combinations. Only the | ||
| Line 4,866: | Line 4,770: | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.3-1 Sheet 1 of 2 Revision 23 December 2016 NUCLEAR DESIGN PARAMETERS (Typical) | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.3-1 Sheet 1 of 2 Revision 23 December 2016 NUCLEAR DESIGN PARAMETERS (Typical) | ||
Core Average Linear Power, kW/ft, including densification effects 5.445 (a) Total Heat Flux Hot Channel Factor, | Core Average Linear Power, kW/ft, including densification effects 5.445 (a) Total Heat Flux Hot Channel Factor, F Q T 2.58 Nuclear Enthalpy Rise Hot Channel Factor, | ||
F H N 1.65 VANTAGE+ | |||
Reactivity Coefficients | Reactivity Coefficients | ||
| Line 4,879: | Line 4,783: | ||
Delayed Neutron Fraction and Lifetime eff BOL, (EOL) 0.0069, (0.0051) | Delayed Neutron Fraction and Lifetime eff BOL, (EOL) 0.0069, (0.0051) | ||
l* BOL, (EOL), | l* BOL, (EOL), µsec 19.2, (18.6) | ||
µsec 19.2, (18.6) | |||
Control Rod Worths | Control Rod Worths | ||
| Line 4,891: | Line 4,794: | ||
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.3-1 Sheet 2 of 2 Revision 23 December 2016 Boron Concentrations (ppm) | DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.3-1 Sheet 2 of 2 Revision 23 December 2016 Boron Concentrations (ppm) | ||
Refueling 2000 | Refueling 2000 k eff = 0.95, cold, rod cluster control assemblies in 2000 Full power, no xenon, k eff = 1.0, hot, rod cluster control assemblies out 1876 (d) | ||
Full power, equilibrium xenon, k eff = 1.0, hot, rod cluster control assemblies out 1536 (d) | Full power, equilibrium xenon, k eff = 1.0, hot, rod cluster control assemblies out 1536 (d) | ||
Reduction with fuel burnup Typical reload cycle, ppm/GWD/MTU (c) Refer to Figure 4.3-3 (a) Data in table based on Unit 1 and Unit 2 | Reduction with fuel burnup Typical reload cycle, ppm/GWD/MTU (c) Refer to Figure 4.3-3 (a) Data in table based on Unit 1 and Unit 2 | ||
(b) 1 pcm = percent mille = 10-5 where is calculated from two state point values of k eff by ln ( | (b) 1 pcm = percent mille = 10-5 where is calculated from two state point values of k eff by ln (k 2/k 1 ) (c) Gigawatt day (GWD) = 1000 megawatt days (1000 MWD) | ||
(d) These values are representative values used for analytical purposes only. | (d) These values are representative values used for analytical purposes only. | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.3-2 UNIT 1 - REACTIVITY REQUIREMENTS FOR ROD CLUSTER CONTROL ASSEMBLIES HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED Reactivity Effects, Beginning of Life End of Life End of Life | DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.3-2 UNIT 1 - REACTIVITY REQUIREMENTS FOR ROD CLUSTER CONTROL ASSEMBLIES HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED Reactivity Effects, Beginning of Life End of Life End of Life | ||
% (First Cycle) | % (First Cycle) (First Cycle) (Equilibrium Cycle) | ||
(First Cycle) | (Typical) 1. Control Requirements Fuel temperature (Doppler) 1.39 (a) 1.12 (a) 1.00 Moderator temperature(includes void) 0.16 0.89 0.80 Redistribution 0.50 0.85 0.90 Rod insertion allowance 0.50 0.50 0.50 2. Total Control 2.55 3.36 3.20 3. Estimated Rod Cluster Control Assembly Worth (53 Rods) | ||
(Equilibrium Cycle) | All but one (highest worth) assemblies inserted 7.18 7.05 6.50 4. Estimated Rod Cluster Control Assembly-Credit with 10% adjustment to accommodate uncertainties 6.46 6.34 5.85 5. Shutdown Margin Available (Section 4.2) 3.91 2.98 2.65 (b) (a) Includes 0.1 percent uncertainty | ||
(Typical) 1. Control Requirements Fuel temperature (Doppler) 1.39(a) 1.12(a) 1.00 Moderator temperature(includes void) 0.16 0.89 0.80 Redistribution 0.50 0.85 0.90 Rod insertion allowance 0.50 0.50 0.50 2. Total Control 2.55 3.36 3.20 3. Estimated Rod Cluster Control Assembly Worth (53 Rods) | |||
All but one (highest worth) assemblies inserted 7.18 7.05 6.50 4. Estimated Rod Cluster Control Assembly-Credit with 10% adjustment to accommodate uncertainties 6.46 6.34 5.85 5. Shutdown Margin Available (Section 4.2) 3.91 2.98 2.65(b) (a) Includes 0.1 percent uncertainty | |||
(b) The design basis minimum shutdown margin is 1.6% | (b) The design basis minimum shutdown margin is 1.6% | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.3-3 UNIT 2 - REACTIVITY REQUIREMENTS FOR ROD CLUSTER CONTROL ASSEMBLIES HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED Reactivity Effects, Beginning of Life End of Life End of Life | DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.3-3 UNIT 2 - REACTIVITY REQUIREMENTS FOR ROD CLUSTER CONTROL ASSEMBLIES HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED Reactivity Effects, Beginning of Life End of Life End of Life | ||
% (First Cycle) | % (First Cycle) (First Cycle) (Equilibrium Cycle) | ||
(First Cycle) | (Typical) 1. Control Requirements Fuel temperature (Doppler) 1.39 (a) 1.12 (a) 1.00 Moderator temperature (includes void) 0.29 0.96 0.94 Redistribution 0.50 0.85 0.90 Rod insertion allowance 0.50 0.50 0.50 2. Total Control 2.68 3.43 3.34 3. Estimated Rod Cluster Control Assembly Worth (53 Rods) | ||
(Equilibrium Cycle) | All but one (highest worth) assemblies inserted 6.48 6.38 5.70 4. Estimated Rod Cluster Control Assembly (Credit with 10% adjustment to accommodate uncertainties 5.83 5.74 5.13 5. Shutdown Margin Available (Section 4.2) 3.15 2.31 1.79 (b) (a) Includes 0.1% uncertainty | ||
(Typical) 1. Control Requirements Fuel temperature (Doppler) 1.39(a) 1.12(a) 1.00 Moderator temperature (includes void) 0.29 0.96 0.94 Redistribution 0.50 0.85 0.90 Rod insertion allowance 0.50 0.50 0.50 2. Total Control 2.68 3.43 3.34 3. Estimated Rod Cluster Control Assembly Worth (53 Rods) | |||
All but one (highest worth) assemblies inserted 6.48 6.38 5.70 4. Estimated Rod Cluster Control Assembly (Credit with 10% adjustment to accommodate uncertainties 5.83 5.74 5.13 5. Shutdown Margin Available (Section 4.2) 3.15 2.31 1.79(b) (a) Includes 0.1% uncertainty | |||
(b) The design basis minimum shutdown margin is 1.6% | (b) The design basis minimum shutdown margin is 1.6% | ||
| Line 4,918: | Line 4,817: | ||
TABLE 4.3-4 AXIAL STABILITY INDEX PWR CORE WITH A 12-FT HEIGHT Burnup Stability Index, hr | TABLE 4.3-4 AXIAL STABILITY INDEX PWR CORE WITH A 12-FT HEIGHT Burnup Stability Index, hr | ||
-1 (MWD/MTU) | -1 (MWD/MTU) | ||
F Z C B (ppm) Exp. Calc. | |||
1550 1.34 1065 | 1550 1.34 1065 | ||
-0.041 -0.032 7700 1.27 700 | -0.041 -0.032 7700 1.27 700 | ||
| Line 4,930: | Line 4,829: | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-6 COMPARISON OF MEASURED AND CALCULATED DOPPLER DEFECTS Core Burnup Measured Calculated | DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-6 COMPARISON OF MEASURED AND CALCULATED DOPPLER DEFECTS Core Burnup Measured Calculated | ||
Plant Fuel Type (MWD/MTU) | Plant Fuel Type (MWD/MTU) (pcm)(a) (pcm) 1 Air filled 1800 1700 1710 | ||
2 Air filled 7700 1300 1440 | 2 Air filled 7700 1300 1440 | ||
| Line 4,938: | Line 4,836: | ||
-5 . See footnote in Table 4.3-1 | -5 . See footnote in Table 4.3-1 | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-7 BENCHMARK CRITICAL EXPERIMENTS Description of No. of LEOPARD k eff Using Experiments Experiments Experimental Bucklings | DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-7 BENCHMARK CRITICAL EXPERIMENTS Description of No. of LEOPARD k eff Using Experiments Experiments Experimental Bucklings UO 2 Al clad 14 1.0012 SS clad 19 0.9963 Borated H 2O 7 0.9989 Total 40 0.9985 | ||
U-metal Al clad 41 0.9995 Unclad 20 0.9990 | U-metal Al clad 41 0.9995 Unclad 20 0.9990 | ||
| Line 4,954: | Line 4,850: | ||
U-234/U 4.65 x 10 | U-234/U 4.65 x 10 | ||
-5 29 4.60 x 10 | -5 29 4.60 x 10-5 U-235/U 5.74 x 10 | ||
-5 U-235/U 5.74 x 10 | -3 0.9 5.73 x 10-3 U-236/U 3.55 x 10 | ||
-3 0.9 5.73 x 10 | -4 5.6 3.74 x 10-4 U-238/U 0.99386 0.01 0.99385 Pu-238/Pu 1.32 x 10 | ||
-3 U-236/U 3.55 x 10 | |||
-4 5.6 3.74 x 10 | |||
-4 U-238/U 0.99386 0.01 0.99385 Pu-238/Pu 1.32 x 10 | |||
-3 2.3 1.222 x 10 | -3 2.3 1.222 x 10 | ||
-3 Pu-239/Pu 0.73971 0.03 0.74497 Pu-240/Pu 0.19302 0.2 0.19102 Pu-241/Pu 6.014 x 10 | -3 Pu-239/Pu 0.73971 0.03 0.74497 Pu-240/Pu 0.19302 0.2 0.19102 Pu-241/Pu 6.014 x 10 | ||
-2 0.3 5.74 x 10 | -2 0.3 5.74 x 10-2 Pu-242/Pu 5.81 x 10 | ||
-2 Pu-242/Pu 5.81 x 10 | -3 0.9 5.38 x 10-3 Pu/U (a) 5.938 x 10 | ||
-3 0.9 5.38 x 10 | |||
-3 Pu/U(a) 5.938 x 10 | |||
-2 0.7 5.970 x 10 | -2 0.7 5.970 x 10 | ||
-2 Np-237/U-238 1.14 x 10 | -2 Np-237/U-238 1.14 x 10 | ||
-4 15 0.86 x 10 | -4 15 0.86 x 10-4 Am-241/Pu-239 1.23 x 10 | ||
-4 Am-241/Pu-239 1.23 x 10 | -2 15 1.08 x 10-2 Cm-242/Pu-239 1.05 x 10 | ||
-2 15 1.08 x 10 | -4 10 1.11 x 10-4 Cm-244/Pu-239 1.09 x 10 | ||
-2 Cm-242/Pu-239 1.05 x 10 | -4 20 0.98 x 10-4 (a) Weight ratio | ||
-4 10 1.11 x 10 | |||
-4 Cm-244/Pu-239 1.09 x 10 | |||
-4 20 0.98 x 10 | |||
-4 (a) Weight ratio | |||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-9 CRITICAL BORON CONCENTRA TIONS, AT HZP, BOL | DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-9 CRITICAL BORON CONCENTRA TIONS, AT HZP, BOL | ||
| Line 5,003: | Line 4,890: | ||
ESADA Critical, 0.69-in pitch, | ESADA Critical, 0.69-in pitch, | ||
2 wt.% PuO 2, 8% | 2 wt.% PuO 2 , 8% Pu 240 , 9 Control Rods 6.21-in rod separation 2250 2250 2.07-in rod separation 4220 4160 1.38-in rod separation 4100 4010 | ||
CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | ||
TABLE 4.3-11 COMPARISON OF MEASURED AND CALCULATED MODERATOR TEMPERATURE COEFFICIENTS AT HZP, BOL Measured iso(a) Calculated iso Plant Type/Control Bank Configuration pcm/°F pcm/°F 3-Loop, 157 Assemblies, 12-foot core D at 160 steps | TABLE 4.3-11 COMPARISON OF MEASURED AND CALCULATED MODERATOR TEMPERATURE COEFFICIENTS AT HZP, BOL Measured iso (a) Calculated iso Plant Type/Control Bank Configuration pcm/°F pcm/°F 3-Loop, 157 Assemblies, 12-foot core D at 160 steps | ||
-0.50 -0.50 D in, C at 190 steps | -0.50 -0.50 D in, C at 190 steps | ||
-3.01 -2.75 D in, C at 28 steps | -3.01 -2.75 D in, C at 28 steps | ||
| Line 5,014: | Line 4,901: | ||
-2.40 -1.90 C and D in, B at 165 steps | -2.40 -1.90 C and D in, B at 165 steps | ||
-4.40 -5.58 B, C, and D in, A at 174 steps | -4.40 -5.58 B, C, and D in, A at 174 steps | ||
-8.70 -8.12 (a) Isothermal coefficients, which include the Doppler effect in the fuel iso = | -8.70 -8.12 (a) Isothermal coefficients, which include the Doppler effect in the fuel iso = 10 5 ln(k 2 k 1)/T(°F) | ||
CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-1 UNIT 1 VOID FRACTIONS AT NOMINAL REACTOR CONDITIONS WITH DESIGN HOT CHANNEL FACTORS | CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-1 UNIT 1 VOID FRACTIONS AT NOMINAL REACTOR CONDITIONS WITH DESIGN HOT CHANNEL FACTORS | ||
| Line 5,032: | Line 4,919: | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED. | ||
TABLE 4.4-3 COMPARISON OF THINC-IV AND THINC-I PREDICTIONS WITH DATA FROM REPRESENTATIVE WESTINGHOUSE TWO- AND THREE-LOOP REACTORS Improvement, | TABLE 4.4-3 COMPARISON OF THINC-IV AND THINC-I PREDICTIONS WITH DATA FROM REPRESENTATIVE WESTINGHOUSE TWO- AND THREE-LOOP REACTORS Improvement, °F Power, % Full Measured Inlet rms , °F , °F for THINC-IV Reactor MWt Power Temp, °F THINC-I THINC-IV over THINC-1 Ginna 847 65.1 543.7 1.97 1.83 0.14 854 65.7 544.9 1.56 1.46 0.10 857 65.9 543.9 1.97 1.82 0.15 947 72.9 543.8 1.92 1.74 0.18 961 74.0 543.7 1.97 1.79 0.18 1091 83.9 542.5 1.73 1.54 0.19 1268 97.5 542.0 2.35 2.11 0.24 1284 98.8 240.2 2.69 2.47 0.22 1284 98.9 541.0 2.42 2.17 0.25 1287 99.0 544.4 2.26 1.97 0.29 1294 99.5 540.8 2.20 1.91 0.29 1295 99.6 542.0 2.10 1.83 0.27 | ||
°F Power, % Full Measured Inlet rms, °F , °F for THINC-IV Reactor MWt Power Temp, °F THINC-I THINC-IV over THINC-1 Ginna 847 65.1 543.7 1.97 1.83 0.14 854 65.7 544.9 1.56 1.46 0.10 857 65.9 543.9 1.97 1.82 0.15 947 72.9 543.8 1.92 1.74 0.18 961 74.0 543.7 1.97 1.79 0.18 1091 83.9 542.5 1.73 1.54 0.19 1268 97.5 542.0 2.35 2.11 0.24 1284 98.8 240.2 2.69 2.47 0.22 1284 98.9 541.0 2.42 2.17 0.25 1287 99.0 544.4 2.26 1.97 0.29 1294 99.5 540.8 2.20 1.91 0.29 1295 99.6 542.0 2.10 1.83 0.27 | |||
Robinson 1427.0 65.1 548.0 1.85 1.88 0.03 1422.6 64.9 549.4 1.39 1.39 0.00 1929.0 88.0 550.0 2.35 2.34 0.01 2207.3 100.7 534.0 2.41 2.41 0.00 2213.9 101.0 533.8 2.52 2.44 0.08 | Robinson 1427.0 65.1 548.0 1.85 1.88 0.03 1422.6 64.9 549.4 1.39 1.39 0.00 1929.0 88.0 550.0 2.35 2.34 0.01 2207.3 100.7 534.0 2.41 2.41 0.00 2213.9 101.0 533.8 2.52 2.44 0.08 | ||
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-4 NON-LOCA DNB ANALYSIS METHOD UFSAR Section(s) | DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-4 NON-LOCA DNB ANALYSIS METHOD UFSAR Section(s) | ||
Event DNB Analysis Method(a) 15.2.1 RCCA Bank Withdrawal from Subcritical Non-ITDP 15.2.2 RCCA Bank Withdrawal at Power ITDP 15.2.3 RCCA Misoperation (Dropped Rod) | Event DNB Analysis Method (a) 15.2.1 RCCA Bank Withdrawal from Subcritical Non-ITDP 15.2.2 RCCA Bank Withdrawal at Power ITDP 15.2.3 RCCA Misoperation (Dropped Rod) | ||
ITDP 15.2.4 Uncontrolled Boron Dilution Not Applicable (b) 15.2.5 Partial Loss of Flow ITDP 15.2.6 Startup of an Inactive Loop (c) Non-ITDP 15.2.7 Loss of Electrical Load / Turbine Trip ITDP 15.2.8, 15.2.9 Loss of Normal Feedwater / Loss of Offsite Power Not Applicable (Non-DNB) 15.2.10 Feedwater Malfunction (excess flow) | ITDP 15.2.4 Uncontrolled Boron Dilution Not Applicable (b) 15.2.5 Partial Loss of Flow ITDP 15.2.6 Startup of an Inactive Loop (c) Non-ITDP 15.2.7 Loss of Electrical Load / Turbine Trip ITDP 15.2.8, 15.2.9 Loss of Normal Feedwater / Loss of Offsite Power Not Applicable (Non-DNB) 15.2.10 Feedwater Malfunction (excess flow) | ||
ITDP 15.2.11 Sudden Feedwater Temperature Reduction ITDP 15.2.12 Excessive Load Increase ITDP 15.2.13 Accidental RCS Depressurization ITDP 15.2.14 Accidental MSS Depressurization (d) Non-ITDP 15.2.15 Spurious SI Actuation at Power ITDP 15.3.4 Complete Loss of Flow ITDP 15.3.5 Single RCCA Withdrawal at Power ITDP 15.4.2.1 Rupture of a Main Steam Line (HZP) | ITDP 15.2.11 Sudden Feedwater Temperature Reduction ITDP 15.2.12 Excessive Load Increase ITDP 15.2.13 Accidental RCS Depressurization ITDP 15.2.14 Accidental MSS Depressurization (d) Non-ITDP 15.2.15 Spurious SI Actuation at Power ITDP 15.3.4 Complete Loss of Flow ITDP 15.3.5 Single RCCA Withdrawal at Power ITDP 15.4.2.1 Rupture of a Main Steam Line (HZP) | ||
| Line 5,047: | Line 4,933: | ||
(d) Bounded by Section 15.4.2.1; no longer analyzed. | (d) Bounded by Section 15.4.2.1; no longer analyzed. | ||
Revision 11 November 1996 FIGURE 4.2-1 FUEL ASSEMBLY CROSS SECTION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-2 FUEL ASSEMBLY OUTLINE (LOPAR) UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-3 FUEL ROD SCHEMATIC (LOPAR) UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-4 TYPICAL CLAD AND PELLET DIMENSIONS AS A FUNCTION OF EXPOSURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-5 REPRESENTATIVE FUEL ROD INTERNAL PRESSURE AND LINEAR POWER DENSITY FOR THE LEAD BURNUP ROD AS A FUNCTION OF TIME UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.2-6 REMOVABLE ROD COMPARED TO STANDARD ROD UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE HISTORICALRevision23December2016 Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-7 REMOVABLE FUEL ROD ASSEMBLY OUTLINE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision23December2016 HISTORICAL Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-8 LOCATION OF REMOVABLE RODS WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision23December2016 HISTORICAL Revision 11 November 1996 FIGURE 4.2-9 LOWER CORE SUPPORT ASSEMBLY UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-10 LOWER CORE SUPPORT ASSEMBLY UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-11 NEUTRON SHIELD PAD LOWER CORE SUPPORT STRUCTURE UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-12 UPPER CORE SUPPORT STRUCTURE UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November Revision 11 November 1996 FIGURE 4.2-13 UPPER CORE SUPPORT STRUCTURE UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-14 PLAN VIEW OF UPPER CORE SUPPORT STRUCTURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-15 ROD CLUSTER CONTROL AND DRIVE ROD ASSEMBLY WITH INTERFACING COMPONENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE | Revision 11 November 1996 FIGURE 4.2-1 FUEL ASSEMBLY CROSS SECTION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-2 FUEL ASSEMBLY OUTLINE (LOPAR) UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-3 FUEL ROD SCHEMATIC (LOPAR) UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-4 TYPICAL CLAD AND PELLET DIMENSIONS AS A FUNCTION OF EXPOSURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-5 REPRESENTATIVE FUEL ROD INTERNAL PRESSURE AND LINEAR POWER DENSITY FOR THE LEAD BURNUP ROD AS A FUNCTION OF TIME UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.2-6 REMOVABLE ROD COMPARED TO STANDARD ROD UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE HISTORICALRevision23December2016 Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-7 REMOVABLE FUEL ROD ASSEMBLY OUTLINE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision23December2016 HISTORICAL Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-8 LOCATION OF REMOVABLE RODS WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision23December2016 HISTORICAL Revision 11 November 1996 FIGURE 4.2-9 LOWER CORE SUPPORT ASSEMBLY UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-10 LOWER CORE SUPPORT ASSEMBLY UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-11 NEUTRON SHIELD PAD LOWER CORE SUPPORT STRUCTURE UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-12 UPPER CORE SUPPORT STRUCTURE UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November Revision 11 November 1996 FIGURE 4.2-13 UPPER CORE SUPPORT STRUCTURE UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-14 PLAN VIEW OF UPPER CORE SUPPORT STRUCTURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-15 ROD CLUSTER CONTROL AND DRIVE ROD ASSEMBLY WITH INTERFACING COMPONENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE | ||
1.840 DIA. | 1.840 DIA. | ||
NOM. (1) | NOM. (1)SPRING SPIDER BODY 0.361 DIA. (3) 0.381 DIA. | ||
.88 TRAV. | .88 TRAV.SPRING RETAINER 1.25 DIA. (2) 150.574 161.0 142.00 ABSORBER LENGTH ABSORBER 80% SILVER, 15% INDIUM, 5% CADMIUM NOTE: DIMENSIONS SHOWN FOR ALL MODELS ANNOTATED DIMENSIONS ARE WESTINGHOUSE MODEL WITH FRAMATOME MODEL HAVING THE FOLLOWING DIMENSIONS: (1) 1.804 (2) 1.240 (3) 0.354 | ||
SPRING RETAINER 1.25 DIA. (2) 150. | |||
Revision 14 November 2001 FSAR UPDATEUNITS 1 AND 2 DIABLO CANYON SITE FIGURE 4.2-16 ROD CLUSTER CONTROL ASSEMBLY OUTLINE | Revision 14 November 2001 FSAR UPDATEUNITS 1 AND 2 DIABLO CANYON SITE FIGURE 4.2-16 ROD CLUSTER CONTROL ASSEMBLY OUTLINE | ||
| Line 5,060: | Line 4,944: | ||
NOTE: WESTINGHOUSE DIMENSION SHOWN. | NOTE: WESTINGHOUSE DIMENSION SHOWN. | ||
FRAMATOME ROD LENGTH IS 153.658-154.468. | FRAMATOME ROD LENGTH IS 153.658-154.468. | ||
Revision 14 November 2001 FSAR UPDATEUNITS 1 AND 2 DIABLO CANYON SITE FIGURE 4.2-17 ABSORBER ROD Revision 11 November 1996 FIGURE 4.2-18A WET ANNULAR BURNABLE ABSORBER ROD UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-21 SECONDARY SOURCE ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-22 THIMBLE PLUG ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE FIGURE 4.2-23 CONTROL ROD DRIVE MECHANISM UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 20 November 2011 FIGURE 4.2-24 CONTROL ROD DRIVE MECHANISM SCHEMATIC UNITS 1 AND 2 DIABLO CANYON SITE | Revision 14 November 2001 FSAR UPDATEUNITS 1 AND 2 DIABLO CANYON SITE FIGURE 4.2-17 ABSORBER ROD Revision 11 November 1996 FIGURE 4.2-18A WET ANNULAR BURNABLE ABSORBER ROD UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-21 SECONDARY SOURCE ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-22 THIMBLE PLUG ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE FIGURE 4.2-23 CONTROL ROD DRIVE MECHANISM UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 20 November 2011 FIGURE 4.2-24 CONTROL ROD DRIVE MECHANISM SCHEMATIC UNITS 1 AND 2 DIABLO CANYON SITE F S AR UPDATERevision 20 November 2011 Revision 11 November 1996 FIGURE 4.2-25 NOM AL LATCH CLEARANCE AT MINIMUM AND MAXIMUM TEMPERATURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.2-26 CONTROL ROD DRIVE MECHANISM LATCH CLEARANCE THERMAL EFFECT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-1 FUEL LOADING ARRANGEMENT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE LBVP Enhanced UFSARLBVPUFSARChangeRequestReactor,NuclearDesign Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-3 BORON CONCENTRATION VS CYCLE BURNUP WITH BURNABLE ABSORBER RODS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-4 BURNABLE ABSORBER ROD ARRANGEMENT WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-5 TYPICAL INTEGRAL FUEL BURNABLE ABSORBER ROD ARRANGEMENT WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-6 BURNABLE ABSORBER LOADING PATTERN UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-7 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BEGINNING OF LIFE (BOL), UNRODDED CORE, HOT FULL POWER, NO XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-8 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BOL UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-9 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BOL GROUP D AT INSERTION LIMIT, HOT FULL POWER, EQUILIBRIUM XENON UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-10 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BOL GROUP D AT INSERTION LIMIT, HOT FULL POWER, EQUILIBRIUM XENON UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-11 NORMALIZED POWER DENSITY DISTRIBUTION NEAR MIDDLE OF LIFE (MOL) | ||
UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-12 NORMALIZED POWER DENSITY DISTRIBUTION NEAR END OF LIFE (EOL) | UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-12 NORMALIZED POWER DENSITY DISTRIBUTION NEAR END OF LIFE (EOL) | ||
UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-13 RODWISE POWER DISTRIBUTION IN A TYPICAL ASSEMBLY (G-10) | UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-13 RODWISE POWER DISTRIBUTION IN A TYPICAL ASSEMBLY (G-10) | ||
NEAR BOL, HOT FULL POWER, EQUILIBRIUM XENON, UNRODDED CORE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-14 RODWISE POWER DISTRIBUTION IN A TYPICAL ASSEMBLY (G-10) | NEAR BOL, HOT FULL POWER, EQUILIBRIUM XENON, UNRODDED CORE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-14 RODWISE POWER DISTRIBUTION IN A TYPICAL ASSEMBLY (G-10) | ||
NEAR EOL, HOT FULL POWER, EQUILIBRIUM XENON, UNRODDED CORE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-15 POSSIBLE AXIAL POWER SHAPES AT BOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-16 POSSIBLE AXIAL POWER SHAPES AT MOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-17 POSSIBLE AXIAL POWER SHAPES AT EOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-21 PEAK POWER DENSITY DURING CONTROL ROD MALFUNCTION OVERPOWER TRANSIENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-22 PEAK LINEAR POWER DURING BORATION / DILUTION OVERPOWER TRANSIENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-23 MAXIMUM | NEAR EOL, HOT FULL POWER, EQUILIBRIUM XENON, UNRODDED CORE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-15 POSSIBLE AXIAL POWER SHAPES AT BOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-16 POSSIBLE AXIAL POWER SHAPES AT MOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-17 POSSIBLE AXIAL POWER SHAPES AT EOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-21 PEAK POWER DENSITY DURING CONTROL ROD MALFUNCTION OVERPOWER TRANSIENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-22 PEAK LINEAR POWER DURING BORATION / DILUTION OVERPOWER TRANSIENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-23 MAXIMUM Fx Q T POWER vs AXIAL HEIGHT DURING NORMAL OPERATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-25 COMPARISON BETWEEN CALCULATED AND MEASURED RELATIVE FUEL ASSEMBLY POWER DISTRIBUTION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-26 COMPARISON OF CALCULATED AND MEASURED AXIAL SHAPE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-27 MEASURED VALUES OF F Q T FOR FULL POWER ROD CONFIGURATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-28 DOPPLER TEMPERATURE COEFFICIENT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-29 DOPPLER ONLY POWER COEFFICIENT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-30 DOPPLER ONLY POWER DEFECT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-31 MODERATOR TEMPERATURE COEFFICIENT AT BOL, NO RODS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-32 MODERATOR TEMPERATURE COEFFICIENT AT EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-33 MODERATOR TEMPERATURE COEFFICIENT AS A FUNCTION OF BORON CONCENTRATION AT BOL, NO RODS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-34 HOT FULL POWER MODERATOR TEMPERATURE COEFFICIENT FOR CRITICAL BORON CONCENTRATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-35 TOTAL POWER COEFFICIENT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-36 TOTAL POWER DEFECT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-37 ROD CLUSTER CONTROL ASSEMBLY PATTERN UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-38 ROD CLUSTER CONTROL ASSEMBLY PATTERN UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-39 ACCIDENTAL SIMULTANEOUS WITHDRAWAL OF TWO CONTROL BANKS EOL, HZP BANKS B AND D MOVING IN THE SAME PLANE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-40 DESIGN - TRIP CURVE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-41 NORMALIZED ROD WORTH vs. | ||
PERCENT INSERTION, ALL RODS BUT ONE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-42 AXIAL OFFSET vs. TIME PWR CORE WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-43 XY XENON TEST THERMOCOUPLE RESPONSE QUADRANT TILT DIFFERENCE vs. TIME UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-44 CALCULATED AND MEASURED DOPPLER DEFECT AND COEFFICIENTS AT BOL, FOR A TWO-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-45 COMPARISON OF CALCULATED AND MEASURED BORON CONCENTRATION FOR A TWO-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-46 COMPARISON OF CALCULATED AND MEASURED BORON FOR A TWO LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-47 COMPARISON OF CALCULATED AND MEASURED BORON IN A 3-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 157 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-1 PEAK FUEL AVERAGE AND SURFACE TEMPERATURES DURING FUEL ROD LIFETIME vs. LINEAR POWER DENSITY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-2 PEAK FUEL CENTERLINE TEMPERATURE DURING FUEL ROD LIFETIME vs. LINEAR POWER DENSITY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-3 THERMAL CONDUCTIVITY OF UO 2 (DATA CORRECTED TO 95% | PERCENT INSERTION, ALL RODS BUT ONE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-42 AXIAL OFFSET vs. TIME PWR CORE WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-43 XY XENON TEST THERMOCOUPLE RESPONSE QUADRANT TILT DIFFERENCE vs. TIME UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-44 CALCULATED AND MEASURED DOPPLER DEFECT AND COEFFICIENTS AT BOL, FOR A TWO-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-45 COMPARISON OF CALCULATED AND MEASURED BORON CONCENTRATION FOR A TWO-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-46 COMPARISON OF CALCULATED AND MEASURED BORON FOR A TWO LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-47 COMPARISON OF CALCULATED AND MEASURED BORON IN A 3-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 157 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-1 PEAK FUEL AVERAGE AND SURFACE TEMPERATURES DURING FUEL ROD LIFETIME vs. LINEAR POWER DENSITY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-2 PEAK FUEL CENTERLINE TEMPERATURE DURING FUEL ROD LIFETIME vs. LINEAR POWER DENSITY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-3 THERMAL CONDUCTIVITY OF UO 2 (DATA CORRECTED TO 95% | ||
THEORETICAL DENSITY) | THEORETICAL DENSITY) | ||
UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-4 AXIAL VARIATION OF AVERAGE CLAD TEMPERATURE FOR ROD OPERATING AT 5.43 KW/FT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-5 PROBABILITY CURVES FOR W-3 AND R GRID DNB CORRELATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-6 TDC vs. REYNOLDS NUMBER FOR 26-INCH GRID SPACING UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-7 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 4-FT ELEVATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-8 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 8-FT ELEVATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-9 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 12-FT ELEVATION CORE EXIT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-10 VOID FRACTION vs. THERMODYNAMIC QUALITY H-HSAT/ | UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-4 AXIAL VARIATION OF AVERAGE CLAD TEMPERATURE FOR ROD OPERATING AT 5.43 KW/FT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-5 PROBABILITY CURVES FOR W-3 AND R GRID DNB CORRELATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-6 TDC vs. REYNOLDS NUMBER FOR 26-INCH GRID SPACING UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-7 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 4-FT ELEVATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-8 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 8-FT ELEVATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-9 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 12-FT ELEVATION CORE EXIT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-10 VOID FRACTION vs. THERMODYNAMIC QUALITY H-HSAT/H G-HSAT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-11 PWR NATURAL CIRCULATION TEST UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-12 COMPARISON OF A REPRESENTATIVE W TWO-LOOP REACTOR INCORE THERMOCOUPLE MEASUREMENTS WITH THINC-IV PREDICTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-13 COMPARISON OF A REPRESENTATIVE W THREE-LOOP REACTOR INCORE THERMOCOUPLE MEASUREMENTS WITH THINC-IV PREDICTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-14 HANFORD SUBCHANNEL TEMPERATURE DATA COMPARISON WITH THINC-IV UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-15 HANFORD SUBCRITICAL TEMPERATURE DATA COMPARISON WITH THINC-IV UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-16 DISTRIBUTION OF INCORE INSTRUMENTATION UNIT 1 DIABLO CANYON SITE FSAR UPDATE Error! Not a valid embedded object. Revision 11 November 1996 FIGURE 4.4-17 DISTRIBUTION OF INCORE INSTRUMENTATION UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-18 IMPROVED THERMAL DESIGN PROCEDURE ILLUSTRATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-19 MEASURED VERSES PREDICTED CRITICAL HEAT FLUX - WRB-1 CO ETION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE HISTORICALRevision23December2016 Revision 11 November 1996 FIGURE 4.4-20 MEASURED VERSES PREDICTED CRITICAL HEAT FLUX - WRB-2 CO ETION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016}} | ||
Latest revision as of 04:06, 16 March 2019
Text
DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title
Page i Revision 23 December 2016 4.1
SUMMARY
DESCRIPTION 4.1-1 4.
1.1 REFERENCES
4.1-3
4.2 MECHANICAL
DESIGN 4.2-1 4.2.1 FUEL 4.2-2 4.2.1.1 Design Bases 4.2-3 4.2.1.2 Fuel Rods 4.2-3 4.2.1.3 Fuel Assembly Structure 4.2-14 4.2.1.4 Operational Experience 4.2-24 4.2.1.5 Safety Evaluation 4.2-24 4.2.1.6 Tests and Inspections 4.2-25
4.2.2 REACTOR
VESS EL INTERNALS 4.2-26 4.2.2.1 Design Bases 4.2-26 4.2.2.2 Acceptance Criteria 4.2-27 4.2.2.3 Reactor Vessel Internals Description 4.2-28 4.2.2.4 Reactor Vessel Internals Design Evaluation 4.2-32 4.2.2.5 Safety Evaluation 4.2-34
4.2.3 REACTIVITY
CONTROL SYSTEM 4.2-36 4.2.3.1 Design Bases 4.2-36 4.2.3.2 Reactivity Control System Acceptance Criteria 4.2-37 4.2.3.3 Reactivity Control System Description 4.2-39 4.2.3.4 Reactivity Control System Design Evaluation 4.2-47 4.2.3.5 Safety Evaluation 4.2-54 4.2.3.6 Tests and Inspections 4.2-56 4.2.3.7 Instrumentation Applications 4.2-57 4.
2.4 REFERENCES
4.2-58
4.3 NUCLEAR
DESIGN 4.3-1
4.3.1 DESIGN
BASES 4.3-2 4.3.1.1 General Design Criterion 10, 1971 - Reactor Design 4.3-2 4.3.1.2 General Design Criterion 11, 1971 - Reactor Inherent
Protection 4.3-2 4.3.1.3 General Design Criterion 12, 1971 - Suppression of DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title
Page ii Revision 23 December 2016 Reactor Power Oscillations 4.3-2 4.3.1.4 General Design Criterion 25, 1971 - Protection System
Requirements for Reactivity Control Malfunctions 4.3-2 4.3.1.5 General Design Criterion 26, 1971 - Reactivity Control
System Redundancy and Capability 4.3-2 4.3.1.6 General Design Criterion 28, 1971 - Reactivity Limits 4.3-2
4.3.2 NUCLEAR
DESIGN ACCEPTANCE CRITERIA 4.3-3 4.3.2.1 Fuel Burnup 4.3-3 4.3.2.2 Control of Power Distribution 4.3-3 4.3.2.3 Negative Reactivity Feedbacks (Reactivity Coefficients) 4.3-3 4.3.2.4 Stability 4.3-4 4.3.2.5 Maximum Controlled Reactivity Insertion Rate 4.3-4 4.3.2.6 Shutdown Margins 4.3-4 4.
3.3 DESCRIPTION
4.3-4 4.3.3.1 Nuclear Design Description 4.3-4 4.3.3.2 Power Distribution 4.3-6 4.3.3.3 Reactivity Coefficients 4.3-16 4.3.3.4 Control Requirements 4.3-19 4.3.3.5 Control 4.3-22 4.3.3.6 Control Rod Patterns and Reactivity Worths 4.3-24 4.3.3.7 Criticality of Fuel Assemblies 4.3-25 4.3.3.8 Stability 4.3-26 4.3.3.9 Vessel Irradiation 4.3-29 4.3.3.10 Analytical Methods 4.3-30 4.3.4 SAFETY EVALUATION 4.3-34 4.3.4.1 General Design Criterion 10, 1971 - Reactor Design 4.3-34 4.3.4.2 General Design Criterion 11, 1971 - Reactor Inherent
Protection 4.3-35 4.3.4.3 General Design Criterion 12, 1971 - Suppression of Reactor
Power Oscillations 4.3-36 4.3.4.4 General Design Criterion 25, 1971 - Protection System Requirements for Reactivity Control Malfunctions 4.3-37 4.3.4.5 General Design Criterion 26, 1971 - Reactivity Control System Redundancy and Capability 4.3-37 4.3.4.6 General Design Criterion 28, 1971 - Reactivity Limits 4.3-37 DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title
Page iii Revision 23 December 2016
4.
3.5 REFERENCES
4.3-38
4.4 THERMAL
AND HYDRAULIC DESIGN 4.4-1
4.4.1 DESIGN
BASES 4.4-1 4.4.1.1 General Design Criterion 10, 1971 - Reactor Design 4.4-1 4.4.1.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations 4.4-1
4.4.2 THERMAL
AND HYDRAULIC DESIGN ACCEPTANCE CRITERIA 4.4-2 4.4.2.1 Departure from Nucleate Boiling Acceptance Criteria 4.4-2 4.4.2.2 Fuel Temperature Acceptance Criteria 4.4-2 4.4.2.3 Core Flow Acceptance Criteria 4.4-2 4.4.2.4 Hydrodynamic Stability Acceptance Criteria 4.4-2
4.4.3 SYSTEM
DESCRIPTION 4.4-2 4.4.3.1 Summary Comparison 4.4-2 4.4.3.2 Fuel Cladding Temperatures 4.4-2 4.4.3.3 Departure from Nucleate Boiling Ratio 4.4-6 4.4.3.4 Flux Tilt Considerations 4.4-12 4.4.3.5 Void Fraction Distribution 4.4-13 4.4.3.6 Core Coolant Flow Distribution 4.4-13 4.4.3.7 Core Pressure Drops and Hydraulic Loads 4.4-13 4.4.3.8 Correlation and Physical Data 4.4-14 4.4.3.9 Thermal Effects of Operation Transients 4.4-16 4.4.3.10 Uncertainties in Estimates 4.4-16 4.4.3.11 Plant Configuration Data 4.4-18 4.4.3.12 Core Hydraulics 4.4-19 4.4.3.13 Influence of Power Distribution 4.4-21 4.4.3.14 Core Thermal Response 4.4-22 4.4.3.15 Analytical Techniques 4.4-22 4.4.3.16 Hydrodynamic and Flow-Power Coupled Instability 4.4-26 4.4.3.17 Temperature Transient Effects Analysis 4.4-27 4.4.3.18 Potentially Damaging Temperature Effects During Transients 4.4-28 4.4.3.19 Energy Release During Fuel Element Burnout 4.4-29 4.4.3.20 Energy Release During Rupture of Waterlogged Fuel Elements 4.4-29 DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 Reactor CONTENTS Section Title
Page iv Revision 23 December 2016 4.4.3.21 Fuel Rod Behavior Effects from Coolant Flow Blockage 4.4-29
4.4.4 THERMAL
AND HYDRAULIC DESIGN EVALUATION 4.4-30 4.4.4.1 Departure from Nucleate Boiling 4.4-30 4.4.4.2 Fuel Temperature 4.4-31 4.4.4.3 Core Flow 4.4-32 4.4.4.4 Hydrodynamic Stability 4.4-32
4.4.5 SAFETY
EVALUATION 4.4-32 4.4.5.1 General Design Criterion 10, 1971 - Reactor Design 4.4-32 4.4.5.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations 4.4-32
4.4.6 TESTS
AND INSPECTIONS 4.4-33 4.4.6.1 Testing Prior to Initial Criticality 4.4-33 4.4.6.2 Initial Power Plant Operation 4.4-33 4.4.6.3 Component and Fuel Inspections 4.4-33
4.4.7 INSTRUMENTATION
APPLICATIONS 4.4-33 4.4.7.1 Incore Instrumentation 4.4-33 4.4.7.2 Overtemperature and Overpower T Instrumentation 4.4-34 4.4.7.3 Instrumentation to Limit Maximum Power Output 4.4-34
4.
4.8 REFERENCES
4.4-35
DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 TABLES Table Title v Revision 23 December 2016 4.1-1 Reactor Design Comparison
4.1-2 Analytical Techniques in Core Design
4.1-3 Design Loading Condit ions for Reactor Core Components
4.2-1 Deleted in Revision 23
4.3-1 Nuclear Design Parameters (Typical)
4.3-2 Unit 1 - Reactivity Requirements for Rod Cluster Control Assemblies
4.3-3 Unit 2 - Reactivity Requirements for Rod Cluster Control Assemblies
4.3-4 Axial Stability Index PWR Core With a 12-ft Height (Historical)
4.3-5 Typical Neutron Flux Levels (n/cm 2 sec) at Full Power 4.3-6 Comparison of Measured and Calculated Doppler Defects
4.3-7 Benchmark Critical Experiments
4.3-8 Saxton Core II Isotopics, Rod MY, Axial Zone 6
4.3-9 Critical Boron Concentrations, at HZP, BOL
4.3-10 Comparison of Measured and Calculated Rod Worth
4.3-11 Comparison of Measured and Calculated Moderator Temperature Coefficients at HZP, BOL (Historical)
4.4-1 Unit 1 - Void Fractions at Nominal Reactor Conditions with Design Hot Channel Factors
4.4-2 Unit 2 - Void Fractions at Nominal Reactor Conditions with Design Hot Channel Factors.
4.4-3 Comparison of THINC-IV and THINC-I Predictions with Data from Representative Westinghouse Two- and Three-loop Reactors (Historical)
4.4-4 Non-LOCA DNB Analysis Method DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 FIGURES Figure Title vi Revision 23 December 2016 4.2-1 Fuel Assembly Cross Section
4.2-2 Fuel Assembly Outline (LOPAR)
4.2-2A Deleted in Revision 23
4.2-3 Fuel Rod Schematic (LOPAR)
4.2-3A Deleted in Revision 23
4.2-4 Typical Clad and Pellet Dimensions as a Function of Exposure
4.2-5 Representative Fuel Rod Internal Pressure and Linear Power Density for the Lead Burnup Rod as a Function of Time
4.2-6 Removable Rod Compared to Standard Rod (HISTORICAL)
4.2-7 Removable Fuel Rod Assembly Outline (HISTORICAL) 4.2-8 Location of Removable Rods Within an Assembly (HISTORICAL)
4.2-9 Unit 1 - Lower Core Support Assembly
4.2-10 Unit 2 - Lower Core Support Assembly
4.2-11 Unit 2 - Neutron Shield Pad Lower Core Support Structure
4.2-12 Unit 1 - Upper Core Support Structure
4.2-13 Unit 2 - Upper Core Support Structure
4.2-14 Plan View of Upper Core Support Structure
4.2-15 Rod Cluster Control and Drive Rod Assembly with Interfacing Components
4.2-16 Rod Cluster Control Assembly Outline
4.2-17 Absorber Rod
4.2-18 Deleted in Revision 23 DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 FIGURES Figure Title vii Revision 23 December 2016 4.2-18A Wet Annular Burnable Absorber
4.2-19 Deleted in Revision 23
4.2-20 Deleted in Revision 23
4.2-21 Secondary Source Assembly
4.2-21A Deleted in Revision 23
4.2-22 Thimble Plug Assembly
4.2-23 Control Rod Drive Mechanism
4.2-23A Deleted
4.2-24 Control Rod Drive Mechanism Schematic
4.2-24A Deleted
4.2-25 Nominal Latch Clearance at Minimum and Maximum Temperature
4.2-26 Control Rod Drive Mechanism Latch Clearance Thermal Effect
4.3-1 Fuel Loading Arrangement
4.3-2 Production and Consumption of Higher Isotopes
4.3-3 Boron Concentration vs. Cycle Burnup With Burnable Absorber Rods
4.3-4 Burnable Absorber Rod Arrangement Within an Assembly
4.3-5 Typical Integral Fuel Burnable Absorber Rod Arrangement Within an Assembly 4.3-6 Burnable Absorber Loading Pattern
4.3-7 Normalized Power Density Distribution Near Beginning of Life (BOL), Unrodded Core, Hot Full Power, No Xenon
DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 FIGURES Figure Title viii Revision 23 December 2016 4.3-8 Normalized Power Density Distribution Near BOL, Unrodded Core, Hot Full Power, Equilibrium Xenon
4.3-9 Unit 1 - Normalized Power Density Distribution Near BOL, Group D at Insertion Limit, Hot Full Power, Equilibrium Xenon
4.3-10 Unit 2 - Normalized Power Density Distribution Near BOL, Group D at Insertion Limit, Hot Full Power, Equilibrium Xenon
4.3-11 Normalized Power Density Distribution Near Middle of Life (MOL), Unrodded Core, Hot Full Power, Equilibrium Xenon
4.3-12 Normalized Power Density Distribution Near End of Life (EOL), Unrodded Core, Hot Full Power, Equilibrium Xenon
4.3-13 Rodwise Power Distribution in a Typical Assembly (G-10) Near BOL, Hot Full Power, Equilibrium Xenon, Unrodded Core 4.3-14 Rodwise Power Distribution in a Typical Assembly (G-10) Near EOL, Hot Full Power, Equilibrium Xenon, Unrodded Core 4.3-15 Possible Axial Power Shapes at BOL Due to Adverse Xenon Distributions
4.3-16 Possible Axial Power Shapes at MOL Due to Adverse Xenon Distributions
4.3-17 Possible Axial Power Shapes at EOL Due to Adverse Xenon Distributions
4.3-18 Deleted
4.3-19 Deleted
4.3-20 Deleted
4.3-21 Peak Power Density During Control Rod Malfunction Overpower Transients
4.3-22 Peak Linear Power During Boration/Dilution Overpower Transients
DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 FIGURES Figure Title ix Revision 23 December 2016 4.3-23 Maximum Fx Q T Power vs. Axial Height During Normal Operations
4.3-24 Deleted in Revision 23
4.3-25 Comparison Between Calculated and Measured Relative Fuel Assembly Power Distribution
4.3-26 Comparison of Calculated and Measured Axial Shape
4.3-27 Measured Values of F Q T for Full Power Rod Configurations 4.3-28 Doppler Temperature Coefficient at BOL and EOL
4.3-29 Doppler Only Power Coefficient at BOL and EOL
4.3-30 Doppler Only Power Defect at BOL and EOL
4.3-31 Moderator Temperature Coefficient at BOL, No Rods
4.3-32 Moderator Temperature Coefficient at EOL 4.3-33 Moderator Temperature Coefficient as a Function of Boron Concentration at BOL, No Rods
4.3-34 Hot Full Power Moderator Temperature Coefficient for Critical Boron Concentration
4.3-35 Total Power Coefficient at BOL and EOL
4.3-36 Total Power Defect at BOL and EOL
4.3-37 Unit 1 - Rod Cluster Control Assembly Pattern
4.3-38 Unit 2 - Rod Cluster Control Assembly Pattern
4.3-39 Accidental Simultaneous Withdrawal of Two Control Banks EOL, HZP Banks B and D Moving in the Same Plane
4.3-40 Design - Trip Curve
DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 FIGURES Figure Title x Revision 23 December 2016 4.3-41 Normalized Rod Worth vs. Percent Insertion, All Rods But One
4.3-42 Axial Offset vs. Time, PWR Core with a 12-ft Core Height and 121 Assemblies
4.3-43 XY Xenon Test Thermocouple Response Quadrant Tilt Difference vs.
Time 4.3-44 Calculated and Measured Doppler Defect and Coefficients at BOL, for a Two-loop Plant with a 12-ft Core Height and 121 Assemblies
4.3-45 Comparison of Calculated and Measured Boron Concentration for a Two-loop Plant with a 12-ft Core Height and 121 Assemblies
4.3-46 Comparison of Calculated and Measured Boron for a Two-loop Plant with a 12-ft Core Height and 121 Assemblies
4.3-47 Comparison of Calculated and Measured Boron in a Three-loop Plant with a 12-ft Core Height and 157 Assemblies
4.4-1 Peak Fuel Average and Surface Temperatures During Fuel Rod Lifetime vs. Linear Power Density
4.4-2 Peak Fuel Centerline Temperature During Fuel Rod Lifetime vs. Linear Power Density
4.4-3 Thermal Conductivity of UO 2 (Data Corrected to 95% Theoretical Density) 4.4-4 Axial Variation of Average Clad Temperature for Rod Operating at 5.43 kW/ft
4.4-5 Probability Curves for W-3 and R Grid DNB Correlations
4.4-6 TDC vs. Reynolds Number for 26-inch Grid Spacing
4.4-7 Normalized Radial Flow and Enth alpy Distribution at 4-ft Elevation
4.4-8 Normalized Radial Flow and Enth alpy Distribution at 8-ft Elevation
DCPP UNITS 1 &
2 FSAR UPDATE Chapter 4 FIGURES Figure Title xi Revision 23 December 2016 4.4-9 Normalized Radial Flow and Enthalpy Distribution at 12-ft Elevation Core Exit 4.4-10 Void Fraction vs. Thermodynamic Quality H-H SAT/H G-HSAT 4.4-11 PWR Natural Circulation Test
4.4-12 Comparison of a Representative W Two-loop Reactor Incore Thermocouple Measurements with THINC-IV Predictions
4.4-13 Comparison of a Representative W Three-loop Reactor Incore Thermocouple Measurements with THINC-IV Predictions
4.4-14 Hanford Subchannel Temperature Data Comparison With THINC-IV
4.4-15 Hanford Subcritical Temperature Data Comparison With THINC-IV
4.4-16 Unit 1 - Distribution of Incore Instrumentation 4.4-17 Unit 2 - Distribution of Incore Instrumentation
4.4-18 Improved Thermal Design Procedure Illustration
4.4-19 Measured Versus Predicted Critical Heat Flux-WRB-1 Correlation (HISTORICAL)
4.4-20 Measured Versus Predicted Critical Heat Flux-WRB-2 Correlation
DCPP UNITS 1 &
2 FSAR UPDATE 4.1-1 Revision 23 December 2016 Chapter 4 REACTOR This chapter describes the design for the reactors at Diablo Canyon Power Plant (DCPP) Unit 1 and Unit 2, and evaluates their capabilities to function safely under all operating modes expected during their lifetimes.
4.1
SUMMARY
DESCRIPTION This chapter describes the following subjects: (a) the mechanical components of the reactor and reactor core, including the fuel rods and fuel assemblies, reactor vessel internals, and the control rod drive mechanisms (CRDMs), (b) the nuclear design, and (c) the thermal-hydraulic design.
The reactor core of each unit consists of VANTAGE+ fuel assemblies.
The significant mechanical design features of the VANTAGE+ design, as defined in Reference 1, include the following:
- Integral fuel burnable absorber (IFBA)
- Intermediate flow mixer (IFM) grids
- Protective grid assemblies (P-Grid)
- Reconstitutable top nozzle (RTN)
- Axial blanket
- Debris filter bottom nozzle (DFBN)
The core is cooled and moderated by light water at a nominal pressure of 2250 psia to preclude bulk boiling under normal operating condition
- s. The coolant uses boron as a neutron absorber. Boron concentration in the coolant is varied as required to control
relatively slow reactivity changes, such as those associated with the fuel burnup.
Additional boron, in the form of IFBA or burnable absorber rods may be employed to limit the moderator temperature coefficient (MTC) and/or the local power peaking that can be achieved.
A fuel assembly consists of up to 264 mechanically joined fuel rods in a 17 x 17 square
array. The fuel rods are supported at intervals along their length by grid assemblies that
maintain the lateral spacing between the rods throughout the design life of the
assembly. The grid assembly consists of an "egg-crate" arrangement of interlocked
straps. The straps contain springs and dimples for maintaining fuel rod lateral and axial support, as well as mixing vanes at the top of the straps for coolant mixing. The fuel DCPP UNITS 1 &
2 FSAR UPDATE 4.1-2 Revision 23 December 2016 rods consist of enriched UO 2 cylindrical pellets contained in zirconium alloy tubing that is plugged and seal-welded at the ends. To increase fatigue life, all fuel rods are pressurized with helium during fabrication to reduce stress and strain.
The center position of the fuel assembly contains an instrument tube; the remaining 24 positions in the array are equipped with guide thimbles joined to the grids and the top
and bottom nozzles. Depending on assembly position in the core, the guide thimbles
are used as core locations for rod cluster control assemblies (RCCAs), neutron source
assemblies, and burnable absorber rods (if used).
The DFBN is a box-like structure that serves as a bottom structural element of the fuel assembly and directs the coolant flow to the assembly. The pattern and size of the flow holes in the bottom nozzle are designed to reduce the possibility of fuel rod damage due to debris-induced fretting. This feature is discussed in Section 4.2.1.3.2.1.
The top nozzle assembly functions as the upper structural element of the fuel assembly
in addition to providing a partial protective housing for the RCCA or other components.
Each RCCA consists of a group of individual absorber rods fastened at the top end to a
common hub or spider assembly.
The CRDMs for the RCCA are of the magnetic latch type. The latches are controlled by three magnetic coils. Upon a loss of power to the coils, the RCCA is released and falls
by gravity to shut down the reactor.
Components of the reactor vessel internals are divided into three parts: (a) the lower core support structure (including the entire core barrel, the Unit 1 thermal shield, and
the Unit 2 neutron shield pad assembly), (b) the upper core support structure, and (c)
the incore instrumentation support structure.
Reactor vessel internals support the core, maintain fuel alignment, limit fuel assembly movement, maintain alignment between fuel assemblies and CRDMs, direct coolant flow past the fuel assemblies to the pressure vessel head, provide gamma and neutron shielding, and provide guides for incore
instrumentation.
The nuclear design analyses and evaluations establish physical locations for fuel assemblies, control rods, burnable absorber, and physical parameters such as fuel enrichments and boron concentration in the coolant. These characteristics, together
with the reactor control and protection systems and the emergency core cooling system (ECCS), provide adequate reactivity control even if the RCCA with the highest reactivity worth is stuck in the fully withdrawn position ensuring that the reactor performance and safety criteria specified in Section 4.2 are met.
The thermal-hydraulic design analyses and evaluations establish coolant flow parameters that ensure adequate heat transfer between fuel cladding and reactor
coolant. The thermal-hydraulic design takes into account local variations in dimensions, power generation, flow distribution, mixing and the IFM grids in the VANTAGE+ fuel DCPP UNITS 1 &
2 FSAR UPDATE 4.1-3 Revision 23 December 2016 assembly. The mixing vanes incorporated in the fuel assembly spacer grid design induce additional flow mixing between the various flow channels within a fuel assembly
as well as between adjacent assemblies.
Instrumentation is provided in and out of the core to monitor the nuclear, thermal-hydraulic, and mechanical performance of the reactor, and to provide input
signals to control and protection functions and to the plant computer.
Table 4.1-1 presents a comparison of the reactor design parameters for the DCPP Unit 1 and Unit 2 reactor cores fueled with VANTAGE+ fuel assemblies. The analysis techniques employed in the core design are tabulated in Table 4.1-2.
4.
1.1 REFERENCES
- 1. S. L. Davidson (Ed.), et al., VANTAGE+ Fuel Assembly Reference Core Report, WCAP-12610-P-A, April 1995.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-1 Revision 23 December 2016
4.2 MECHANICAL
DESIGN For design purposes, the DCPP conditions are divided into four categories, in accordance with their anticipated frequency of occurrence and risk to the public, as
follows:
(1) Condition I - Normal Operation (2) Condition II - Incidents of Moderate Frequency (3) Condition III - Infrequent Faults (4) Condition IV - Limiting Faults
In general, Condition I occurrences are accommodated with margin between any plant
parameter and the value of that parameter which would require either automatic or
manual protective action. Condition II incidents are accommodated with, at most, a
shutdown of the reactor with the plant capable of returning to operation after corrective
action.
The release of radioactive material due to Condition III incidents should not be sufficient
to interrupt or restrict public use of areas outs ide the exclusion area. Furthermore, a Condition III incident shall not, by itself, generate a Condition IV fault or result in a
consequential loss of function of t he reactor coolant system (RCS) or reactor
containment barriers.
Condition IV occurrences are faults that are not expected to occur, but are defined as limiting faults that must be considered in design. Condition IV faults shall not cause a release of radioactive material that results in an undue risk to public health and safety.
The reactor is designed so that its components meet the following performance and
safety criteria:
(1) The mechanical design of the reactor core components and their physical arrangement, together with corrective actions by the reactor control, protection, and emergency cooling systems (when applicable) ensure that:
(a) Fuel damage is not expected duri ng Conditions I and II events, although a very small number of fuel rod failures is anticipated. This
number of failures is within the capability of the plant cleanup system
and is consistent with the plant design bases. Fuel damage is defined as penetration of the fission product barrier (i.e., the fuel rod cladding).
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-2 Revision 23 December 2016 (b) The reactor can be brought to a safe state following a Condition III event with only a small number of fuel rods damaged, although sufficient fuel damage may occur to preclude resumption of
operation without considerable outage time.
(c) The reactor can be brought to a safe state and the core can be kept subcritical with acceptable heat transfer geometry, following
transients arising from Condition IV events.
(2) The fuel assemblies are designed to withstand loads induced during shipping, handling, and core loading without exceeding the criteria of Section 4.2.1.3.2.5.
(3) The fuel assemblies are designed to accept control rod insertions to provide the reactivity control required for power operations and shutdown
conditions (if in such core locations).
(4) All fuel assemblies have provisions for the insertion of the incore instrumentation necessary for plant operation (if in such core locations).
(5) The reactor vessel internals, in conjunction with the fuel assemblies, direct reactor coolant through the core. This achieves acceptable flow distribution and to restricts bypass flow so that the heat transfer performance requirements can be met for all modes of operation. In
addition, internals provide core support and distribute coolant flow to the
pressure vessel head. The distribution of flow into the vessel head minimizes axial and circumferential temperature gradients, thus precluding excessive rotation or warpage that could result in leakage past the O-ring
gaskets during Conditions I and II operations. Required inservice
inspections can be carried out since the internals are removable and
provide access to the inside of the pressure vessel.
4.2.1 FUEL The fuel assembly and fuel rod design data are listed in Table 4.1-1. U.S. Nuclear Regulatory Commission (NRC) approval of the VANTAGE+ design is given in Reference 29. Figure 4.2-1 shows a cross-section of the fuel assembly array, and Figure 4.2-2 shows a fuel assembly full-length outline. The fuel rods are loaded into the fuel assembly structure so that there is clearance between the fuel rod ends and the top and bottom nozzles.
Each fuel assembly is installed vertically in the reactor vessel and stands upright on the lower core plate, which is fitted with alignment pins to locate and orient the assembly.
After all fuel assemblies are set in place, the upper support structure is installed.
Alignment pins, built into the upper core plate, engage and locate the upper ends of the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-3 Revision 23 December 2016 fuel assemblies. The upper core plate then bears downward against the fuel assemblies' top nozzles, via the holddown springs, to hold the fuel assemblies in place.
4.2.1.1 Design Bases 4.2.1.1.1 General Design Criterion 2, 1967 - Performance Standards The reactor core is designed to withstand, without fuel and/or clad damage that could interfere with continued effective core cooling, the ef fects of, or is protected against, natural phenomena such as earthquakes.
4.2.1.1.2 General Design Criterion 10, 1971 - Reactor Design The fuel is designed with appropriate margin to assure that specified acceptable fuel design limits (SAFDLs) are not exceeded during any condition of normal operation, including the effects of anticipated operational occurrences.
4.2.1.1.3 Safety Function Requirements (1) Loads During Handling The fuel assemblies are designed to accommodate conditions expected to exist as a result of handling during assembly, inspection, and refueling operations, as well as shipping loads.
4.2.1.1.4 10 CFR 50.46(b)(4) - Coolable Geometry The fuel is designed with appropriate margin to assure that following a postulated loss-of-coolant accident (LOCA) the calculated core geometry remains amenable to cooling by the ECCS. The calculated core geometry allows adequate ECCS cooling to assure the peak cladding temperature does not exceed 2200F and the maximum cladding oxidation nowhere exceeds 0.17 times the to tal cladding thickness before the start of significant oxidation during the event.
4.2.1.2 Fuel Rods 4.2.1.2.1 Fuel Rods Acceptance Criteria To meet GDC 10, 1971 and ensure their integrity, fuel rods are designed to prevent excessive fuel temperatures, excessive internal gas pressures due to fission gas
buildup, and excessive cladding stresses and strains. To this end, the following conservative design bases are adopted for Condition I and Condition II events: (1) Fuel Pellet Temperatures - The center temperature of the hottest pellet is to be below the melting temperature of the UO
- 2. The melting point of un-irradiated UO 2 is 5080°F (Reference 1). Irradiation reduces the melting point of UO 2 by 58°F per 10,000 megawatt days/metric ton of uranium DCPP UNITS 1 &
2 FSAR UPDATE 4.2-4 Revision 23 December 2016 (MWD/MTU). While a limited amount of center melting can be tolerated, the design conservatively precludes center melting. A calculated
centerline fuel temperature of 4700°F has been selected as the overpower
limit. This provides sufficient margin for uncertainties.
(2) Internal Gas Pressure - The fuel rod internal gas pressure remains below the value that can cause the fuel-cladding diametral gap to increase due
to outward cladding creep during steady state operation. Rod pressure is
also limited so that extensive departure from nucleate boiling (DNB)
propagation does not occur during normal operation and accident events (Reference 14). Also, cladding fla ttening (Reference 15) will not occur during the fuel rod incore life.
(3) Cladding Stress and Strain - The design limit for the fuel rod clad strain is the total plastic tensile creep strain due to:
- uniform clad creep,
- uniform cylindrical fuel pellet expansion due to swelling, and
- thermal expansion is less than 1% from the un-irradiated condition.
The design limit for the fuel rod clad stress is that the volume average effective stress calculated with the von Mises equation considering interference due to uniform cylindrical pellet-clad contact, caused by:
- pellet thermal expansion,
- pellet swelling and uniform clad creep, and
- pressure differences is less than the ZIRLO 0.2% offset yield stress, with due consideration to temperature and irradiation effects under Condition I and Condition ll events. While the clad has some capability for accommodating plastic strain, the yield stress has been established as a conservative design limit.
(4) Cladding Tensile Strain - The total tensile strain due to uniform cylindrical pellet thermal expansion during a transient is less than 1% from the pre-transient value.
(5) Strain Fatigue - The fuel system will not be damaged due to excessive clad fatigue. The fatigue life usage factor is limited to less than 1.0 to prevent reaching the material fatigue limit.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-5 Revision 23 December 2016 (6) Fuel Clad Oxidation and Hydriding - Fuel rod damage will not occur due to excessive clad oxidati on and hydriding. In order to limit metal-oxide formation to acceptable values, the ZIRLO metal-oxide interface temperature is limited for Condition I and Condition II events. The clad and structural component hydrogen pickup is limited at end of life (EOL) to preclude loss of ductility due to hydrogen embrittlement by the formation of zirconium hydride platelets.
(7) Fuel Clad Wear - The fuel system will not be damaged due to fuel rod clad fretting. A design wall thickness reduction of 10% is a general guide in evaluating clad imperfections including fretting wear marks.
(8) Fuel Clad Flattening - Fuel clad flattening is the long-term creep collapse of the fuel rod into the axial gap between fuel pellet columns. No clad flattening occurs in Westinghouse fuel designs (Reference 33).
(9) Fuel Rod Axial Growth - The fuel rods will be designed with adequate clearance between the fuel rod ends and the top and bottom nozzles to accommodate the differences in the growth of fuel rods and the growth of the fuel assembly.
The preceding fuel rod acceptance criteria and other supplementary fuel design criteria/limits are given in Reference 29. Reference 25 provides the methodology for peak rod burnup in excess of 50,000 MWD/MTU. The above requirements impact design parameters such as pellet size and density, cladding-pellet diametral gap, gas
plenum size, and helium pre-pressurization. The design also considers effects such as fuel density changes, fission gas release, cladding creep, and other physical properties
that vary with burnup.
An extensive irradiation testing and fuel surveillance operational experience program has been conducted to verify the adequacy of the fuel performance and design bases.
This program is discussed in Section 4.2.1.4.
4.2.1.2.2 Fuel Rods Description The fuel rods consist of zirconium alloy tubing that is plugged and seal-welded at the ends. The VANTAGE+ fuel rods contain enr iched uranium dioxide fuel pellets and may also include axial blan ket (natural or enriched uranium dioxide) pellets, and/or an IFBA coating on some of the enriched fuel pellets. The VANTAGE + design is capable of achieving extended burnup operation. Fuel rod schematics are shown in Figure 4.2-3.
The fuel pellets are right circular cylinders consisting of uranium dioxide powder that has been compacted by cold pressing and then sintered to the required density. The ends of each pellet are dished slightly to allow greater axial expansion at the center of
the pellets.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-6 Revision 23 December 2016 The axial blanket reduces power at the ends of the rods and causes a slight increase in axial power peaking. Axial blankets reduce neutron leakage and improve fuel utilization.
Certain fuel assemblies utilize annular fuel pellets in the axial blanket region of the fuel rods. The use of this feature provides additional margin to the fuel rod internal pressure design limits. The axial blankets typically ar e a nominal 6 inches of natural or enriched fuel pellets at each end of the fuel rod pellet stack. However, the option exists to increase the top axial blanket length to a nominal 7 inches. The axial blankets utilize pellets, which are physically different from the non-axial blanket pellets to prevent accidental mixing during manufacturing.
The IFBA coated fuel pellets are identical to the enriched uranium dioxide pellets except for the addition of a thin ZrB 2 coating on the pellet cylindrical surface. Coated pellets may occupy the central portion of the fuel column. The number and pattern of IFBA rods within an assembly may vary depending on specific application. An evaluation and test program for the IFBA design features is given in Section 2.5 in Reference 26.
The IFBA flattens the axial po wer distribution and reduces the local peaking as it burns out during irradiation. The net result of axial blankets and IFBA is a slight increase in power peaking during core operation.
The new fuel regions incorporate assemblies whose non-IFBA rods contain fully enriched solid fuel pellets in the blanket region.
All fuel rods are internally pressurized with helium during the welding process to minimize compressive cladding stresses and creep due to coolant operating pressures.
Fuel rod pressurization depends on the planned fuel burnup, as well as other fuel design parameters and fuel characteristics. To avoid overstressing of the cladding or seal welds, void volume and clearances are provided within the rods to accommodate fission gases released from the f uel, differential thermal expansion between the cladding and the fuel, and fuel density changes during burnup. Shifting of the fuel within the cladding during handling or shipping pri or to core loading is prevented by a helical spring within the fuel rod that bears on top of the fuel.
4.2.1.2.2.1 Materials - Fuel Cladding VANTAGE+ fuel has ZIRLO fuel cladding. Reference 29 provides additional details on ZIRLO fuel cladding.
Metallographic examination of irradiated co mmercial fuel rods has shown occurrences of fuel/cladding chemical interaction. Reaction layers of 1 mil in thickness have been observed between fuel and cladding at limited points around the circumference. These data give no indication of propagation of the layer and eventual cladding penetration.
Stress corrosion cracking is another postulated phenomenon related to fuel/cladding chemical interaction. Out-of-reactor tests have shown that in the presence of high cladding tensile stresses, large concentrations of iodine can chemically attack the fuel DCPP UNITS 1 &
2 FSAR UPDATE 4.2-7 Revision 23 December 2016 cladding and lead to eventual cladding cracking. Westinghouse has no evidence that this mechanism is operative in commercial fuel.
4.2.1.2.2.2 Materials - Fuel Pellets Sintered, high-density UO 2 reacts only slightly with the cladding at core operating temperatures and pressures. In the event of cladding defects, the high resistance of uranium dioxide to attack by water protects against fuel deterioration, although limited fuel erosion can occur. Operating experien ce and extensive experimental work reveal that the thermal design parameters conservatively account for changes in the thermal performance of the fuel elements due to pellet fracture that may occur during power operation. The consequences of defects in the cladding are greatly reduced by the ability of uranium dioxide to retain fission products, including those that are gaseous or highly volatile.
Improvements in fuel fabrication techniques, based on extensive analytical and experimental work (References 9 and 33), have eliminated or minimized the fuel pellet densification effect that had previously been observed in fuel irradiated in operating Westinghouse pressurized water reactors (PWRs) (References 5 and 8).
Fuel densification is considered in the nuclear and thermal-hydraulic design of the reactor, as described in Sections 4.3.3.2.5 and 4.4.3.2.1, respectively.
Some fuel pellets are fabricated with a thin boride coating on the pellet outside surface for reactivity control (refer to Section 4.2.1.2.2).
4.2.1.2.2.3 Materials - Strength Considerations One of the most important limiting factors in fuel element duty is the mechanical interaction of fuel and cladding. This fuel-cl adding interaction produces cyclic stresses and strains in the cladding, and these in turn consume cladding fatigue life. To reduce fuel-cladding interaction, which is a principal goal of design, and enhance the cyclic operational capability of the fuel rod, pre-pressurized fuel rods are used.
Pre-pressurized fuel rods partially offset the effect of the coolant external pressure and reduce the rate of cladding creep toward the surface of the fuel. Fuel rod pre-pressurization delays the time at which subs tantial fuel-cladding interaction and hard contact occur. This significantly reduces the number and extent of cyclic stresses and strains experienced by the cladding, both before and after fuel-cladding contact. These factors increase the fatigue life margin of the cladding and lead to greater cladding reliability. If gaps should form in the fuel stacks, cladding flattening will be prevented by the rod pre-pressurization so that the flattening time will be greater than the fuel core life.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-8 Revision 23 December 2016 To minimize fuel-cladding interaction during startup, f ollowing handling of irradiated fuel assemblies during a refueling, or a cold shutdown, limitations in power increase rates are instituted.
4.2.1.2.2.4 Steady State Performance Evaluation In the calculation of the steady state performance of a nuclear fuel rod, the following interacting factors must be considered:
(1) Cladding creep and elastic deflection (2) Pellet density changes, ther mal expansion, gas release, and thermal properties as a function of temperature and fuel burnup (3) Internal pressure as a function of fission gas release, rod geometry, and temperature distribution These effects are evaluated using the fuel rod design model of Reference 34. The model modifications for time-dependent fuel densification are given in Reference 34.
The model determines fuel rod performance characteristics for a given rod geometry, power history, and axial power shape. In particular, internal gas pressure, fuel and cladding temperatures, and cladding deflections are calculated. The fuel rod is divided lengthwise into several sections and radially into a number of annular zones. Fuel density changes, cladding stresses, strains and deformations, and fission gas releases are calculated separately for each segment. These effects are then integrated to obtain the total internal pressure.
Subject to the design criteria of Section 4.2.1.2.1, the initial rod internal pressure is selected to delay fuel-cladding mechanical interaction and to avoid the potential for flattened rod formation.
The gap conductance between the pellet surface and the cladding inner diameter is calculated as a function of the composition, temperature, and pressure of the gas mixture, and the gap size or contact pressure between cladding and pellet. After computing the fuel temperature for each pellet's annular zone, the fractional fission gas release is calculated based on local fuel temperature and burnup. Finally, the gas released is summed over all zones and the pressure is calculated.
The PAD 4.0 code shows good agreement in fit for a variety of published and proprietary data on fission gas release, fuel temperatures, and cladding deflection (Reference 34). Included in this spectrum are variations in power, time, fuel density, and geometry.
Typical fuel cladding inner diameter and the fuel pellet outer diameter as a function of exposure are presented in Figure 4.2-4.
The cycle-to-cycle changes in the pellet outer diameter represent the effects of power changes as the fuel is moved into different DCPP UNITS 1 &
2 FSAR UPDATE 4.2-9 Revision 23 December 2016 positions during refueling. The gap size at any time is given by the difference between cladding inner radius and pellet outer radius. Total cladding-pellet surface contact occurs between 600 and 800 effective full power days (EFPD). Figure 4.2-4 represents hot fuel dimensions for a fuel rod operating at the power level shown in Figure 4.2-5.
Figure 4.2-5 also illustrates representative fuel rod internal gas pressure and linear power for the lead burnup rod versus irradiation time. In addition, it outlines the typical operating range of internal gas pressures that is applicable to the total fuel rod population within a region. The plenum height of the fuel rod, in conjunction with other characteristics, is designed to ensure that the maximum internal pressure of the fuel rod remains below the value that causes the fuel-cladding diametral gap to increase due to outward cladding creep (Reference 29).
Cladding stresses during steady state operation are low. Compressive stresses are created by the pressure differential between the coolant pressure and the rod internal gas pressure.
The design fuel rod internal pressure limit which precludes gap increase is up to 1150 psi above system pressure for ZIRLO rods, based on the ZIRLO creep rate.
Stresses due to the temperature gradient are not included because their contribution to the cladding volume average stress is small and decreases with time during steady state operation due to stress relaxation. The stress due to pressure differential is highest in the minimum power rod at the beginning of life (BOL) (due to low internal gas pressure), and the thermal stress is highest in the maximum power rod (due to the steep radial temperature gradient).
Tensile stresses could be created once the cladding comes in contact with the pellet.
These stresses would be induced by the fuel pellet swelling during irradiation. As shown in Figure 4.2-4, there is very limited cladding pushout after pellet-cladding contact. Fuel swelling can result in small cladding strains (<1% for expected discharge burnups but the associated cladding stresses are very low because of cladding creep thermal and irradiation-induced creep). The 1% strain criterion is extremely conservative for fuel-swelling driven cladding strain because the strain rate associated with solid fission products swelling is very slow.
4.2.1.2.2.5 Transient Evaluation Method The PAD 4.0 code (Reference 34) is the principal design tool for fuel rod performance evaluations. PAD 4.0 iteratively calculates the interrelated effects of temperature, pressure, cladding elastic and plastic behavior, fission gas release, and fuel densification and swelling as a function of time and linear power as a function time and linear power.
Westinghouse uses the PAD 4.0 code to show that the VANTAGE+ fuel design meets pellet cladding interaction (PCI) acceptance criteria, 1) less than 1% transient-induced cladding strain, and 2) no centerline fuel melting. The NRC has found PAD 4.0 acceptable for application to the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-10 Revision 23 December 2016 VANTAGE+ design with changes in the cladding creep model for ZIRLO cladding and changes in the rod growth model for the rod pressure calculation (Reference 34).
Pellet thermal expansion due to power incr eases in a fuel rod is considered the only mechanism by which significant stresses and strains can be imposed on the cladding.
Such power increases in commercial reactors can result from fuel shuffling, reactor power escalation following extended reduced power operation, and control rod movement. In the mechanical design model, depletion of lead rods is calculated using best estimate power histories as determined from core physics calculations. During the depletion, the diametral gap closure is evaluated using the pellet expansion-cracking model, cladding creep model, and fuel swelli ng model. At various times during the depletion, the power is increased locally on the rod to the burnup-dependent attainable power density, as determined by core physics calculation. The radial, tangential, and axial cladding stresses resulting from the power increase are combined into a volume average effective cladding stress.
The von Mises' criterion, described in Section 4.2.1.2.3, is used to determine if the cladding yield stress has been exceeded. The yield stress correlation is that for irradiated cladding, since fuel-cladding interaction occurs at high burnup. Furthermore, the effective stress is increased by an allowance that accounts for stress concentrations in the cladding adjacent to radial cracks in the pellet, prior to the comparison with the yield stress. This allowance was evaluated using a two-dimensional (r, ) finite element model. Since slow transient power increases can result in large cladding strains without exceeding the cladding yield stress due to cladding creep and stress relaxation, a criterion on allowable cladding positive strain is necessary. Based on high strain rate burst and tensile test data for irradiated tubing, 1 percent strain was adopted as the lower limit on irradiated cladding ductility.
It is recognized that a possib le limitation to the satisfactory behavior of the fuel rods in a reactor that is subjected to daily load follow is the failure of the cladding by low cycle strain fatigue. During their normal residence time in a reactor, the fuel rods may be subjected to 1000 cycles with typical changes in power level from 50 to 100 percent of their steady state values.
The ZIRLO cladding fatigue analyses have been performed using the Zircaloy-4 fatigue model. Fatigue properties of materials can be generally correlated with tensile properties, and are frequently described in terms of the fatigue ratio, defined as the ratio of the fatigue limit to the tensile strength.
While the ratio is considered to be an approximation, it can serve as a useful tool to predict fatigue properties within a given alloy system. At room temperature, ZIRLO cladding has an average tensile strength equivalent to Zircaloy-4 cladding. At elevated temperatures, ZIRLO cladding has a higher tensile strength than Zircaloy-4 cladding. On this basis, it is conservative to assume that the fatigue properties of ZIRLO cladding are equivalent to those of Zircaloy-4 cladding, and that on a best estimate basis, ZIRLO cladding has a higher fatigue strength than does Zircaloy-4 cladding at elevated temperatures.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-11 Revision 23 December 2016 The evaluation of the fatigue life usage factor for extended burnup operation conservatively assumes daily load follow operation over the life of the fuel rod, plus ten (10) cold shutdowns per cycle. The Westinghouse fuel performance code, PAD 4.0, (Reference 34) is used to determine the strain range for the fatigue life usage analysis.
PAD 4.0, is used to determine the strain range for the fatigue usage analysis of the VANTAGE+ fuel design. The Langer-O'Donnell fatigue model is used with the calculated strains from PAD 4.0 to assure that the above criterion is met for VANTAGE+. The Westinghouse analytical approach to strain fatigue results from evaluating several strain-fatigue models and the results of the Westingho use experimental programs. In conclusion, the approach defined by Langer-O'Donnell (Reference 12) was retained, and the empirical factors of their correlation were modified to conservatively bound the results of the Westinghouse testing program.
The Langer-O'Donnell empirical correlation has the following form:
e SRA100 100 ln 4 f N E a S+= (4.2-1) where: S a = 1/2 E = pseudo-stress amplitude that causes failure in N f cycles, lb/in 2 = total strain range, in./in E = Young's Modulus, lb/in 2 N f = number of cycles to failure RA = reduction in area at fracture in a uniaxial tensile test, %
S e = endurance limit, lb/in 2 Both RA and S e are empirical constants that depend on the type of material, the temperature, and the irradiation.
The results of the Westinghouse test programs provided information on different cladding conditions, including the effect of irradiation, hydrogen level, and temperature.
The Westinghouse design equations followed the concept for the fatigue design criterion according to the ASME BPVC Section III, namely:
(1) The calculated pseudo-stress amplitude (Sa) includes a safety factor of 2.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-12 Revision 23 December 2016 (2) The allowable cycles for a given Sa are 5 percent of Nf or a safety factor of 20 on cycles.
The lesser of the two allowable n umbers of cycles is selected. The cumulative fatigue life fraction is then computed as:
k fk k N n 1 1 (4.2-2) where: n k = number of diurnal cycles of mode k 4.2.1.2.3 Fuel Rod Design Evaluation
The fuel rod design ensures that the design bases are satisfied.
(1) Fuel Pellet Temperatures - The temperature of the VANTAGE+ fuel pellets is evaluated by the same methods as are used for all Westinghouse fuel designs. Rod geometries, thermal properties, heat fluxes, and temperature differences are modeled to calculate the temperature at the surface and centerline of the fuel pellets. Fuel centerline temperatures are calculated as a function of local power and rod burnup. To preclude fuel melting, the peak local power experienced during Condition I and Condition II events can be limited to a maximum value which is sufficient to ensure that the fuel centerline temperatures remain below the melting temperature at all burnups. Design scoping evaluations for Condition I and Conditio n II events show that fuel melting will not occur for achievable local powers and extended burnups (refer to Section 4.2.1.2.1).
(2) Internal Gas Pressure - The rod internal pressure of the VANTAGE+ fuel rod is evaluated in the same manner as is used for other Westinghouse fuel types. Gas inventories, gas temperature, and rod internal volumes are modeled and the resulting rod internal pressure is compared to the design limit. VANTAGE+ design evaluations to extended burnup levels verify that the fuel rod internal pressure as calculated will meet the design basis. This evaluation is discussed in detail in Appendix B, Section B.2.2 of Reference 29.
(3) Cladding Stress and Strain - Radial, tangential, and axial stress components due to pressure differential and fuel cladding contact pressure are combined into an effective stress using the maximum-distortion-energy theory. The von Mises criterion (Reference
- 22) is used to evaluate whether or not the yield strength has been exceeded. The criterion states that an isotropic material under multiaxial DCPP UNITS 1 &
2 FSAR UPDATE 4.2-13 Revision 23 December 2016 stress will begin to yield plastically when the effective stress (i.e., combined stress using maximum-distortion-energy theory) becomes equal to the material yield stress in simple tension, as determined by a uniaxial tensile test. Since general yielding is prohibited, the volume average effective stress determined by integrating across the cladding thickness is increased by an allowance for local nonuniformity effects before the stress is compared to the yield strength. The yield strength correlation is appropriate for irradiated cladding since the irradiated properties are attained at low exposure, whereas the fuel/cladding interaction conditions, which can lead to minimum margin to the design basis limit, always occur at much higher exposures. The clad stresses in the VANTAGE+ fuel rod clad caused by power transients are evaluated (refer to Section 4.2.1.2.2.5). These evaluations show that the clad stresses and clad strains for VANTAGE+ fuel rod designs (IFBA and non-IFBA) meet the design limits.
(4) Cladding Tensile Strain -
Section 4.2.1.2.2.5 shows that the cladding tensile strain stresses for the VANTAGE+ fuel rod designs meet the design limits.
(5) Strain Fatigue - Clad fatigue for the VANTAGE+ fuel rod design is evaluated by the same methods as are used for other Westinghouse fuel designs. Computer modeling of the fuel rod simulates a daily load follow cycling scheme 100-15-100% power and 12-3-6-3 hour intervals for residence times of more than 60 months.
Design evaluations have shown that the cumulative fatigue usage factor for the VANTAGE+ fuel rod will meet the design criterion. Details regarding this evaluation are presented in Reference 29, Section B.2.3.
(6) Fuel Clad Oxidation and Hydriding - The clad surface temperature and hydriding of the VANTAGE+ fuel rod is evaluated by the same methods as are used for other Westinghouse fuel designs. The coolant temperature rise over the length of the fuel rod and temperature rise through the film, crud and oxide layer are calculated and the temperature at the metal-oxide interface is determined. Calculations show that the clad surface temperature and hydriding of the VANTAGE+ fuel rod meet the design limits. (7) Fuel Clad Wear - The design criteria with regard to clad fretting wear are met for VANTAGE+ to its design burnup. Details regarding this evaluation are presented in Reference 29, Section B.2.5.1.
(8) Fuel Clad Flattening - Calculations for VANTAGE+ fuel show that predicted clad flattening time exceeds residence times expected for extended burnup fuel management.
The evaluation is discussed in detail in Reference 29, Section B.2.4.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-14 Revision 23 December 2016 (9) Fuel Rod Axial Growth - The fuel assembly design is sized to provide sufficient fuel-rod-to-nozzle gaps, as discussed in Reference 29, Section 2.3.1.1. Sufficient top and bottom nozzle-to-fuel rod gaps are provided to assure that fuel rod growth is accommodated during the fuel design lifetime.
4.2.1.3 Fuel Assembly Structure 4.2.1.3.1 Fuel Assembly Structure Acceptance Criteria 4.2.1.3.1.1 Fuel Assembly Structural Integrity The VANTAGE+ fuel assembly must maintain its structural integrity in response to seismic and LOCA loads (refer to Sections 3.7.3.15.2 and 4.2.1.5.4). The stresses and deformations due to various loads on the fuel assemblies are discussed in Section 4.2.1.3.2.5, including the effects of Seismic/LOCA loads..
4.2.1.3.1.2 Fuel Assembly Shipping and Handling Loads The design acceleration limit for the fuel assembly handling and shipping loads is 4g's minimum. 4.2.1.3.1.3 Top Nozzle The top nozzle is required to transmit 4g shipping and handling loads without permanent deformation. The joints must transmit the same loads and be capable of disconnecting using a special disassembly tool.
4.2.1.3.1.4 Fuel Assembly Holddown Springs The fuel assembly holddown springs, Figure 4.2-2, are designed to keep the fuel assemblies resting on the lower core plate under transients associated with Condition I and Condition II events with the exception of the turbine overspeed transient associated with a loss of external load. The holddown springs are designed to tolerate the possibility of a deflection associated with fuel assembly liftoff for this case and provide contact between the fuel assembly and the lower core plate following this transient. . 4.2.1.3.2 Fuel Assembly Structure Description The fuel assembly structure consists of a bottom nozzle, top nozzle, guide thimbles, and
grids, as shown in Figure 4.2-2.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-15 Revision 23 December 2016 4.2.1.3.2.1 Bottom Nozzle The bottom nozzle is a box-like structure that serves as a bottom structural element of
the fuel assembly and directs the coolant flow distribution to the assembly. The square
nozzle is fabricated from Type 304 stainless steel. The legs form a plenum for the inlet
coolant flow. The plate prevents a downward ejection of the fuel rods. The bottom
nozzle is fastened to the fuel assembly guide tubes by locked screws that penetrate
through the nozzle and mate with an inside fitting in each guide thimble tube.
The bottom nozzle design, known as the DFBN, reduces the possibility of fuel rod damage due to debris-induced fretting. The holes in the bottom nozzle plate are sized to minimize passage of debris particles large enough to cause damage while providing
sufficient flow area, comparable pressure drop, and continued structural integrity of the
nozzle. Tests to measure pressure drop and demonstrate structural integrity have been
performed to verify that the DFBN meets the applicable mechanical design criteria for both Condition I and Condition II events.
The bottom nozzle design has a reconstitution feature that permits remote unlocking, removing, and relocking of the thimble screws. Coolant flow through the fuel assembly is directed from the plenum in the bottom nozzle upward through the penetrations in the plate to the channels between the fuel rods.
The weight and axial loads (holddown) imposed on the fuel assembly are transmitted through the bottom nozzle to the lower core plate. Indexing and positioning of the fuel
assembly is controlled by alignment holes in two diagonally opposite bearing plates that mate with locating pins in the lower core plate. Any lateral loads on the fuel assembly are transmitted to the lower core plate through the locating pins.
Westinghouse has developed the standardized debris filter bottom nozzle (SDFBN) for use on its 17x17 fuel designs, including the 1 7x17 VANTAGE+ fuel design. The SDFBN improves the debris mitigation performance of the bottom nozzle by eliminating the side skirt communication flow holes. This nozzle has been evaluated and meets all of the applicable mechanical design criteria. In addition, there is no adverse effect on the
thermal hydraulic performance of the SDFBN either with respect to the pressure drop or
with respect to DNB. The SDFBN was imple mented at Diablo Can yon beginning with Unit 2 Region 20 (Cycle 18 feed) and Unit 1 Region 21 (Cycle 19 feed).
4.2.1.3.2.2 Top Nozzle The RTN assembly functions as the upper structural element of the fuel assembly in addition to providing a partial protective housing for the RCCA. It consists of an adapter plate, enclosure, top plate, and pads. The integral welded assembly has holddown
springs mounted on the assembly, as shown in Figure 4.2-2. The springs are made of
Inconel 718. The other components are made of Type 304 stainless steel.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-16 Revision 23 December 2016 The square adapter plate is provided with round penetrations and semicircular-ended slots that permit the flow of coolant upward through the top nozzle. Other round holes are provided to accept sleeves that are welded to the adapter plate and mechanically attached to the thimble tubes. The ligaments in the plate cover the tops of the fuel rods and prevent their upward ejection from the fuel assembly. The enclosure is a box-like structure that sets the distance between the adapter plate and the top plate. The top plate has a large square hole in the center to permit access for the control rods and the control rod spiders. Holddown springs are mounted on the top plate and are fastened in place by bolts and clamps located at two diagonally opposite corners. The Westinghouse integral nozzle (WIN) design provides a wedged joint for transfer of the fuel assembly hold-down forces into the top nozzle structure. On the other two corners, integral pads contain alignment holes to locate the upper end of the fuel assembly.
In the removable top nozzle design, a stainless steel nozzle insert is mechanically connected to the top nozzle adapter plate by means of a pre-formed circumferential bulge near the top of the insert. The insert engages a mating groove in the wall of the adapter plate thimble tube thru-hole. The insert has 4 equally spaced axial slots which allow the insert to deflect inwardly at the elevation of the bulge thus permitting the installation or removal of the nozzle. The insert bulge is positively held in the adapter plate mating groove by placing a lock tube, with a uniform ID identical to that of the thimble tube, into the insert. The lock tube is secured in place by locally deforming it into the concave side of the bulge in the insert.
The full complement of these joints comprises the structural connection between the top nozzle and the remainder of the fuel assembly. The nozzle insert-to-adapter plate bulge joints replace the uppermost grid sleeve-to-adapter plate welded joints found in current fuel assemblies. The nozzle insert-to-thimble tube multiple 4-lobe bulge joint located in the lower portion of the insert represents the structural connection between the insert and the remainder of the fuel assembly below the elevation of the insert.
4.2.1.3.2.3 Guide and Instrument Thimbles Guide thimbles are structural members that also provide channels for the neutron
absorber rods, burnable poison rods, or neutron source assemblies. Each guide
thimble is fabricated from zirconium alloy tubing having two different diameters. The
larger tube diameter at the top provides the annular area necessary to permit rapid insertion of the control rods during a reactor trip. The lower portion of the guide thimble has a reduced diameter to produce a dashpot action near the end of the control rod travel during a reactor trip. Four holes are provided on the thimble tube above the dashpot to reduce the rod drop time. The dashpot is closed at the bottom by an end plug and thimble screw that is provided with a small flow port to avoid fluid stagnation in the dashpot volume during normal operation.
The central instrumentation tube, fabricated from zirconium alloy tubing, is constrained by its seating in counterbores of each nozzle. Incore neutron detectors pass through
the bottom nozzle's large counterbore into the center instrumentation tube.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-17 Revision 23 December 2016 The VANTAGE+ guide thimble tube ID provides an adequate nominal diametral clearance of 0.061 inches for the control rods. The VANTAGE+ thimble tube ID also provides sufficient diametral clearance for burnable absorber rods, source rods, and
dually compatible thimble plugs.
The VANTAGE+ instrumentation tube allow s sufficient diametral clearance for the flux thimble to traverse the tube without binding.
4.2.1.3.2.4 Grid Assemblies The fuel rods, as shown in Figure 4.2-2, are supported laterally at eight intervals along
their length by grid assemblies that maintain the lateral spacing between the rods by the
combination of support dimples and springs. The grid assembly consists of individual
slotted straps interlocked and brazed or welded in an "egg-crate" arrangement to join the straps permanently at their points of intersection. The straps contain springs and support dimples. The outside straps on all grids contain mixing vanes which, in addition to their mixing function, help guide the grids and fuel assemblies past projecting surfaces during fuel handling or core loading and unloading.
Inconel 718 and zirconium alloys were chosen as the grid materials because of corrosion resistance, neutron economy, and high strength properties. The grids are connected to the thimble tube with 4-lobe bulge joints similar to the top nozzle (refer to Section 4.2.1.3.2.2). The magnitude of the grid restraining force on the fuel rod is set high enough to minimize possible fretting, without overstressing the cladding at the
points of contact. The grid assemblies also allo w axial thermal expansion of the fuel rods to prevent their buckling or distortion.
VANTAGE+ fuel assemblies have four types of grid assemblies: top and bottom grids, Mid-grids, IFM grids, and protective grids (P-Grid). Each fuel assembly has a total of twelve grids: one bottom and one top grid, six Mid-grids, three IFM grids, and one P-Grid. The most critical grids from a standpoint of preventing fretting of fuel rods are the bottom and top grids (i.e., the end grids). The bottom and top grid assemblies do not include mixing vanes on the inner straps. The material of these grid assemblies is Inconel 718, chosen because of its corrosion resistance and high strength. These grid assemblies, being at the ends of the fuel assembly, are in the lower flux regions of the fuel assembly.
The Mid-grid assemblies consist of zirconium alloy straps arranged as described above and permanently joined by welding at their points of intersection. This material is primarily chosen for its low neutron absorption properties. These grids are used in the high heat flux region of the fuel assemblies. The inner straps include mixing vanes that project into the coolant stream and promote mixing of the coolant.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-18 Revision 23 December 2016 The IFM grids, as shown in Figure 4.2-2, are located between the three uppermost spans between the Mid-grids and incorporate a similar mixing vane array. Their prime function is mid-span flow mixing in the hottest fuel assembly spans. Each IFM grid cell contains four dimples which are designed to prevent mid-span channel closure in the spans containing IFMs and fuel rod contact with the mixing vanes. This simplified cell arrangement allows short grid cells so that the IFM can accomplish its flow mixing objective with minimal pressure drop. The IFM grids are fabricated from Zircaloy. This material was selected to take advantage of the material's inherent low neutron capture cross-section.
The P-Grid, configured with the same egg crate support matrix and other internal structures as the other grid assemblies, is added to the bottom of the fuel assembly to provide an additional debris barrier thereby improving fuel reliability. This protective or P grid is thinner (i.e., shorter) th an the normal grid to accommodate the gap between the bottom nozzle and the fuel rods. It has no mixing vanes and has shorter inner
straps comprising the support matrix compared to the top and bottom grids. The P-Grid is composed of Inconel 718 material.
4.2.1.3.2.5 Stresses and Deflections
Structural integrity of fuel assemblies is ensured by setting limits on stresses and deformations due to various loads, and by determining that the assemblies do not interfere with other components' functionality.
These stress and deformation limits are applied to the design and evaluation of the top and bottom nozzles, the guide thimbles, the grids, and the thimble joints.
The design bases for evaluating the structural integrity of the fuel assemblies are:
(1) Nonoperational - 4g minimum lateral loading with dimensional stability in both lateral and axial directions.
(2) Normal Operation (Condition I) and Incidents of Moderate Frequency (Condition II). The fuel assembly component structural design criteria are classified into two material categories: austenitic steels and zirconium alloys. Although not strictly fuel assembly components, reactor core elements that are made of stainless steel and are closely related to the fuel assembly design include the top and bottom nozzle, the RCCA cladding, and some burnable absorber rod's cladding.
The stress categories and strength theory presented in the ASME BPVC Section III, are used as a general guide.
Zirconium alloy structural components, which consist of guide thimbles and fuel tubes, are in turn subdivided into two categories because of material differences and functional requirements. The fuel tube design DCPP UNITS 1 &
2 FSAR UPDATE 4.2-19 Revision 23 December 2016 criteria are covered separately in Section 4.2.1.2.3. For the guide thimble design, the stress intensities, the design stress intensities and the stress intensity limits are calculated using the same methods as for the austenitic steel structural components. Un-irradiated zirconium alloy properties are used to define the stress limits.
The maximum shear stress theory (Tresca criterion {Reference 22}) for combined stresses is used to determine the stress intensities for the austenitic steel components. The stress intensity is defined as the numerically largest difference between the various principal stresses in a three-dimensional field. The allowable stress intensity value for austenitic stainless steel is given by the lowest of the following:
(a) One-third of the specified minimum tensile strength, or two-thirds of the minimum yield strength, at room temperature.
(b) One-third of the tensile strength or 90 percent of the yield strength, at temperature, but not to exceed two-thirds of the specified minimum yield strength at room temperature.
The stress intensity limits for the austenitic steel components are:
Stress Intensity Limits Categories Limit General Primary Membrane Stress Intensity 1.0 S m Local Primary Membrane Stress Intensity 1.5 S m Primary Membrane plus Bending Stress Intensity 1.5 S m Total Primary plus Secondary Stress Intensity Range 3.0 S m where S m is the membrane stress.
(3) Abnormal Loads during Conditions II I or IV - Worst cases are represented by combined seismic and blowdown loads. However, with NRC approval of the DCPP leak-before-break (LBB) analysis (Reference 30) and Amendments 221 and 223, to perform the fuel assembly structural analyses based on postulated pipe break locations that consider the application of LBB (Reference 32), the blowdown loads resulting from pipe rupture events in the main reactor coolant loop piping no longer have to be considered in the structural design basis analysis. Only the much smaller blowdown loads from RCS branch line breaks have to be considered (see Section 3.6.2.1.1.1).
(a) Deflections of components cannot interfere with reactor shutdown or emergency cooling of fuel rods.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-20 Revision 23 December 2016 (b) The fuel assembly structural component stress under faulted conditions are evaluated using primarily the methods outlined in Appendix F of the ASME BPVC Section III. Since the current analytical methods utilize elastic analys is, the stress allowables are defined as the smaller value of 2.4 S m or 0.70 Su (ultimate stress) for primary membrane and 3.6 S m or 1.05 Su for primary membrane plus primary bending. For the austenitic steel fuel assembly components, the stress intensity is defined in accordance with the rules described in the previous section for normal operating conditions. For the Zircaloy components the stress intensity limits are set at two-thirds of the materi al yield strength, Sy, at reactor operating temperature. This results in Zircaloy stress limits being the smaller of 1.6 Sy or 0.70 Su for primary membrane and 2.4 Sy or 1.05 Su for primary membrane plus bending. For conservative purposes, the Zircaloy unirradiated properties are used to define the stress limits. The grid component strength criteria are based on experimental tests. For both Zircaloy and Inconel grids, the limit is the 95 percent confidence level on the true mean as taken from the distribution of measurements at operating temperature.
Stresses in the fuel rod due to thermal expansion and fuel cladding irradiation growth are limited by the relative motion of the rod as it slips over the grid spring and dimple
surfaces. Clearances between the fuel rod ends and nozzles are provided so that fuel cladding irradiation growth does not produce interferences. Stresses due to hold-down
springs opposing the hydraulic lift force are limited by the deflection characteristic of the
springs. Stresses in the fuel assembly caused by tripping of the RCCA have little influence on fatigue because of the small number of events during the life of an assembly. Welded joints in the fuel assembly structure are considered in the structural
analysis of the assembly. Appropriate material properties of welds ensure that the
design bases are met. Assembly components and prototype fuel assemblies made
from production parts were subjected to stru ctural tests to verify that the design bases requirements were met.
Precautions are taken during fuel handling operations to minimize fuel assembly grid
strap damage. These precautions include proper training of operators, confirmation of
proper functioning and alignment of the fuel handling and transfer equipment, implementation of appropriate handling precautions, and Westinghouse recommendations.
The fuel assembly design loads for shipping have been established at 4g. Probes, permanently placed in the shipping cask, monitor and detect fuel assembly
displacements that would result from loads in excess of the criteria. Experience indicates that loads which exc eed the allowable limits rarely occur. Exceeding the limits requires re-inspection of the fuel assembly. Tests on various fuel assembly components such as the grid assembly, sleeves, inserts, and structure joints have been DCPP UNITS 1 &
2 FSAR UPDATE 4.2-21 Revision 23 December 2016 performed to ensure that the shipping design limits do not result in impairment of fuel assembly function.
The seismic/LOCA analysis methodology for fuel assembly analysis is presented in Reference 27. Specific seismic/LOCA analyses have been performed for Diablo Canyon and have demonstrated that all Condition II, III and IV load requirements are satisfied for the VANTAGE+ fuel design. The seismic analyses are performed for Design Earthquake (DE) (Condition II) and f or both the Double Design Earthquake (DDE) and Hosgri Earthquake (HE) (Condition III and IV).The LOCA analysis is performed for the largest RCS branch lines (accumulator, pressure surge, residual heat removal). In all cases, the combined faulted condition seismic/LOCA grid impact forces were less than the grid strength and all stress values were found to be acceptable. Fuel assembly stresses and deflections meet the acceptance criteria for all loading conditions, as described in Section 4.2.1.3.2.5. Therefore, no fuel rod fragmentation will occur, long term core coolable geometry is maintained and RCCA insertability is maintained.
4.2.1.3.2.6 Dimensional Stability
The dimensional stability of coolant flow channels is maintained by the grids and guide thimbles structure. The lateral spacing between fuel rods is controlled by the support
dimples of adjacent grid cells plus the spring force and the internal moments generated
between the spring and the support dimples.
No interference with control rod insertion into thimble tubes will occur during a postulated LOCA transient due to fuel rod swelling, thermal expansion, or bowing. In the early phase of the event, the high axi al loads, which could be potentially generated by the difference in thermal expansion between fuel cladding and thimbles, are relieved
by slippage of the fuel rods through the grids. The relatively low drag force restraint on
the fuel rods will induce only minor ther mal bowing, not enough to close the fuel rod-to-thimble tube gap. This rod-to-grid slip mechanism occurs simultaneously with control
rod drop. Subsequent to the control rod insertion, the transient temperature increase of
the fuel rod cladding can result in sufficient swelling to contact the thimbles.
4.2.1.3.2.7 Vibration and Wear The effect of a flow-induced vibration on the fuel assembly and individual fuel rods is minimal. Both fretting and vibration have been experimentally investigated. The cyclic
stress range associated with deflections of such small magnitude is insignificant and has no effect on the structural integrity of the fuel rod.
The conclusion that the effect of flow-in duced vibrations on the fuel assembly and fuel rod is minimal is based on test results and analysis documented in WCAP-8279 (Reference 13), which considered conditions normally encountered in reactor operation.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-22 Revision 23 December 2016 The reaction on the grid support due to vibrational motions is correspondingly small and much less than the spring preload. Fir m contact is therefore maintained. No significant cladding or grid support wear is expected during the life of the fuel assembly, as described in Section 4.2.1.4.
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
During the mid-1970s, unexpected degradation of guide thimble tube walls was observed during examination of irradiated fuel assemblies taken from several operating
PWRs. It was later determined that coolant up-flow through the guide thimble tubes and turbulent cross-flow above the fuel assemblies were responsible for inducing vibratory
motion in normally full y withdrawn ("parked") control rods. When these vibrating rods were in contact with the inner surface of the thim ble wall, a fret ting wear of the thimble wall occurred. The extent of the observed w ear is both time and nuclear steam supply system (NSSS) design-dependent and has been observed, in some non-Westinghouse cases, to extend through the guide tube walls, resulting in the formation of holes.
Guide thimble tubes function as the main structural members of the fuel assembly and
as channels to guide and decelerate tripped control rods. Significant loss of mechanical integrity due to wear or hole formation could: (a) result in the inability of the guide
thimble tubes to withstand their anticipated loadings for fuel handling accidents and
transients, and (b) hinder RCCA trip.
The susceptibility and impact of guide thimble tube wear in Westinghouse plants of the
DCPP design have been assessed in References 17 through 20. Included is a mechanistic wear model and the impact of the model's wear predictions on plant designs such as for DCPP.
Accordingly, the DCPP fuel design will exp erience less wear than that reported for other NSSS designs because the DCPP fuel desi gn uses thinner, more flexible control rods that have relatively more lateral support in the guide tube assembly of the upper core
structure. Such a design provides the housing and guide path for the RCCA above the core, and thus restricts control rod vibration due to lateral exit flow. The wear model is
also believed to conservatively predict guide thimble tube wear and even with the worst anticipated wear conditions (both in the degree of wear and the location of wear), the
guide thimble tubes will be able to fulfill their design functions.
Pacific Gas and Electric Company (PG&E) participated in a surveillance program to obtain data related to guide tube thimble we ar (References 20 and 21). Data obtained from surveillance program examinations confirmed that guide thimble tubes used in
DCPP meet design requirements.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-23 Revision 23 December 2016 4.2.1.3.3 Fuel Assembly Structure Design Evaluation 4.2.1.3.3.1 Structural Integrity Design Evaluation Structural integrity of fuel assemblies is ensured by setting limits on stresses and deformations due to various loads and by determining that the assemblies do not interfere with other components' operability (refer to Section 4.2.1.3.2.5). No interference with control rod insertion into thimble tubes will occur during a postulated LOCA transient due to fuel rod swelling, thermal expansion, or bowing (refer to Section 4.2.1.3.2.6). Deflections of components have been determined not to interfere with reactor shutdown or emergency cooling of fuel rods (refer to Section 4.2.1.3.2.5).
4.2.1.3.3.2 Fuel Assembly Shipping and Handling Loads Design Evaluation Fuel handling accelerations at both the manufacturing facility and reactor sites have been determined to be well below the 4g limit. Extensive over-the-road tests with shipping containers containing dummy (lead weighted) fuel assemblies were made during the current shipping container design development. Roads were specifically selected to ensure that the most realistic adverse conditions such as jumping curbs, railroad tracks, rough roads, etc. were encountered. Recording accelerometers confirmed that insignificant g loads were communicated to the fuel assembly carriage in the container.
4.2.1.3.3.3 Top Nozzle Design Evaluation Finite element analyses of the nozzle have been performed which show that the design is more than adequate to resist the 4g load ing. Structural testing has verified this result.
The RTN feature was tested both as individual joints and functionally as part of the fuel assembly flow test assembly (refer to Appendix A, Sections A.1.0 and A.3.0 of Reference 26). The results of these tests demonstrate that the joint strength exceeds the structural (4g) and functional requirement.
4.2.1.3.3.4 Fuel Assembly Holddown Springs Design Evaluation The results of the flow testing serve as the basis for optimizing the spring force with due consideration of fuel assembly growth and holddown spring relaxation and holddown force requirements (refer to Appendix A, Section A.1.0 of Reference 26).
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-24 Revision 23 December 2016 4.2.1.4 Operational Experience The operational experience of Westinghouse cores is presented in WCAP-8183 (Reference 8).
4.2.1.5 Safety Evaluation 4.2.1.5.1 General Design Criterion 2, 1967 - Performance Standards The seismic analyses for the fuel assemblies documents that the fuel assembly design can withstand the additional forces that might be imposed under DDE and HE conditions without fuel or clad damage that could interfere with continued effective core cooling (refer to Section 3.7.3.15.2).
4.2.1.5.2 General Design Criterion 10, 1971 - Reactor Design Section 4.2.1.2.1 provides the conservative design bases of the fuel rods adopted for Condition I and Condition II events.
Section 4.2.1.2.3 describes how the fuel rods are designed to ensure that the design bases are satisfied for Condition I and Condition II events. Section 4.2.1.3.1 provides the design bases to ensure the structural integrity of the fuel assembly adopted for Condition I and Conditi on II events. Section 4.2.1.3.3 describes how the fuel assembly meets its design basis.
4.2.1.5.3 Safety Function Requirements (1) Loads During Handling Section 4.2.1.3.3.2 documents that the fuel assembly shipping and handling load safety function requirements are met.
4.2.1.5.4 10 CFR 50.46(b)(4) - Coolable Geometry The fuel is designed with appropriate margin to assure that following a postulated LOCA, the calculated core geometry remains amenable to cooling by the ECCS. The calculated core geometry allows adequate ECCS cooling to assure the peak cladding temperature does not exceed 2200F and the maximum cladding oxidation nowhere exceeds 0.17 times the total cladding thickness prior to oxidation (refer to Sections 4.2.1.3.3.1 and 15.4.1).
Plant specific analyses were performed using the approved methodology in WCAP-9401 (Reference 27) to demonstrate structural integrity of fuel assemblies, in accordance with NUREG-0800, Standard Review P lan (SRP) for the Review of Safety Analysis Reports for Nuclear Power Plants, Section 4.2, Appendix A.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-25 Revision 23 December 2016 4.2.1.6 Tests and Inspections 4.2.1.6.1 Quality Assurance Program The Quality Assurance Program for Westinghouse nuclear fuel is summarized in the
latest edition of the Westinghouse Nucle ar Fuel Division Quality Assurance Program Plan, as listed in the PG&E Qualified Suppliers List.
4.2.1.6.2 Manufacturing The Westinghouse quality control philosophy during manufacturing is described in the
Westinghouse Nuclear Fuel Division Quality Assurance Program Plan, as listed in the
PG&E Qualified Suppliers List.
4.2.1.6.3 Onsite Inspection Onsite inspection of fuel assemblies, control rods, and reactor vessel internals is performed in accordance with the inspection program requirements discussed in
Chapter 17.
Surveillance of fuel and reactor performance is routinely conducted on Westinghouse
reactors. Power distribution is monitored using the excore fixed and incore movable detectors. Coolant activity and chemistry are followed, which permit early detection of
any fuel cladding defects.
Visual examinations are routinely conducted during refueling outages. Additional fuel inspections are dependent on results of the operational monitoring and the visual examinations. Onsite examinatio ns, if required, could include fuel integrity or other fuel performance evaluation examinations.
4.2.1.6.4 Removable Fuel Rod Assembly
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
As part of a continuing Westinghouse fuel performance evaluation program, one surveillance fuel assembly containing 88 rem ovable fuel rods was included in Region 3 of the initial DCPP Unit 1 and Unit 2 core loading. The objective of this program was to facilitate interim and EOL fuel evaluation as a function of exposure. The rods could be removed, nondestructively examined, and reinserted at the end of intermediate fuel cycles. The rods could be removed easily and subjected to a destructive examination at EOL.
The overall dimensions, rod pitch , number of rods, and material are the same as for other Region 3 assemblies. These fuel rods were fabricated in parallel with the regular Region 3 rods using selected Region 3 cladding and pellets fabricated to the same DCPP UNITS 1 &
2 FSAR UPDATE 4.2-26 Revision 23 December 2016 manufacturing tolerance limits. Mechanically, the special assemblies differ from other Region 3 assemblies only in those features that facilitate removal and reinsertion.
Figure 4.2-6 compares the mechanica l design of a removable fuel rod to a standard rod.
Figure 4.2-7 shows the removable rod fuel asse mbly, the modified upper nozzle adapter plate, and thimble plug assembly; it may be compared to the standard assembly shown in Figure 4.2-2. The location of the removable rods within the fuel assembly is shown in
Figure 4.2-8. Fuel handling with removable fuel rods has been done routinely and without difficulty in many operating plants.
4.2.2 REACTOR
VESS EL INTERNALS 4.2.2.1 Design Bases 4.2.2.1.1 General Design Criterion 2, 1967 - Performance Standards The reactor internals are designed to withstand the effects of, or are protected against, natural phenomena such as earthquakes.
4.2.2.1.2 General Design Criterion 4, 1987
- Environmental and Dynamic Effects Design Bases Consideration of the dynamic effects associated with main reactor coolant loop (RCL) piping postulated pipe ruptures are excluded from the DCPP design basis with the approval of leak-before-break (LBB) methodology by demonstrating that the probability of fluid system piping rupture is extremely low under conditions consistent with the design basis for the piping.
4.2.2.1.3 General Design Criterion 10, 1971 - Reactor Design The reactor vessel internals are designed with appropriate margin to assure that SAFDLs are not exceeded during any condi tion of normal operation, including the effects of anticipated operational occurrences.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-27 Revision 23 December 2016 4.2.2.1.4 Safety Function Requirements (1) Core Flow Distribution The reactor vessel internals, in conjunction with the fuel assemblies, direct reactor coolant through the core to achieve acceptable flow distribution and to restrict bypass flow so that the heat transfer performance requirements are met for all modes of
operation. In addition, required cooling for the pressure vessel head is provided so that the temperature differences between the vessel flange and head do not result in leakage from the flange during reactor operation.
(2) Protection of the Reactor Pressure Vessel from Neutron Exposure In addition to neutron shielding provided by the reactor coolant, a thermal shield in Unit 1 and a neutron pad (Reference 7) assembly in Unit 2 limit the neutron exposure of the pressure vessel. Additionally, provisions are made to install the vessel material test specimens for the reactor pressure vessel material surveillance program (refer to Section 5.2).
(3) Incore Instrumentation
Provisions are made to install incore instrumentation for plant operation.
4.2.2.2 Acceptance Criteria The acceptance criteria for the mechanical design of the reactor vessel internals components are:
(1) The core internals were designed to withstand mechanical loads arising from the DE, DDE, HE, and pipe ruptures (refer to Sections 3.7.3.15 and 3.9.2.1.3). The seismic and pipe rupture design of core internals is further discussed in Sections 3.7.3 and 3.9.3. This addresses GDC 2, 1967.
(2) The reactor has mechanical provisions to adequately support the core and internals and to ensure that the core is intact with acceptable heat transfer geometry following transients arising from abnormal operating conditions.
This addresses GDC 10, 1971.
(3) Following the design basis accid ent, the plant shall be capable of being shut down and cooled in an orderly fashion so that fuel cladding
temperature is kept within 10 CFR 50.46 limits. This implies that the
deformation of certain critical reactor internals must be kept sufficiently
small to allow core cooling (refer to Section 3.9.2.3.1).
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-28 Revision 23 December 2016 4.2.2.3 Reactor Vessel Internals Description The components of the reactor vessel internals consist of the lower core support structure (including the entire core barrel, the thermal shield on Unit 1, and the neutron shield pad assembly on Unit 2), the upper core support structure, and the incore
instrumentation support structure. The rea ctor vessel internals support the core, maintain fuel alignment, limit fuel assembly movement, maintain alignment between fuel assemblies and CRDMs, direct coolant flow past the fuel elements, direct coolant flow to the pressure vessel head, and provide gamma and neutron shielding and guides for
incore instrumentation.
In DCPP Unit 1, the coolant flows from the vessel inlet nozzles down the annulus between the core barrel and the vessel wall around the thermal shield. Most of the coolant then enters the plenum at the bottom of the vessel. The coolant then reverses and flows up through the core support and lower core plate. A small portion of the coolant passes through core barrel flow holes and flows downward between the core barrel and the baffle plate, providing additional cooling of the barrel, and enters the core between the bottom of the baffle plate and the top of the lower support plate. The coolant coming up through the lower core plate and the coolant coming out to the baffle region then passes through the core. After passing through the core, the coolant enters the upper support structure and flows radially to the core barrel outlet nozzles and
directly through the vessel outlet nozzles. Additio nally, a small amount of the entering flow is directed into the vessel head plenum and exits through the vessel outlet nozzles.
In DCPP Unit 2, all the flow entering the core barrel from the inlet nozzle flows downward around the thermal neutron pads into the lower plenum. The coolant then reverses and flows upwards through the lower core plate and into the core and the
baffle barrel region. After passing through the core, the coolant enters the upper support structure and flows radially to the core barrel outlet nozzles and directly through the vessel outlet nozzles. A small portion passes up between the core barrel and the baffle plate, providing additional cooling of the barrel, and enters the upper support structure through flow holes in the baffle region top plate. Also for Unit 2, an additional modification has been made to reduce the upper head bulk fluid temperature to
approximately T-cold. In this modification, reactor upper and lower internals were
modified to provide additional flow in the upper head region.
The major material for the reactor vessel internals is Type 304 stainless steel. Parts not fabricated from Type 304 stainless steel include bolts and dowel pins, which are
fabricated from Type 316 stainless steel, the radial support clevis inserts which are fabricated from alloy 600, and insert bolts, which are fabricated from alloy X-750. The Unit 1 reactor vessel internals hold-down springs are Type 304 stainless steel. The Unit 2 reactor vessel internals hold-down springs are made of Type 403 stainless steel treated in accordance with ASME BPVC-1971, Case Number 1337 to have a yield stress greater than 90,000 psi. Undue susceptibility to intergranular stress corrosion cracking is prevented by not using sensitized stainless steel, as recommended in
Regulatory Guide 1.44, May 1973 (Reference 23).
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-29 Revision 23 December 2016 All reactor vessel internals are removable, thus permitting inspection of the vessel internal surface.
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
With respect to previous plants, there is no change in the design configuration of reactor vessel internals and the reactor vessel internals core support structures. Moreover, since their mechanical properties (e.g., fuel assembly weight, beam stiffness) are virtually the same, the response of the reactor vessel internals core support structure will not change.
The qualification of identical plants by the first-of-a-kind analysis is further verified by the Internals Vibration Assurance Program discussed in Section 3.9.2.1.
4.2.2.3.1 Lower Core Support Structure The reactor vessel internals support member is the lower core support structure shown in Figures 4.2-9 and 4.2-10 for DCPP Unit 1 and Unit 2, respectively. This support structure assembly consists of the core barrel, the core baffle, the lower core plate and support columns, the thermal shield on Unit 1, and the neutron shield pad assembly on Unit 2 (the transition from a thermal shield to neutron shield pad assembly is explained in WCAP-7870 {Reference 7}), and the core support, which is welded to the core barrel.
All the major material for this structure is Type 304 stainless steel. The lower core
support structure is supported at its upper flange from a ledge in the reactor vessel and
its lower end is restrained from transverse motion by a radial support system attached to the vessel wall. Within the core barrel are an axial baffle and a lower core plate, both
of which are attached to the core barrel wall and form the enclosure periphery of the core. The lower core support structure and core barrel provide passageways and direct
the coolant flow. The lower core plate is positioned at the bottom level of the core
below the baffle plates and provides support and orientation for the fuel assemblies.
The lower core plate contains the necessary flow distribution holes for each fuel
assembly. On Unit 2, adequate coolant distri bution is obtained through the use of the lower core plate and the flat core support. Unit 1 has a domed core support plate.
Adequate coolant distribution is obtained through the use of an intermediate flow diffuser plate and the lower core plate.
On Unit 1, the one-piece thermal shield is fix ed to the core barrel at the top with rigid bolted connections. The bottom of the thermal shield is connected to the core barrel by means of axial flexures. Rectangular specimen guides in which material samples can
be inserted, held by a preloaded spring device, and irradiated during reactor operation, are welded to the thermal shield.
On Unit 2, the neutron shield pad assembly, shown in Figure 4.2-11, consists of four
panels, constructed of Type 304 stainless steel, that are bolted and pinned to the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-30 Revision 23 December 2016 outside of the core barrel. Rectangular specimen guides in which material surveillance samples are inserted, held by a preloaded spring device, and irradiated during reactor
operation, are bolted and pinned to the panels.
Additional details of the neutron shielding pads and irradiation specimen holders are given in Reference 7.
Vertically downward loads from weight, fuel assembly preload, control rod dynamic loading, hydraulic loads, and earthquake acceleration are carried by the lower core
plate into the lower core plate support flange on the core barrel shell, and through the
lower support columns to the core support and then through the core barrel shell to the
core barrel flange supported by the vessel flange. Transverse loads from earthquake
acceleration, coolant cross flow, and vibration are carried by the core barrel shell and
distributed between the lower radial support to the vessel wall and to the vessel flange.
Transverse loads of the fuel assemblies are transmitted to the core barrel shell by direct
connection of the lower core plate to the barrel wall, and by upper core plate alignment
pins that are welded into the core barrel.
The radial support system of the core barrel is accomplished by "key" and "keyway" joints to the reactor vessel wall. At six equally spaced points around the circumference, an Inconel clevis block is welded to the vessel inner diameter. An Inconel insert block is bolted to each of these clevis blocks, and has a keyway geometry. Opposite each of
these is a key that is welded to the lower core support. During assembly, as the
internals are lowered into the vessel, the keys engage the keyways in the axial
direction.
Radial and axial expansions of the core barrel are accommodated, but this design
restricts transverse movement of the core barrel. With this system, cyclic stresses in the internal structures are within the ASME BPVC Section III limits. In the event of an abnormal downward vertical displacement of the internals following a hypothetical
failure, the load is transferred through energy absorbing devices of the lower internals to
the vessel. The number and design of these absorbers are determined so as to limit the
stresses imposed on all components (except the energy absorber) to less than yield
stress (ASME BPVC Section III values).
To prevent fuel rod damage as a result of water jetting through lower internals baffle
gaps in Unit 2, edge bolts have been added along the full length of the center injection
baffle plate joints and the gaps have been peened after bolting. Unit 1 has edge bolts
along the entire length of all corner and center injection baffle plate joints.
In addition, if baffle jetting is detected in Unit 2, anti-baffle jetting fuel clips may be used
to dampen the amplitude of the fuel rod vibrations.
4.2.2.3.2 Upper Core Support Assembly The upper core support assembly, shown in Figures 4.2-12through 4.2-14, consists of the upper support assembly and the upper core plate between which are contained
support columns and guide tube assemblies. The support columns establish the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-31 Revision 23 December 2016 spacing between the upper support assembly and the upper core plate, and transmit the mechanical loadings between the upper support and upper core plate. The guide tube
assemblies shield and guide the control rod drive shafts and control rods. Flow
restrictors are installed in the guide tubes that formerly housed the part length CRDM
drive shafts.
The upper core support assembly, which is removed as a unit during the refueling
operation, is positioned in its proper orientation with respect to the lower support
structure by slots in the upper core plate. Fuel assembly locating pins protrude from the
bottom of the upper core plate and engage the fuel assemblies as the upper assembly
is lowered into place, thus ensuring proper alignment of the lower core support
structure, the upper core support assembly, the fuel assemblies, and control rods. The
upper core support assembly is restrained from any axial movements by a large
circumferential spring that rests between the upper barrel flange and the upper core support assembly. The spring is compressed when the reactor vessel head is installed
on the pressure vessel.
Vertical loads from weight, earthquake accel eration, hydraulic loads, and fuel assembly preload are transmitted through the upper core plate, via the support columns, to the
upper support assembly and then into the reactor vessel head. Transverse loads from
coolant cross flow, earthquake acceleration, and possible vibrations are distributed by
the support columns to the upper support and upper core plate. The upper support
plate is particularly stiff to minimize deflection.
4.2.2.3.3 Incore Instrumentation Support Structures The incore instrumentation support structures consist of an upper system to convey and support thermocouples penetrating the vessel through the head, and a lower system to
convey and support flux thimbles penetrating the vessel through the bottom (Figure 7.7-9 shows the basic flux-mapping system).
The upper system utilizes the reactor vessel head penetrations. Instrumentation port
columns are slip-connected to in-line columns that are, in turn, fastened to the upper
support plate. These port columns protrude through the head penetrations. The
thermocouple conduits, made of Type 304 stainless steel, are supported from the
columns of the upper core support system.
In addition to the upper incore instrumentation, there are reactor vessel bottom port
columns that carry the retractable, cold-worked stainless steel flux thimbles that are
pushed upward into the reactor core. Conduits exten d from the bottom of the reactor vessel down through the concrete shield area and up to a thimble seal table. The
thimbles are closed at the leading ends and serve as the pressure barrier between the
reactor pressurized water and the containment atmosphere.
Mechanical seals between the retractable thimbles and conduits are provided at the
seal table. During normal operation, the retractable thimbles are stationary and move DCPP UNITS 1 &
2 FSAR UPDATE 4.2-32 Revision 23 December 2016 only during refueling or for maintenance, at which time a space of approximately 15 feet above the seal table is cleared for the retraction operation.
The incore instrumentation support structure is designed for adequate support of
instrumentation during reactor operation and is sturdy enough to resist damage or
distortion under the conditions imposed by handling during the refueling sequence.
Reactor vessel surveillance specimen capsules are covered in Section 5.2.2.4.
4.2.2.4 Reactor Vessel Internals Design Evaluation The following show the acceptance criteria in Section 4.2.2.2 are satisfied.
4.2.2.4.1 Design Loading Conditions The design loading conditions for the reactor vessel internals are:
(1) Fuel assembly weight (2) Fuel assembly spring forces (3) Internals weight (4) Control rod scram (equivalent static load)
(5) Differential pressure (6) Spring preloads (7) Coolant flow forces (static)
(8) Temperature gradients (9) Differences in thermal expansion (a) Due to temperature differences (b) Due to expansion of different materials (10) Interference between components (11) Vibration (mechanically or hydraulically induced)
(12) One or more loops out of service (13) All operational transients listed in Table 5.2-4
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-33 Revision 23 December 2016 (14) Pump overspeed (15) Seismic loads (DE, DDE and HE)
(16) Blowdown forces (due to RCS branch line breaks)
Combined seismic and blowdown forces ar e included in the stress analysis by assuming the maximum amplitude of each force to act concurrently. In the original
analyses, the blowdown forces were those resulting from breaks in the RCS cold and
hot legs. However, with the acceptance of the DCPP LBB analysis by the NRC (Reference 30), the blowdown forces resulting from pipe rupture events in the main RCL piping no longer have to be considered in the design basis analyses. Only the much smaller loads from RCS branch line breaks have to be considered (refer to Section 3.6.2.1.1.1).
The design analysis ensures that allowable stress limits are not exceeded, that adequate design margin exists, and establishes deformation limits that are concerned primarily with components' operability. The stress limits are established not only to
ensure that peak stresses do not reach unacceptable values, but also to limit the
amplitude of the oscillatory stress component in consideration of material fatigue
characteristics. Both low and high cycle fatigue stresses are considered when the
allowable amplitude of oscillation is established. Dynamic analysis on the reactor internals is provided in Section 3.9.2.3.
As part of the evaluation of design loading conditions, extensive testing and inspections are performed from the initial selection of raw materials up to and including component installation and plant operation. Among these tests and inspections are those
performed during component fabrication, plant construction, startup and checkout, and
plant operation.
4.2.2.4.2 Design Loading Categories The combination of design loadings fits into either the normal, upset, or faulted
conditions(refer to Table 5.2-4). The reactor vessel internals are designed to withstand stresses originating from RCS design transients, as summarized in Table 5.2-6.
Loads and deflections imposed on components due to shock and vibration are
determined analytically and experimentally in both scaled models and operating
reactors. The cyclic stresses due to these dynamic loads and deflections are combined
with the stresses imposed by loads from component weights, hydraulic forces, and thermal gradients for the determination of the total stresses of the internals.
The scope and methodology of the stress analysis problem is discussed in Section
3.9.2.3.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-34 Revision 23 December 2016 4.2.2.4.3 Allowable Deflections For normal operating conditions, downward vertical deflection of the lower core support plate is negligible.
Limiting deflection values from the LOCA plus the earthquake (larger of the DDE or HE), and for the deflection criteria of critical internal structures, are given in Section 3.9.2.3 and Table 3.9-10.
The criteria for the core drop accident are based on determining the total downward
displacement of the internal structures followi ng a hypothesized core drop resulting from loss of supports. The initial clearance between the secondary core support structures and the reactor vessel lower head in the hot condition is approximately 1/2 inch. An additional displacement of approximately 3/4 inch would occur due to strain of the energy absorbing devices of the secondary core support; thus the total drop distance is
about 1-1/4 inches, which is insufficient to permit the tips of a fully withdrawn RCCA to come out of the guide thimble.
Specifically, the secondary core support is a device that will never be used, except
during a hypothetical accident of the core support (core barrel, barrel flange, etc.).
There are four supports in each reactor. This device limits the fall of the core and
absorbs the energy of the fall that otherwise would be imparted to the vessel. The
energy of the fall is calculated assuming a complete and instantaneous failure of the
primary core support and is absorbed during the plastic deformation of the controlled
stainless steel volume loaded in tension.
4.2.2.4.4 Design Criteria Bases
The structural adequacy of the reactor vessel internals is discussed in Section 3.9.2.3.5.1.
4.2.2.5 Safety Evaluation 4.2.2.5.1 General Design Criterion 2, 1967 - Performance Standards The design loading conditions for the reactor vessel internals include the additional forces that may be imposed by earthquakes. The design analysis ensures that allowable stress limits are not exceeded and establishes deformation limits that are concerned primarily with components' operability (refer to Section 4.2.2.4.1).
Allowable deflections for normal operating conditions and the limiting deflection values from the LOCA plus the earthquake are discussed in Section 3.9.2.3.3.
Section 3.7.3.15.1 provides a detailed discussion of the seismic analyses for the reactor vessel internals.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-35 Revision 23 December 2016 4.2.2.5.2 General Design Criterion 4, 1987
- Environmental and Dynamic Effects Design Bases Protection from the dynamic effects of the most limiting breaks of auxiliary lines is considered. RCS branch line breaks and other high energy line breaks are provided.
Refer to Section 3.9. 3.3 for additional discus sion of LBB methodology and application.
The LOCA dynamic analyses are based on the accumulator, pressurizer surge, and residual heat removal system RCS branch line breaks credited LBB (Reference 32).
4.2.2.5.3 General Design Criterion 10, 1971 - Reactor Design The reactor vessel internals are designed with appropriate margin to assure that SAFDLs are not exceeded during any condi tion of normal operation, including the effects of anticipated operational occurrences. Section 4.2.2.4.2 documents that the reactor vessel internals are designed to withstand stresses originating from design transients. Section 3.9.2.3 discusses the design criteria used for normal operating conditions to evaluate calculated static and dynamic stresses. These calculated allowable stresses are considered appropriate and conservative.
4.2.2.5.4 Safety Function Requirements (1) Core Flow Distribution The components of the reactor vessel internals direct coolant flow past the fuel elements and direct coolant flow to the pressure vessel head (refer to Section 4.2.2.3).
The design loading conditions for the reactor vessel internals include temperature gradients and differences in thermal expansion due to temperature differences and the expansion of different materials (refer to Section 4.2.2.4.1).
(2) Protection of the Reactor Pressure Vessel from Neutron Exposure The Unit 1 one-piece thermal shield is fixed to the core barrel at the top with rigid bolted connections. The bottom of the thermal shi eld is connected to the core barrel by means of axial flexures. Rectangular specimen guides in which material samples can be inserted, held by a preloaded spring device, and irradiated during reactor operation, are welded to the thermal shield (refer to Section 4.2.2.3.1).
The Unit 2 neutron shield pad assembly consists of four panels, constructed of Type 304 stainless steel, that are bolted and pinned to the outside of the core barrel (refer to Figure 4.2-11). Rectangular specimen guides in which material surveillance samples are inserted, held by a preloaded spring device, and irradiated during reactor operation, are bolted and pinned to the panels. Additi onal details of the neutron shielding pads and irradiation specimen holders are given in Reference 7.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-36 Revision 23 December 2016 The reactor vessel internals have provisions to install material test specimens for the reactor vessel material surveillance program (refer to Section 5.2.2.4.4).
(3) Incore Instrumentation The reactor vessel internals have provisions to install incore instrumentation. The incore instrumentation support structure is designed for adequate support of instrumentation during reactor operation (refer to Section 4.2.2.3.3).
4.2.3 REACTIVITY
CONTROL SYSTEM 4.2.3.1 Design Bases 4.2.3.1.1 General Design Criterion 2, 1967 - Performance Standards The CRDMs are designed to withstand the effects of, or are protected against, natural phenomena, such as earthquakes.
4.2.3.1.2 General Design Criterion 4, 1987
- Environmental and Dynamic Effects Design Bases Consideration of the dynamic effects associated with main RCL piping postulated pipe ruptures are excluded from the DCPP des ign basis with the approval of LBB methodology by demonstrating that the probability of fluid system piping rupture is extremely low under conditions consistent with the design basis for the piping.
4.2.3.1.3 General Design Criterion 25, 1971 - Protection System Requirements for Reactivity Control Malfunctions The reactivity control system is designed to assure that no single malfunction (this does not include rod ejection) causes a violation of the acceptable fuel design limits.
4.2.3.1.4 General Design Criterion 26, 1971 - Reactivity Control System Redundancy And Capability The reactivity control system is provided with redundancy and capability such that two independent reactivity control systems of diff erent design principles and capabilities of reliably controlling reactivity changes under conditio ns of normal operation, including anticipated operational occurrences, to assure acceptable fuel design limits are not exceeded.
In addition, one of the systems is capable of holding the reactor core subcritical under cold conditions. To meet this requirement the rod control system is designed to provide sufficient operational control and reliability during reactivity changes during normal and anticipated transients and the c hemical and volume control system (CVCS) regulates the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-37 Revision 23 December 2016 concentration of chemical neutron absorber in the reactor coolant to control reactivity changes.
4.2.3.1.5 General Design Criterion 29, 1971 - Protection Against Anticipated Operational Occurrences The reactivity control system is designed to ensure an extremely high probability of functioning during anticipated operational occurrences.
4.2.3.1.6 General Design Criterion 30, 1967
- Reactivity Holddown Capability At least one of the reactivity control systems provided is capable of making and holding the core subcritical under any conditions with appropriate margins for contingencies.
4.2.3.2 Reactivity Control System Acceptance Criteria 4.2.3.2.1 Design Stresses Acceptance Criteria The reactivity control system is designed to withstand stresses originating from the
operating transients summarized in Table 5.2-4.
Allowable stresses for normal operating conditions are in accordance with ASME BPVC Section III. All components are analyzed as Class I components under Article NB-3000.
The cyclic stresses due to dynamic loads and deflections are combined with the
stresses imposed by loads from component weights, hydraulic forces, and thermal gradients to determine the total stresses of the reactivity control system.
4.2.3.2.2 Material Compatibilit y Acceptance Criteria Materials are selected for compatibility in a PWR environment, adequate mechanical properties at room and operating temperature, resistance to adverse property changes
in a radioactive environment, and compatibility with interfacing components.
4.2.3.2.3 Absorber Rods Acceptance Criteria
The following design conditions, based on Article NB-3000 of the ASME BPVC Section III-1973, are considered.
(1) The external pressure equal to the RCS operating pressure (2) The wear allowance equivalent to 1000 reactor trips (3) Bending of the rod due to a misalignment in the guide tube (4) Forces imposed on the rods during rod drop DCPP UNITS 1 &
2 FSAR UPDATE 4.2-38 Revision 23 December 2016 (5) Loads caused by accelerations imposed by the CRDM (6) Radiation exposure for maximum core life.
The absorber material temperature shall not exceed its melting temperature (1470°F for
silver-indium-cadmium absorber material {Reference 2}).
The Westinghouse RCCA and Enhanced Performance RCCA (EP-RCCA) model control rods that are cold-rolled Type 304 stainless steel is the only noncode material
used in the control assembly. The stress intensity limit S m for this material is defined as two-thirds of the 0.2 percent offset yield stress.
The Framatome RCCAs have an ion-nitrided 316L cladding material that improves wear resistance. The Framatome control rod noncode material stress intensity limit S m is also two-thirds of the 0.2 percent offset yield stress.
4.2.3.2.4 Burnable Absorber Rods Acceptance Criteria The burnable absorber rod cladding (Zircalo y-4 for the wet annular burnable absorber
{WABA} design) is designed as a Class I component under Article NB-3000 of the ASME BPVC Section III-1973, for Conditions I and II. For Conditions III and IV loads, code stresses are not considered limiting. Failures of the burnable absorber rods during
these conditions must not interfere with reactor shutdown or emergency cooling of the
fuel rods.
The structural elements of the burnable absorber rod are designed to maintain absorber geometry. The rods are designed so that the Al 2 O 3-B 4 C material is below 1200°F during normal operation or overpower transients.
4.2.3.2.5 Neutron Source Rods Acceptance Criteria The neutron source rods are designed to withstand:
(1) An external pressure equal to the RCS operating pressure (2) An internal pressure equal to the pressure generated by gases released over the neutron source rod life.
4.2.3.2.6 Thimble Plug Assembly Acceptance Criteria The thimble plug assemblies:
(1) Accommodate the differential thermal expansion between fuel assembly and core internals
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-39 Revision 23 December 2016 (2) Maintain positive contact with the fuel assembly and the core internals (3) Can be inserted into, or withdrawn from, the fuel assembly by a force not exceeding 65 pounds.
4.2.3.2.7 Control Rod Drive Mechanism Acceptance Criteria The CRDMs were designed to meet the following basic operational requirements:
(1) 5/8-inch per step (2) 142.5-inch travel (nominal)
(3) 360 pounds-force maximum load (4) Step in or out at 45 inches per minute (72 steps per minute) maximum (5) Power interruption shall initiate release of drive rod assembly (6) Trip delay of 150 milliseconds or less - Free fall of drive rod assembly shall begin less than 150 milliseconds after power interruption, no matter what holding or stepping action is being executed, with any load and
coolant temperatures between 100°F and 650°F.
(7) 50-year design life with normal refurbishment (8) 13,200 complete travel excursions equaling 6 million steps with normal refurbishment 4.2.3.3 Reactivity Control System Description Reactivity control is provided by neutron absorbing rods and a soluble chemical neutron
absorber (boric acid). The boric acid concentration is varied to control long-term
reactivity changes such as:
(1) Fuel depletion and fission product buildup (2) Cold to hot, zero power reactivity change (3) Reactivity change produced by intermediate-term fission products such as xenon and samarium (4) Burnable poison depletion
The concentration of boric acid in the reactor coolant is regulated by the CVCS, as described in Section 9.3.4.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-40 Revision 23 December 2016 The RCCAs provide reactivity control for:
(1) Shutdown (2) Reactivity changes due to coolant temperature changes in the power range (3) Reactivity changes associated with the power coefficient of reactivity (4) Reactivity changes due to void formation
The neutron source assemblies provide a means of verifying that the neutron
instrumentation performs its function during periods of low neutron activity. They also
provide the required count rate during startup.
The most effective reactivity control component is the RCCA and its corresponding drive
rod assemblies. Figure 4.2-15 identifies the rod cluster control and drive rod assembly, in addition to the interfacing fuel assembly, guide tubes, and CRDM.
Guidance for the control rod cluster is provided by the guide tube, as shown in
Figure 4.2-15. The guide tube provides two types of guidance:
(1) In the lower section, a continuous guidance system provides support immediately above the core. This system protects the rod against
excessive deformation and wear due to hydraulic loading.
(2) The region above the continuous section provides support and guidance at uniformly spaced intervals.
The support envelope is determined by the RCCA pattern, as shown in Figure 4.2-16.
The guide tube ensures alignment and support of the control rods, spider body, and drive rod while maintaining trip times at or below required limits.
4.2.3.3.1 Reactivity Control Components Description The reactivity control components are subdivided into two categories:
(1) Permanent devices used to control or monitor the core (2) Optional burnable absorber assemblies The permanent type components are the RCCAs, control rod drive assemblies, and neutron source assemblies. Although the optional thimble plug assembly does not directly contribute to the reactivity control of the reactor, it is presented as a reactivity DCPP UNITS 1 &
2 FSAR UPDATE 4.2-41 Revision 23 December 2016 control system component in this document because it is used to restrict bypass flow through those thimbles not occupied by absorber, source or burnable poison rods.
The purpose of the optional burnable absorber assemblies is to control assembly power and ensure that the temperature coefficient of reactivity is less positive under normal operating conditions.
4.2.3.3.2 Rod Cluster Control Assembly Description The RCCA banks are divided into two categories: control and shutdown. Two criteria have been employed for selection of the control groups. First, the total reactivity worth
must be adequate to meet the nuclear requirements. Second, because some of these
rods may be partially inserted at power operation, the total power peaking factor should
be low enough to ensure that the power capability is met. The control and shutdown
groups provide adequate shutdown margin (SDM) which is defined as: the
instantaneous amount of reactivity by which the reactor is subcritical, or would be
subcritical from its present condition, assuming
(1) all RCCAs are fully inserted, except for the single RCCA of highest reactivity worth which is assumed to be fully withdrawn (with any RCCA not capable of being fully inserted, the reactivity worth of the RCCA must be accounted for in the determination of SDM) and (2) when in MODE 1 or 2, the fuel and moderator temperatures are changed to the hot zero power temperatures.
An RCCA comprises a group of individual neutron absorber rods fastened at the top end to a common spider assembly, as illustrated in Figure 4.2-16.
The absorber material used in the control rods is a silver-indium-cadmium alloy that is
essentially "black" to thermal neutrons and has sufficient additional resonance
absorption to significantly increase its worth. The alloy is in the form of extruded rods
that are sealed in stainless steel tubes to prevent the rods from coming in direct contact
with the coolant. The silver-indium-cadmium rods are inserted into cold-worked
stainless steel tubing. It is sealed at the bottom and top by welded end plugs, as shown
in Figure 4.2-17. Sufficient diametral and end clearance is provided to accommodate
relative thermal expansions.
The bullet-nosed bottom plugs reduce the hydraulic drag during reactor trip and guide
the absorber rods smoothly into the dashpot section of the fuel assembly guide
thimbles. The upper plug is threaded for assembly to the spider and has a reduced end
section to make the joint more flexible.
The spider assembly is in the form of a central hub with radial vanes containing
cylindrical fingers from which the absorber rods are suspended. Handling detents and
detents for connection to the drive rod assembly are machined into the upper end of the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-42 Revision 23 December 2016 hub. Coiled springs inside the spider body absorb the impact energy at the end of a trip insertion. All components of the spider assembly are made from Types 304 and 308 stainless steel, except for the retainer, which is made of 17-4 PH stainless steel
material, and the springs, which are made of Inconel 718 alloy or, for the Westinghouse RCCA and EP-RCCA spiders only, an austenitic stainless steel where the springs do not contact the coolant. Other Framatome spider assembly components
not made from 304 or 308 stainless steel are the spider itself, cast from Type 316L stainless steel, the cladding which is tempered and cold worked Type 316 stainless
steel and the rod spring spacer which is Inconel 750. The absorber rods are fastened securely to the spider to ensure trouble-free service.
The overall length is such that when the assembly is withdrawn through its full travel, the tips of the absorber rods remain engaged in the guide thimbles so that alignment between rods and thimbles is always maintained. Because the rods are long and
slender, they are relatively free to conform to any small misalignments with the guide
thimble.
4.2.3.3.3 Burnable Absorber Assembly Description Each burnable absorber assembly consists of WABA burnable absorber rods attached to a hold down assembly.
A WABA rod (refer to Figure 4.2-18a) consists of annular pellets of alumina-boron carbide (Al 2 O 3-B 4 C) burnable absorber material contai ned within two concentric Zircaloy tubes. These Zircaloy tubes, which form the inner and outer cladding for the WABA rod, are plugged and welded at each end to encapsulate the annular stack of absorber material. The assembled rod is then internally pressurized to 650 psig and seal welded.
The absorber stack lengths are positioned axially within the WABA rods by the use of
Zircaloy bottom-end spacers. An annular plenum is provided within the rod to
accommodate the helium gas released from absorber material depletion during
irradiation. The reactor coolant flows inside the inner tube and outside the outer tube of
the annular rod. Further design details are given in Section 3.0 of Reference 28.
The burnable absorber rods are statically sus pended and positioned in selected guide thimbles within the fuel assemblies. The absorber rods in each assembly are attached
together at the top end of the rods to a hold down assembly by a flat, perforated
retaining plate which fits within the fuel assembly top nozzle and rests on the adapter
plate. The absorber rod assembly is held down and restrained against vertical motion
through a spring pack which is attached to the plate and is compressed by the upper
core plate when the reactor upper internals assembly is lowered into the reactor. This
arrangement ensures that the absorber rods cannot be ejected from the core by flow forces. Each rod is permanently attached to the base plate by a nut, which is locked
into place.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-43 Revision 23 December 2016 4.2.3.3.4 Neutron Source Ass embly Description The neutron source assembly provides a base neutron level to ensure that the detectors
are operational and responding to core multiplication neutrons. Because there is very
little neutron activity during core loading, refueling, hot and cold shutdown, and
approach to criticality, neutron sources are placed in the reactor to help determine if
source range detectors are properly responding.
During core loading, it is verified that active source assemblies provide the responding
source range detectors with a sufficient count rate. For normal source range detectors (N-31 and N-32), and for alternate source ra nge detectors (N-51 and N-52), the following count rate requirements must be met after an installed active source is
neutronically coupled to a detector:
(1) For N-31 and N-32:
The count rate shall be equal to or greater than the maximum of the following count rates:
- Twice the background radiation in counts per second (CPS), or
- 1.0 CPS.
(2) For N-51 and N-52:
The count rate shall be equal to or greater than the maximum of the following count rates:
- Twice the background radiation in CPS, or
- 0.1 CPS.
The differences in required count rates are due to differences in detector sensitivity
between the proportional counters (N-31 and N-32) and the fission chambers (N-51 and
N-52).
The source assembly also permits detection of changes in the core multiplication factor
during core loading, refueling, and approach to criticality. This can be done since the
multiplication factor is related to an inverse function of the detector count rate.
Therefore, a change in the multiplication factor can be detected during addition of fuel
assemblies while loading the core, a change in control rod positions, and changes in
boron concentration.
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
The DCPP Unit 1 and Unit 2 reactor cores each employed two primary source assemblies and two secondary source assemblies in the first core. Each primary DCPP UNITS 1 &
2 FSAR UPDATE 4.2-44 Revision 23 December 2016 source assembly contained one primary source rod and between zero and twenty-three burnable absorber rods. The primary source rod, containing californium-252, spontaneously fissions and emits neutrons.
After the primary source rod decays beyond the desired neutron flux level, neutrons are then supplied by the secondary source rod.
The secondary source rod contains a mixture of approximately half antimony and half beryllium by volume, which is activated by neutron bombardment during reactor operation. Activation of antimony results in the subsequent release of neutrons by the
(,n) reaction in beryllium. This becomes a source of neutrons during periods of low neutron flux, such as during refueling and subsequent startups.
Each of the two secondary source assemblies has six secondary source rods and no burnable poison rods (refer to Figure 4.2-21).
Neutron source assemblies are located at diametrically opposite sides of the core. The assemblies are inserted into the guide thimbles at selected unrodded locations.
The secondary source rods utilize slightly cold worked 304 SS material. The secondary source rods contain about 500 grams of stacked antimony-beryllium pellets, and the rod is internally pre-pressurized to 625 50 psig. The rods in each assembly are permanently fastened at the top end to a hold down assembly, which is identical to that of the burnable absorber assemblies.
The other structural members are fabricated from Type 304 and 308 stainless steel
except for the springs exposed to the reactor coolant. They are wound from an age
hardened nickel base alloy for corrosion resistance and high strength.
4.2.3.3.5 Thimble Plug Assembly Description Thimble plug assemblies are utilized, if desired, to further limit bypass flow through the
guide thimbles in fuel assemblies that do not contain either control rods, source rods, or
burnable absorber rods.
The thimble plug assemblies shown in Figur e 4.2-22 consist of a flat base plate with short rods suspended from the bottom sur face and a spring pack assembly. The 24 short rods, called thimble plugs, project into the upper ends of the guide thimbles to
reduce the bypass flow area. Similar short rods may be also used on the source
assemblies and burnable absorber assemblies to plug the ends of all vacant fuel
assembly guide thimbles.
All components in the thimble plug assembly, except for the springs, are fabricated from
Type 304 stainless steel. The springs are wound from an age-hardened nickel base
alloy for corrosion resistance and high strength.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-45 Revision 23 December 2016 4.2.3.3.6 Control Rod Drive Mechanism Description All parts exposed to reactor coolant are made of metals that resist the corrosive action
of the water. Three types of metals are used exclusively: stainless steels, nickel alloy, and cobalt-based alloys. Wherever magnetic flux is carried by parts exposed to the main coolant, 400 series stainless steel is used. Cobalt-based alloys are used for the
pins and latch tips. Nickel alloy is used for the springs of the latch assemblies, and Type 304 stainless steel for all pressure-containing parts. Hard chrome plating provides
wear surfaces on the sliding parts and prevents galling between mating parts.
A position indicator assembly slides over the CRDM rod travel housing. This position
indicator assembly detects the drive rod assembly position by means of 42 discrete
coils that magnetically sense the entry and presence of the rod drive line through its
centerline over the normal length of the drive rod travel.
The CRDMs are located on the head of the reactor vessel. They are coupled to
RCCAs. An actual CRDM is shown in Figure 4.2-23, and a schematic in Figure 4.2-24.
The primary function of the CRDM is to insert or withdraw RCCAs into or from the core
to control average core temperature and to shut down the reactor. The CRDM is a
magnetically operated jack. A magnetic jack is an arrangement of three electromagnets
that are energized in a controlled sequence by a power cycler to insert or withdraw the
RCCAs of the reactor core in discrete steps.
The CRDM consists of the pressure vessel, coil stack assembly, the latch assembly, and the drive rod assembly:
(1) The pressure vessel includes a one-piece integrated latch housing / head adaptor. A seal weld is located between the integrated latch housing and the rod travel housing. The integrated latch housing is butt welded to the CRDM nozzle; however, the butt weld is not part of the pressure housing assembly.
The latch housing is the lower portion of the vessel and contains the latch
assembly. The rod travel housing is the upper portion of the vessel and
provides space for the drive rod during its upward movement as the
control rods are withdrawn from the core.
(2) The coil stack assembly includes the coil housings, an electrical conduit and connector, and three operating coils: (a) the stationary gripper coil, (b) the movable gripper coil, and (c) the lift coil.
Energizing the operation coils causes movement of the pole pieces and
latches in the latch assembly.
(3) The latch assembly includes the guide tube, stationary pole pieces, movable pole pieces, and two sets of latches: (a) the movable gripper latch, and (b) the stationary gripper latch.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-46 Revision 23 December 2016 The latches engage grooves in the drive rod assembly. The movable gripper latches are moved up or down in 5/8-inch steps by the lift pole to
raise or lower the drive rod. The stationary gripper latches hold the drive
rod assembly while the movable gripper latches are repositioned for the
next 5/8-inch step.
(4) The drive rod assembly includes a flexible coupling, a drive rod, a disconnect button, a disconnect rod, and a locking button.
The drive rod has 5/8-inch grooves that receive the latches during holding
or moving of the drive rod.
The disconnect button, disconnect rod, and locking button provide positive
locking of the coupling to the RCCA and permit remote disconnection.
The CRDM has a trip design. Tripping can occur during any part of the power cycler
sequencing if power to the coils is interrupted.
The mechanism can handle a 360-pound load, includ ing the drive rod weight, at a rate of 45 inches per minute (72 steps per minute). Withdrawal of the RCCA is accomplished by magnetic forces while insertion is by gravity.
The mechanism internals are designed to operate in 650°F reactor coolant. The three
operating coils are designed to operate at 392°F with forced air cooling required to maintain that temperature.
The CRDM, shown schematically in Figure 4.2-24, withdraws and inserts its control rod
as electrical pulses are received by the operator coils. Position of the control rod is
measured by 42 discrete coils mounted on the position indicator assembly surrounding
the rod travel housing. Each coil magnetically senses the entry and presence of the top
of the ferromagnetic drive rod assembly as it moves through the coil centerline.
During plant operation, the stationary gripper coil of the drive mechanism holds the
control rod withdrawn from the core in a static position until the movable gripper coil is
energized.
If power to the stationary gripper coil is cut off, the combined weight of the drive rod assembly and the RCCA is sufficient to move latches out of the drive rod assembly
groove. The control rod falls by gravity into the core. The trip occurs as the magnetic
field, holding the stationary gripper plunger half against the stationary gripper pole, collapses, and the stationary gripper plunger half is forced down by the weight acting
upon the latches. After the drive r od assembly is released by the mechanism, it falls freely until the control rods enter the buffer section of their guide tubes.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-47 Revision 23 December 2016 4.2.3.4 Reactivity Control System Design Evaluation 4.2.3.4.1 Reactivity Control Components Design Evaluation The components are analyzed for loads corresponding to normal, upset, emergency, and faulted conditions. The analysis performed depends on the mode of operation
under consideration.
The scope of the analysis requires many different techniques and methods, both static
and dynamic.
Some of the loads that are considered on each component, where applicable, are:
(1) Control rod scram (equivalent static load)
(2) Differential pressure (3) Spring preloads (4) Coolant flow forces (static)
(5) Temperature gradients (6) Differences in thermal expansion (a) Due to temperature differences (b) Due to expansion of different materials (7) Interference between components (8) Vibration (mechanically or hydraulically induced)
(9) All operational transients listed in Table 5.2-4 (10) Pump overspeed (11) Seismic loads (refer to Section 3.7.3.15)
The main objective of the analysis is to ensure that allowable stress limits are not
exceeded, that an adequate design margin exists, and to establish deformation limits
that are concerned primarily with the components' functioning. The stress limits are
established not only to ensure that peak stresses will not reach unacceptable values, but also to limit the amplitude of the oscillatory stress component in consideration of
fatigue characteristics of the materials. Standard methods of strength of materials are
used to establish the stresses and deflections of these components. The dynamic DCPP UNITS 1 &
2 FSAR UPDATE 4.2-48 Revision 23 December 2016 behavior of the reactivity control components has been studied using experimental test data and experience from operating reactors.
The design of reactivity component rods provides sufficient cold void volume within the
source rods to limit internal pressures to a value that satisfies the criteria in Section 4.2.1.2.3. The WABA rods have an annular plenum within the rod to accommodate the helium gas released from the absorber material during boron depletion (refer to Figure 4.2-18a). The internal pressure of source rods continues to increase from ambient until EOL; the internal pressure never exceeds that allowed by the criteria in
Section 4.2.1.2.3. The stress analysis for the WABA rods assumed a maximum 30 percent gas release, consistent with Reference 28.
The WABA rod cladding and rod initial intern al pressure have been designed so that the clad will not rely upon the pellets for support under all Condition I and Condition II events. Rodlet pre-pressurization will support the outer clad against irradiation induced creep collapse in the event of 0% gas release (worst case) from the Al 2 O 3-B 4 C for the design life. Calculations also verify the clad integrity under Condition I and Condition II events with a conservative maximum gas release.
Thermal analyses have shown that the maximum absorber temperature is less than 1200°F for both normal operation (Condition I) and for Condition II upset events. This provides assurance that the He gas release will not exceed limits for the WABA rod's mechanical design life of 18,000 EFPH. This also assures that the Zircaloy clad strain limit is satisfied. A conservatively large heating rate was used in the thermal analyses.
The actual heating rate would be less for the reference design due to the lower B 10 loading.
An evaluation of the WABA rod design is given in Reference 28.
Analysis of the RCCA spider indicates it is structurally adequate to withstand the various operating loads, including the higher loads that occur during the drive mechanism
stepping action and rod drop. Verification of the spider structural capability has been
experimentally demonstrated.
The material was selected on the basis of resistance to irradiation damage and
compatibility with the reactor environment. No apparent degradation of construction
material has occurred in operating plants with the DCPP reactivity control design.
Regarding material behavior in a radioactive environment, it should be noted that at
high fluences, the austenitic material increases in strength with a corresponding
decreased ductility (as measured by tensile tests), but energy absorption (as measured by impact tests) remains quite high. Corrosion of the material exposed to the coolant is
quite low, and proper control of Cl
- and O 2 in the coolant prevents stress corrosion. All of the austenitic stainless steel base material used is processed and fabricated to
preclude sensitization.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-49 Revision 23 December 2016 Analysis of the RCCA shows that if the drive mechanism housing ru ptures, the RCCA will be ejected from the core by the pressure differential of the operating pressure and ambient pressure across the drive rod assembly. The ejection is also predicated on the
failure of the drive mechanism to retain the drive rod/RCCA position. It should be
pointed out that a drive mechanism housing rupture causes the ejection of only one
RCCA with the other assemblies remaining in the core. For the Westinghouse RCCA only, analysis also showed that a pressure drop in excess of 4000 psi must occur across a two-fingered vane to break the vane/spider body joint, causing ejection of two
neutron absorber rods from the core.
Since the highest normal pressure of the primary system coolant is only 2250 psi, with the safety valves set to lift at 2485 psig, a pressure
drop in excess of 4000 psi is not expected. Thus, ejection of the neutron absorber rods
is not possible.
Ejection of a burnable absorber or thimble plug assembly is conceivable if one
postulates that the hold-down bar fails and that the base plate and burnable absorber
rods are severely deformed. In the unlikely event of hold-down bar failure, the upward
displacement of the burnable absorber assembly only permits the base plate to contact the upper core plate. Since this displacement is small, the major portion of the absorber material remains positioned within the core.
In the case of the thimble plug assembly, the thimble plugs will partially remain in the fuel assembly guide thimbles, thus
maintaining a majority of the desired flow impedance. Further displacement or
complete ejection would necessitate that the square base plate and burnable absorber rods be forced, thus plastically deformed, to f it up through a smaller diameter hole. As expected, this condition requires a substantially higher force or pressure drop than that
of the hold-down bar failure.
Experience with control rods, burnable absorber rods, and source rods is discussed in Reference 8.
The mechanical design of the reactivity control components provides for the protection of the active elements to prevent the loss of control capability and functional failure of
critical components. The components have been reviewed for potential failure and
consequences of a functional failure of critic al parts. The results of the review are summarized below.
4.2.3.4.2 Rod Cluster Control Assembly Design Evaluation (1) The basic absorbing material is sealed from contact with the primary coolant and the fuel assembly and guidance surfaces by a high quality stainless steel cladding. Potential loss of absorber mass or reduction in
reactivity control material due to mechanical or chemical erosion or wear
is therefore reliably prevented.
(2) A breach of the cladding for any postulated reason does not result in serious consequences. The silver-indium-cadmium absorber material is
relatively inert and would still remain remote from high coolant velocity DCPP UNITS 1 &
2 FSAR UPDATE 4.2-50 Revision 23 December 2016 regions. Rapid loss of material resulting in significant loss of reactivity control material would not occur.
(3) The individually clad absorber rods are doubly secured to the retaining spider vane by a threaded joint and a welded lock pin. A failure of the joint
would result in the insertion of the indiv idual rod into the core. This results in reduced core reactivity which is a fail-safe condition.
(4) The spider finger braze joint that fastens the individual rods to the vanes on the Westinghouse RCCA and EP-RCCA models have also experienced many years of service, as described above, without failure. A
failure of this joint would also result in insertion of the individual rod into
the core. The Framatome RCCA spider is one-piece casting that includes
vanes and fingers, a failure of which could also result in insertion of the
individual rod into the core.
(5) The Westinghouse RCCA and EP-RCCA models radial vanes are brazed to the spider body and guidance of the RCCA is accomplished by the inner fingers of these vanes. They are therefore the most susceptible to
mechanical damage. For the Framatome RCCA, the radial vanes are
integral parts of the one-piece spider casting.
Failure of the vane-to-hub joint of a single rod vane could potentially result
in failure of the separated vane and rod insertion. This could occur only at
withdrawal elevation where the spider is above the continuous guidance section of the guide tube (in the upper internals). A rotation of the disconnected vane could cause it to hang on one of the guide cards in the intermediate guide tube. Such an occurrence would be evident from the
failure of the RCCA to insert below a certain elevation, but with free motion above this point.
This possibility is considered extremely remote because the single rod
vanes are subjected to only vertical loads and very light lateral reactions
from the rods even during a seismic event (refer to Section 3.7.3.15). The consequences of such a failure are not considered critical since only one
drive line of the reactivity control system would be involved. This condition
is readily observed and can be cleared at shutdown.
(6) The spider hub, being of single unit cylindrical construction, is very rugged and has extremely low potential for damage. Should some unforeseen
event cause fracture of the hub above the vanes, the lower portion with
the vanes and rods attached would insert by gravity into the core causing
reactivity decrease, again a fail-safe condition.
(7) The RCCA rods are provided a clear channel for insertion by the guide thimbles of the fuel assemblies. All fuel rod failures are protected against DCPP UNITS 1 &
2 FSAR UPDATE 4.2-51 Revision 23 December 2016 by providing this physical barrier between the fuel rod and the intended insertion channel. Distortion of the fuel rods by bending cannot apply
sufficient force to damage or significantly distort the guide thimble. Fuel
rod distortion by swelling, though precluded by design, would be
terminated by fracture before contact with the guide thimble occurs. If
such were not the case, a force reaction at the point of contact would
cause a slight deflection of the guide thimble. The radius of curvature of
the deflected shape of the guide thimbles would be sufficiently large to
have a negligible influence on rod cluster control insertion.
4.2.3.4.3 Burnable Absorber Assemblies Design Evaluation
The burnable absorber assemblies are static temporary reactivity control elements. The axial position is ensured by the holddo wn assembly that bears against the upper core plate. Their lateral position is maintained by the guide thimbles of the fuel assemblies.
The individual rods are shouldered against the underside of the retainer plate and securely fastened at the top by a threaded nut that is then locked in place. The square
dimension of the retainer plate is larger than the diameter of the flow holes through the
core plate. Therefore, failure of the holddown bar or spring pack does not result in ejection of the burnable absorber rods from the core.
The only incident that could result in ejection of the burnable absorber rods is a multiple fracture of the retainer plate. This is not considered credible because of the light loads
borne by this component.
The burnable absorber rods are clad with either stainless steel or Zircaloy 4. The burnable absorber is Al 2 O 3-B 4 C annular pellets contain ed within two concentric Zircaloy tubes. Burnable absorber rods are placed in static assemblies and are not subjected to motion which might damage the rods. Further, the guide thimble tubes of the fuel
assembly afford additional protection from damage.
During the accumulated thousands of years of burnable absorber rodlet operating experience, only one instance of penetration of the stainless steel burnable absorber cladding has been observed. The consequences of cladding breach are also small. It
is anticipated that upon cladding breach, the B 4 C would be leached by the coolant water and that localized power peaking of a few percent would occur; no design criteria would be violated. Additional information on the consequences of postulated WABA rod
failures is presented in Reference 28.
4.2.3.4.4 Drive Rod Assemblies Design Evaluation
All postulated failures of the drive rod assemblies, either by fracture or uncoupling, lead
to the fail-safe condition. If the drive rod assembly fractures at any elevation, that portion remaining coupled falls with, and is guided by, the RCCA. This always results in a reactivity decrease.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-52 Revision 23 December 2016 4.2.3.4.5 Control Rod Drive Mechanism Design Evaluation The CRDMs are Code Class I components designed to meet the stress requirements for normal operating conditions of the ASME BPV C Section III, Division I, 2001 Edition through 2003 Addenda.
Structural analysis of the CRDMs was performed for normal and faulted conditions as described in Section 5.2.2.1.15.7.
4.2.3.4.5.1 Material Selection Design Evaluation Materials for all pressure-containing CRDM components comply with ASME BPVC Section III and were fabricated from austenitic (Type 304) stainless steel.
Magnetic pole pieces are fabricated from Type 410 stainless steel. All nonmagnetic
parts, except pins and springs, are fabricated from Type 304 stainless steel. Cobalt
alloy is used to fabricate link pins. Springs are made from nickel alloy. Latch arm tips
are clad with Stellite 6 or ERCoCrA to provide improved wearability. Hard chrome plate
and Stellite 6 or ERCoCrA are used selectively for bearing and wear surfaces.
The cast coil housings require a magnetic material. The choice was the ductile iron used in the CRDM. The finished housings are zinc-plated to provide corrosion
resistance.
Coils are wound on bobbins of molded Dow Corning 302 material, with double glass-insulated copper wire. Coils are then vacuum-impregnated with silicon varnish. A wrapping of mica sheet is secured to the coil outer surface. The result is a
well-insulated coil capable of sustained operation at 200°C.
The drive rod assembly uses a Type 410 stainless steel drive rod. The coupling is machined from Type 403 stainless steel. Other parts are Type 304 stainless steel with
the exception of the springs, which are Inconel
-X, and the locking button, which is Haynes 25.
4.2.3.4.5.2 Radiation Damage Design Evaluation As required by the equipment specification, the CRDMs are designed to accommodate
a radiation dose rate of 10 rad/hr. The above radiation level, which amounts to
1.753 x 10 6 rads in 20 years, will not limit CRDM life.
4.2.3.4.5.3 Positioning Requirements Design Evaluation The mechanism has a step length of 5/8 inch that determines the positioning
capabilities of the CRDM. (Note:
Positioning requirements are determined by reactor physics.)
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-53 Revision 23 December 2016 4.2.3.4.5.4 Evaluation of Materials' Adequacy Design Evaluation The ability of the pressure housing components to perform throughout the design
lifetime as defined in the equipment specification is confirmed by the stress analysis
report required by the ASME BPVC Section III.
The CRDM latch assembly may be significantly worn and should be replaced after 6 million individual steps.
4.2.3.4.5.5 Results of Dimensional and Tolerance Analysis
With respect to the CRDM systems as a whole, critical clearances are present in the
following areas:
(1) Latch assembly (diametral clearances)
(2) Latch arm-drive rod clearances (3) Coil stack assembly-thermal clearances (4) Coil fit in coil housing
These clearances have been proven by life tests and actual field performance at
operating plants:
(1) Latch Assembly - Thermal Clearances - The magnetic jack has several clearances where parts made of Type 410 stainless steel fit over parts
made from Type 304 stainless steel. Differential thermal expansion is
therefore important.
(2) Latch Arm - Drive Rod Clearances - The CRDM incorporates a load transfer action. The movable or stationary gripper latch is not under load
during engagement due to load transfer action.
Figure 4.2-25 shows latch clearance variation with the drive rod at
minimum and maximum temperatures. Figure 4.2-26 shows clearance
variations over the design temperature range.
(3) Coil Stack Assembly - Thermal Clearances - The assembly clearance of the coil stack assembly over the latch housing was selected so that the
assembly could be removed under all anticipated conditions of thermal
expansion.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-54 Revision 23 December 2016 (4) Coil Fit in Coil Housing - CRDM and coil housing clearances are selected so that coil heatup results in a close or tight fit. This facilitates thermal transfer and coil cooling in a hot CRDM.
4.2.3.5 Safety Evaluation 4.2.3.5.1 General Design Criterion 2, 1967 - Performance Standards A dynamic seismic analysis is performed on the CRDMs to confirm their ability to trip under a postulated seismic disturbance while maintaining resulting stresses under allowable values (refer to Section 5.2.2.1.15.7).
Additionally, seismic loads (DE, DDE, and HE) are considered on each component, where applicable (refer to Section 3.7.3.15.3).
The containment building, in which the CRDMs are located, is a PG&E Design Class I structure (refer to Section 3.8). As such it is designed to withstand the effects of winds (refer to Section 3.3), floods and tsunamis (refer to Section 3.4), external missiles (refer to Section 3.5), and earthquakes (refer to Section 3.7). This design protects the CRDMs, ensuring their safety function will be performed.
4.2.3.5.2 General Design Criterion 4, 1987
- Environmental and Dynamic Effects Design Bases The LBB methodology was applied to the primary loops of DCPP Unit 1 and Unit 2. The following postulated breaks were eliminated: the six terminal ends in the RCS cold, hot, and crossover legs; a split in the steam generator inlet elbow; and the loop closure weld in the crossover leg. Protection from the dynamic effects of the most limiting breaks of auxiliary lines is considered. RCS branch line breaks and other high energy line breaks are provided. Refer to Section 5.2 for additional discussion of LBB methodology and application.
The LOCA dynamic analyses are based on the accumulator, pressurizer surge, and residual heat removal system RCS branch line breaks credited LBB (Reference 32).
4.2.3.5.3 General Design Criterion 25, 1971 - Protection System Requirements for Reactivity Control Malfunctions The maximum reactivity insertion rate due to withdrawal of RCCAs, or by boron dilution, is limited as discussed in Section 4.3.4.4.
4.2.3.5.4 General Design Criterion 26, 1971 - Reactivity Control System Redundancy and Capability The rod control system relies on gravity to i nsert the rods into the core (refer to Section 4.2.3.3.6). The mechanical design of the reactivity control components provides for the DCPP UNITS 1 &
2 FSAR UPDATE 4.2-55 Revision 23 December 2016 protection of the active elements to prevent the loss of control capability and functional failure of critical components. The components have been reviewed for potential failure and consequences of a functional failure of critical parts (refer to Section 4.2.3.4).
The CVCS regulates the concentration of chemical neutron absorber in the reactor coolant to control reactivity changes resulting from the change in reactor coolant temperature between cold shutdown and hot full power (HFP) operation, burnup of fuel and burnable poisons, and xenon transients (refer to Section 9.3.4).
This documents that the reactivity control system is provided with redundancy and capability such that two independent reactivity control systems of different design principles and capable of reliably controllin g reactivity changes under conditions of normal operation, including anticipated operational occurrences to assure acceptable fuel design limits are not exceeded and that one is capable of holding the reactor core subcritical under cold conditions.
4.2.3.5.5 General Design Criterion 29, 1971 - Protection Against Anticipated Operational Occurrences During plant operation, the stationary gripper coil of the drive mechanism holds the control rod withdrawn from the core in a static position until the movable gripper coil is energized. If power to the stationary gripper coil is cut off, the combined weight of the drive rod assembly and the RCCA is sufficient to move latches out of the drive rod assembly groove. The control rod falls by gravity into the core. After the drive rod assembly is released by the mechanism, it falls freely until the control rods enter the buffer section of their thimble tubes.
4.2.3.5.6 General Design Criterion 30, 1967
- Reactivity Holddown Capability The control and shutdown rod groups provide adequate SDM (refer to Section 4.2.3.3.2) which is defined as: the instantaneous amount of reactivity by which the reactor is subcritical, or would be subcritical from its present condition, assuming (1) all RCCAs are fully inserted, except for the single RCCA of highest reactivity worth which is assumed to be fully withdrawn (with any RCCA not capable of being fully inserted, the reactivity worth of the RCCA must be accounted for in the determination of SDM) and (2) when in MODE 1 or 2, the fuel and moderator temperatures are changed to the hot zero power temperatures.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-56 Revision 23 December 2016 4.2.3.6 Tests and Inspections 4.2.3.6.1 Reactivity Control Components Tests and inspections are performed on each reactivity control component to verify its
mechanical characteristics. For the RCCA, prototype testing has been conducted and
both manufacturing tests/inspections and functional testing are performed at the plant
site.
During the component manufacturing phase, the following requirements apply to the reactivity control components to ensure proper functioning during reactor operation:
(1) To attain the desired standard of quality, all materials are procured to specifications.
(2) For the Westinghouse RCCA and EP-RCCA models only, all spiders are proof tested by an applied load to the spider body which is reacted on by
the 16 peripheral, outermost fingers. This proof load subjects the spider
assembly to a load greater than the acceleration loads caused by the
CRDM stepping.
(3) All cladding/end plug welds are checked for integrity by visual inspection, X-ray, and helium leak tests. All the seal welds in the neutron absorber
rods, burnable absorber rods, and source rods are checked in this
manner. (4) To ensure proper fitup with the fu el assembly, the rod cluster control, burnable absorber, and source assemblies are installed in the fuel
assembly without restriction or binding in the dry condition.
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
The RCCAs are functionally tested following initial core loading, but prior to criticality, to demonstrate reliable operati on of the assemblies. Each assembly is operated (and tripped) once each at the following conditions:
no flow cold, full flow cold, no flow hot, and full flow hot. In addition, the
slowest and fastest rods for each condition are tripped six more times.
Rod drop tests following refueling outages are performed in accordance with the DCPP Technical Specifications (Reference 24) requirements.
4.2.3.6.2 Control Rod Drive Mechanisms The quality assurance program and testing for the CRDMs is discussed in the CRDM component design specification.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-57 Revision 23 December 2016 It is expected that all CRDMs will meet specified operating requirements for the duration of plant life with normal refurbishment. Technical Specifications define actions to be taken for rod group misalignment and rod inoperability.
To demonstrate continuous free movement of the RCCA and to ensure acceptable core
power distributions during operation, partial-movement checks are performed in
accordance with Technical Specifications. In addition, periodic drop tests of the RCCAs are performed at each refueling shutdown to demonstrate continued ability to meet trip time requirements. During these tests, the acceptable trip time of each assembly is not
greater than the requirements listed in the Technical Specifications at full flow and
operating temperature, from decay of the sta tionary gripper voltage to dashpot entry.
Periodic tests are also conducted during plant operation in accordance with the Technical Specifications.
4.2.3.7 Instrumentation Applications Instrumentation for determining reactor coolant average temperature is provided to create demand signals for moving groups of RCCAs to provide load follow (determined as a function of turbine impulse pressure) during normal operation, and to counteract
operational transients. The hot and cold leg resistance temperature detectors (RTDs)
are described in Section 7.2. The reactor control system, which controls the reactor
coolant average temperature by regulation of control rod bank position, is described in Section 7.7.
Rod position indication instrumentation is provided to sense the actual position of each control rod so that it may be displayed to the operator. Signals are also supplied by this system as input to the rod deviation comparator.
The rod position indication system is described in Chapter 7. The CVCS, one of whose functions is to permit adjustment of
the reactor coolant boron concentration for reactivity control (as well as to maintain the
desired operating fluid inventory in the volume control tank), consists of a group of
instruments arranged to provide a manually preselected makeup composition that is
borated or diluted, as required, to the charging pump suction header or the volume
control tank. This system, as well as other systems, including boron sampling
provisions that are part of the CVCS, is described in Section 9.3.4.
When the reactor is critical, the normal indicat ion of reactivity status in the core is the position of the control bank in relation to reactor power (as indicated by the RCS loop T) and coolant average temperature. These parameters are used to calculate insertion limits for the control banks to warn the operator of excessive rod insertion.
Monitoring of the neutron flux for various phases of reactor power operation, as well as
of core loading, shutdown, startup, and refueling is by means of the nuclear
instrumentation system. The monitoring functions and readout and indication
characteristics for the following reactivity monitoring systems are included in the
discussion on the safety parameter display system (SPDS) in Section 7.5:
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-58 Revision 23 December 2016 (1) Nuclear instrumentation system (2) Temperature indicators (a) T average (measured)
(b) T (measured)
(c) Auctioneered T average (3) Demand position of RCCA group (4) Actual rod position indicator.
4.
2.4 REFERENCES
- 1. J. A. Christensen, et al, Melting Point of Irradiated UO 2 , WCAP-6065, February 1965.
- 2. J. Cohen, Development and Properties of Silver-Based Alloys as Control Rod Materials for Pressurized Water Reactors, WAPD-214, December 1959.
- 3. Deleted in Revision 23.
- 4. Deleted in Revision 23.
- 5. F.T. Eggleston, Safety-Related Re search and Development for Westinghouse Pressurized Water Reactors - Program Summaries, Winter 1977 - Summer 1978, WCAP-8768, Revision 2, October 1978.
- 6. Deleted.
- 7. S. Kraus, Neutron Shielding Pads, WCAP-7870, May 1972.
- 8. Westinghouse Electric Company, Operational Experience with Westinghouse Cores, WCAP-8183.
- 9. J. M. Hellman (Ed.), Fuel Densification Experimental Results and Model For Reactor Application, WCAP-8218-P-A, March 1975 (Westinghouse Proprietary) and WCAP-8219-A, March 1975.
- 10. Deleted.
- 11. Deleted.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-59 Revision 23 December 2016
- 12. W. J. O'Donnell and B. F. Langer, "Fatigue Design Basis for Zircaloy Components," Nuclear Science and Engineering, 20, 1-12, 1964.
- 13. E. E. DeMario and S. Nakazato, Hydraulic Flow Test of the 17 x 17 Fuel Assembly, WCAP-8279, February 1974.
- 14. D. H. Risher, et al, Safety Analysi s for the Revised Fuel Rod Internal Pressure Design Basis, WCAP-8963-P-A, August 1978.
- 15. R. A. George, et al, Revised Clad Flattening Model, WCAP-8377 (Westinghouse Proprietary) and WCAP-8381, July 1974.
- 16. Deleted.
- 17. Letter from T. M. Anderson (Westinghouse) to D. G. Eisenhut (NRC), Integrity of Control Rod Guide Thimble, NS-TMA-1936, September 1978.
- 18. Letter from T. M. Anderson (Westinghouse) to D. G. Eisenhut (NRC), Additional Information - Integrity of CRGT, NS-TMA-1992, December 1978.
- 19. Letter from T. M. Anderson (Westinghouse) to D. G. Eisenhut (NRC), Guide Thimble Tube Wear, NS-TMA-2102, June 1979.
- 20. Letter from P. A. Crane (PG&E) to J. F. Stolz (NRC), Response to NRC Questions on Guide Tube Wear, March 1980.
- 21. H. Kunishi and G.R. Schmidt, J. Skaritka (Ed.), Salem Unit 1 17 x 17 Fuel Assembly Guide Thimble Tube Wear Examination Report, Westinghouse Report, January 1982.
- 22. R. L. Cloud, et al. (Ed.), Pressure Vessels and Piping: Design and Analysis, Volume 1, Chapter 1, The American Society of Mechanical Engineers, 1972.
- 23. Regulatory Guide 1.44, Control of the Use of Sensitized Stainless Steel, USNRC, May 1973.
- 24. Technical Specifications, Diablo Canyon Power Plant Units 1 and 2, Appendix A to License Nos. DPR-80 and DPR-82, as amended.
- 25. S. L. Davidson (Ed.), et al, Extended Burnup Evaluation of Westinghouse Fuel, WCAP-10125-P-A, December 1985.
- 26. S. L. Davidson (Ed.), Reference Core Report - VANTAGE 5 Fuel Assembly, WCAP-10444-P-A, September 1985 (Westinghouse Proprietary) and WCAP-10445-NP-A, September 1985.
DCPP UNITS 1 &
2 FSAR UPDATE 4.2-60 Revision 23 December 2016
- 27. S. L. Davidson (Ed.), et al, Verification Testing and Analysis of the 17 x 17 Optimized Fuel Assembly, WCAP-9401-P-A, August 1981.
- 28. J. Skaritka, Westinghouse Wet Annular Burnable Absorber Evaluation Report, WCAP-10021-P-A, Revision 1, October 1983.
- 29. S. L. Davidson (Ed.), et al, VANTAGE+ Fuel Assembly Reference Core Report, WCAP-12610-P-A, April 1995.
- 30. Letter from S.R. Peterson (NRC) to G.M. Rueger (PG&E), Leak-Before-Break Evaluation of Reactor Coolant System Piping for DCPP Units 1 and 2, (Docket Nos. 50-275 and 50-323), March 1993.
- 31. Deleted
- 32. D. Staub, et al., Diablo Canyon Replacemen t Reactor Vessel Closure Head and Integrated Head Assembly Project - Impact of IHA on Reactor Vessel, Internals, Fuel and Loop Piping, WCAP-16946-P, Revision 3, October 2011.
- 33. P. J. Kersting, et al., Assessment of Clad Flattening and Densification Power Spike Factor Elimination in Westinghouse Nuclear Fuel, WCAP-13589-A, March 1995 (Westinghouse Proprietary) and WCAP-14297-A, March 1995.
- 34. J.P. Foster, et al., Westinghouse Improved Performance Analysis and Design Model (PAD 4.0), WCAP-15063-P-A, Revision 1, with Errata, July 2000.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-1 Revision 23 December 2016
4.3 NUCLEAR
DESIGN The nuclear design of the reactors for DCPP Unit 1 and Unit 2, including fuel and reactivity control systems, is described in this section; the analytical methods used in
reactor design and evaluation are also discussed.
Before discussing the nuclear design bases, a brief review of the four major plant
operation conditions, categorized in accorda nce with their anticipated frequency of occurrence and risk to the public, (refer to Section 4.2) are as follows:
(1) Condition I - Normal Operation (2) Condition II - Incidents of Moderate Frequency (3) Condition III - Infrequent Faults (4) Condition IV - Limiting Faults
In general, Condition I occurrences are accommodated with margin between any plant
parameter and the value of that parameter which would require either automatic or
manual protective action. Condition II incidents are accommodated with, at most, a
shutdown of the reactor with the plant capable of returning to operation after corrective
action. Fuel damage (penetration of the fission product barrier; i.e., the fuel rod cladding) is not expected during Conditions I and II events. It is not possible, however, to preclude a very small number of rod failur es. These are within the capability of the plant cleanup system and are consistent with the plant design bases.
Condition III incidents shall not cause more than a small fraction of the fuel elements in
the reactor to be damaged, although sufficient fuel element damage might occur to
preclude immediate resumption of operation. The release of radioactive material due to
Condition III incidents should not be sufficient to interrupt or restrict public use of those areas beyond the exclusion radius. Further more, a Condition III incident shall not, by itself, generate a Condition IV fault or result in a consequential loss of function of the RCS or reactor containment barriers. Condition IV occurrences are faults that are not expected to occur, but are defined as limiting faults that must be considered in design.
Condition IV faults shall not cause a release of radioactive material that results in an undue risk to public health and safety.
The core design power distribution limits related to fuel integrity are met for Condition I
occurrences through conservative design, and maintained by the action of the control
system. The requirements for Condition II occurrences are met by providing an adequate protection system that monitors reactor parameters. The control and protection systems are described in Chapter 7 and the consequences of Conditions II, III, and IV occurrences are discussed in Chapter 15.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-2 Revision 23 December 2016
4.3.1 DESIGN
BASES The design bases and functional requirements for the nuclear design of the fuel and
reactivity control system, and the relationships of these design bases to the GDC of July 1971, are presented in this section. Where appropriate, supplemental criteria, such
as 10 CFR 50.46, are addressed.
4.3.1.1 General Design Criterion 10, 1971 - Reactor Design The reactor core and associated coolant, control and protection systems are designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation, including the effects of anticipated operational occurrences.
4.3.1.2 General Design Criterion 11, 1971 - Reactor Inherent Protection The reactor core is designed so that in the power operating range, the prompt inherent nuclear feedback characteristics tend to compensate for a rapid increase in reactivity.
4.3.1.3 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations The reactor core is designed to assure that power oscillations that could result in conditions exceeding SAFDLs are not possible or can be reliably and readily detected and suppressed.
4.3.1.4 General Design Criterion 25, 1971 - Protection System Requirements for Reactivity Control Malfunctions The reactivity control system is designed to assure that no single malfunction (this does not include rod ejection) causes a violation of the acceptable fuel design limits.
4.3.1.5 General Design Criterion 26, 1971 - Reactivity Control System Redundancy and Capability Two independent reactivity control systems of different design principles are provided.
Each system has the capability to control the rate of reactivity changes resulting from planned, normal power changes. One of the systems is capable of reliably controlling anticipated operational occurrences. In addition, one of the systems is capable of holding the reactor core subcritical under cold conditions.
4.3.1.6 General Design Criterion 28, 1971 - Reactivity Limits The reactivity control systems are designed to assure that the effects of postulated reactivity accidents neither result in damage to the reactor coolant pressure boundary greater than limited local yielding nor cause sufficient damage to significantly impair the capability to cool the core.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-3 Revision 23 December 2016
4.3.2 NUCLEAR
DESIGN ACCEPTANCE CRITERIA 4.3.2.1 Fuel Burnup Sufficient reactivity should be incorporated in the fuel to attain a desired region average discharge burnup.
4.3.2.2 Control of Power Distribution The nuclear design basis, with at least a 95 percent confidence level, is as follows:
(1) The fuel will not be operated at greater than 14.3 kW/ft under normal operating conditions, including an allowance of 2 percent for calorimetric error and not including the power spike factor due to densification effects (Reference 31).
(2) Under abnormal conditions, including the maximum overpower condition, the fuel peak power will not cause melting as defined in Section 4.4.2.2.
(3) The fuel will not operate with a power distribution that violates the DNB design basis (i.e., the departure from nucleate boiling ratio {DNBR} shall not be less than the design limit DNBR, as discussed in Section 4.4.2) under Conditions I and II events, including the maximum overpower
condition.
(4) Fuel management will be such as to produce fuel rod powers and burnups consistent with the assumptions in the fuel rod mechanical integrity
analysis of Section 4.2.
4.3.2.3 Negative Reactivity Feedbacks (Reactivity Coefficients)
The fuel temperature coefficient of reactivity will be negative, and the MTC of reactivity will be nonpositive for full power o perating conditions, thus providing negative reactivity feedback characteristics over the operating range. Below 70 percent power, an MTC of
up to +5 pcm (percent mille)/°F is allowed.
From 70 percent to 100 percent the MTC limit decreases linearly from +5 to 0 pcm/°F.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-4 Revision 23 December 2016 4.3.2.4 Stability Spatial power oscillations within the core, with a constant core power output, should
they occur, can be reliably and readily detected and suppressed.
4.3.2.5 Maximum Controlled Reactivity Insertion Rate The maximum reactivity insertion rate due to withdrawal of RCCAs, or by boron dilution, is limited. This limit, expressed as a maximum reactivity change rate (75 pcm/sec) is set such that the peak heat generation rate does not exceed the maximum allowable, and DNBR is not below the minimum allowable at overpower conditions (refer to Note (b) of Table 4.3-1).
4.3.2.6 Shutdown Margins
Minimum SDM, as specified in the Core Operating Limits Reports, is required in all operational modes.
In all analyses involving reactor trip, the single, highest worth RCCA is postulated to
remain untripped in its full-out position (stuck rod criterion).
4.
3.3 DESCRIPTION
4.3.3.1 Nuclear Design Description The reactor core consists of 193 fuel assemblies arranged in a pattern that approximates a right circular cylinder. Each fuel assembly contains a 17 x 17 rod array composed of 264 fuel rods, 24 RCCA guide tubes, and an incore instrumentation
thimble. Each rod is held in place by spacer grids and top and bottom nozzles. The
fuel rods are constructed of zirconium alloy tubing containing enriched UO 2 fuel pellets.
A limited substitution of fuel rods by filler rods of zirconium alloy or stainless steel may
be made for a particular design if justified by a cycle-specific reload analysis. Figure
4.2-1 shows a cross-sectional view of a fuel assembly and the related RCCA locations.
The fuel assembly design is discussed in Section 4.2.1.
All the fuel rods within a given assembly generally have the same nominal uranium
enrichment. The exceptions are that the top and bottom portions of the rods may contain a low enriched or natural uranium blanket and that some assemblies may
contain more than one enrichment as a result of reconstitution operations. Figure 4.3-1
shows a typical equilibrium 18-month cycle core loading of fresh and burned fuel
assemblies. This "typical" loading pattern is modified for fuel cycles of longer length to
accommodate the needed additional cycle energy.
A typical reload pattern employs low leakage fuel management in which more highly
burned fuel is placed on the core periphery.
Reload cores will operate approximately 12 months to 24 months between refuelings. The feed fuel enrichment is determined by DCPP UNITS 1 &
2 FSAR UPDATE 4.3-5 Revision 23 December 2016 the amount of fissionable material required to provide the desired core lifetime and energy production. Reactivity losses due to U-235 depletion and the buildup of fission
products are partially offset by the buildu p of plutonium produced by the capture of neutrons in U-238, as shown in Figure 4.3-2.
At the beginning of any cycle, an excess reactivity to compensate for these losses over the specified cycle life must be "built" into
the reactor. This excess reactivity is controlled by removable neutron absorbing
material in the form of boron dissolved in the primary coolant and burnable absorber rods or boron coated fuel pellets.
Boric acid concentration in the primary coolant is varied to control and to compensate
for long-term reactivity requirements, such as those due to fuel burnup, fission product
poisoning, including xenon and samarium, burnable absorber material depletion, and the cold-to-operating moderator temperature change. Using its normal makeup path, the CVCS is capable of inserting negative reactivity at a rate of approximately 30 pcm/min when the reactor coolant boron concentration is 100 ppm. In an emergency, the CVCS can insert negative reactivity at approximately 65 pcm/min when
the reactor coolant concentration is 1000 ppm, and 75 pcm/min when the reactor
coolant boron concentration is 100 ppm. The peak xenon burnout rate is 25 pcm/min (Section 9.3.4 discusses the capability of the CVCS to counteract xenon decay). Rapid
transient reactivity requirements and safe shutdown requirements are met with control
rods.
As the boron concentration increases, the MTC becomes less negative. Using soluble
poison alone would result in a positive MTC at BOL at full power operating conditions.
Therefore, burnable absorber and IFBA rods are used to reduce the soluble boron concentration sufficiently to ensure that the MTC is not positive for full power operating conditions. During operation, the absorber content in these rods is depleted, thus adding positive reactivity to offset some of the negative reactivity from fuel depletion and fission product buildup. The depletion rate of the burnable absorber material is not critical since chemical shim is always available and flexible enough to cover any possible deviations in the expected burnable absorber depletion rate. Figure 4.3-3 shows typical core depletion curves with burnable absorbers.
In addition to reactivity control, the burnable absorbers are strategically located to
provide a favorable radial power distribution. Figures 4.3-4 and 4.3-5 show the typical
burnable absorber distribution within a fuel assembly for the several burnable absorber
patterns used for both discrete and IFBAs. The burnable absorber loading pattern for a typical equilibrium cycle reload core is shown in Figure 4.3-6.
Tables 4.1-1, and 4.3-1 through 4.3-3, summarize the reactor core design parameters
for a typical reload fuel cycle, including reactivity coefficients, delayed neutron fraction, and neutron lifetimes.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-6 Revision 23 December 2016 4.3.3.2 Power Distribution DCPP employs two methods for performing core power distribution calculations: the power distribution monitoring system (PDMS) and the movable incore detector system (MIDS). .
The PDMS generates a continuous measurement of the core power distribution using the methodology documented in References 32 and 33. The measured core power
distribution is used to determine the most limiting core peaking factors, which are used
to verify that the reactor is operating within the design limits.
The PDMS requires information on current plant and core conditions in order to
determine the core power distribution using the core peaking factor measurement and
measurement uncertainty methodology described in References 32 and 33. The core
and plant condition information is used as input to the continuous core power
distribution measurement software that continuously and automatically determines the
current core peaking factor values. The core power distribution calculation software
provides the measured peaking factor values at nominal one-minute intervals to allow
operators to confirm that the core peaking factors are within design limits. In order for
the PDMS to accurately determine the peaking factor values, the core power distribution
measurement software requires accurate information about the current reactor power
level average reactor vessel inlet temperature, control bank positions, the power range
detector currents, and the core exit thermocouples.
Data obtained from the MIDS, described in Section 7.7.2.9.2, are used to calibrate the PDMS, and may also be used independent of the PDMS to generate a flux map of the core power distribution. The accuracy of these power distribution calculations has been confirmed under conditions similar to those expected for DCPP, as discussed in References 1 and 3 and in Section 4.3.3.2.7.
4.3.3.2.1 Definitions Power distributions are quantified in terms of hot channel factors. These factors are a
measure of the peak pellet power within the reactor core and the total energy produced
in a coolant channel and are expressed in terms of quantities related to the nuclear or
thermal design; namely:
Power density is the thermal power produced per unit volume of the core (kW/liter).
Linear power density is the thermal power produced per unit length of active fuel (kW/ft).
Since fuel assembly geometry is standardized, this is the unit of power density most
commonly used. For all practical purposes, it differs from kW/liter by a constant factor that includes geometry effects and the frac tion of the total thermal power which is generated in the fuel rods.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-7 Revision 23 December 2016 Average linear power density is the total thermal power produced in the fuel rods divided by the total active fuel length of all rods in the core.
Local heat flux is the heat flux at the surface of the cladding (Btu ft
-2 hr-1). For nominal fuel rod parameters, this differs from linear power density by a constant factor.
Rod power or rod integral power is the linear power density in one rod integrated over
its length (kW).
Average rod power is the total thermal power produced in the fuel rods divided by the number of fuel rods.
The hot channel factors used in the discussion of power distributions in this section are
defined as follows:
F T Q , heat flux hot channel factor , is defined as the maximum local heat flux on the surface of a fuel rod divided by the average fuel rod heat flux, allowing for manufacturing tolerances on fuel pellets and rods.
F N Q , nuclear heat flux hot channel factor , is defined as the maximum local fuel rod linear power density divided by the average fuel rod linear power density, assuming nominal
fuel pellet and rod parameters. (No densification effects included.)
F E Q , engineering heat flux hot channel factor , is the allowance on heat flux required for manufacturing tolerances. The engineering factor allows for local variations in
enrichment, pellet density and diameter, surface area of the fuel rod, and eccentricity of the gap between pellet and clad.
Combined statistically, the net effect is a factor of 1.03 to be applied to the fuel rod surface heat flux.
F N H, nuclear enthalpy rise hot channel factor , is defined as the ratio of the integral of linear power along the rod with the highest integrated power to the average rod power.
Manufacturing tolerances, hot channel powe r distribution, and surrounding channel power distributions are treated explicitly in the calculation of DNBR described in Section 4.4.
For the purposes of discussion, it is convenient to define subfactors of F T Q; design limits are set, however, in terms of the total peaking factor:
F T Q factor channel hotflux heat or factor peaking Total
=
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-8 Revision 23 December 2016 kW/ft AveragekW/ft Maximum
= (4.3-1) without densification effects.
F T Q = F N Qx F E Q = max [F N XY (z) x P(z)] x F N U x F E Q (4.3-2) where: F N Q and F E Q are defined above.
F N U = the measurement uncertainty associated with a full core flux map with movable detectors or PDMS F N XY(z) = ratio of peak power density to average power density in the horizontal plane of peak local power P(z) = ratio of the power per unit core height in the horizontal plane at elevation Z to the average value of power per unit core height 4.3.3.2.2 Radial Power Distributions
The power shape in horizontal sections of the core at full power is a function of the fuel and burnable absorber loading patterns, and the presence or absence of a single bank
of control rods. Thus, at any time in the cycle, any horizontal section of the core can be
characterized as unrodded, or with control banks inserted. These two situations, combined with burnup effects, determine the radial power shapes that can exist in the core at full power. The effects on radial po wer shapes of power level, xenon, samarium, and moderator density effects are also considered, but these are smaller. While radial
power distributions in various planes of the core are often illustrated, the core radial enthalpy rise distribution, as determined by the power integral of each channel, is of
greater interest. Figures 4.3-7 through 4.3-12 show representative radial power
distributions for one-eighth of the core for representative operating conditions during the
initial cycle, as follows:
Figure Conditions 4.3-7 HFP at BOL unrodded no xenon 4.3-8 HFP at BOL unrodded equilibrium xenon 4.3-9 HFP at BOL Bank D in equilibrium xenon - Unit 1 4.3-10 HFP at BOL Bank D in equilibrium xenon - Unit 2 4.3-11 HFP at middle of life (MOL) unrodded equilibrium xenon, and 4.3-12 HFP at EOL unrodded equilibrium xenon.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-9 Revision 23 December 2016 Since hot channel location varies from time to time, a single reference radial design power distribution is selected for DNB calculations. This reference power distribution, normalized to core average power, is chosen conservatively to concentrate power in
one area of the core, minimizing the benefits of flow redistribution.
4.3.3.2.3 Assembly Power Distributions
For the purpose of illustration, assembly power distributions for the BOL and EOL
conditions corresponding to Figures 4.3-8 and 4.3-12 are given for the same assembly
in Figures 4.3-13 and 4.3-14, respectively.
Since the detailed power distribution surrounding the hot channel varies from time to
time, a conservatively flat assembly power distribution is assumed in the DNB analysis, described in Section 4.4, with the rod of maximum integrated power artificially raised to the design value of F N H. The nuclear design considers all fuel cycles and all operating conditions to ensure that a flatter assembly power distribution does not occur with
limiting values of F N H. 4.3.3.2.4 Axial Power Distributions The shape of the power profile in the axial direction is largely under the control of the
operator through the manual operation of the control rods or the automatic motion of the control rods responding to manual operation of the CVCS. Nuclear effects that cause variations in the axial power shape include moderator density, Doppler effect on
resonance absorption, spatial xenon variatio ns, fuel and burnable absorber material distribution and burnup. Automatically controlled variations in total power output and control rod motion are also important in determining the ax ial power shape at any time.
Signals are available to the operator from the excore ion chambers that run parallel to the axis of the core. Separate signals are taken from the top and bottom halves of the
chambers. The difference between top and bottom signals for each of four pairs of detectors is called the flux difference, . If it deviates from the flux difference target band, an alarm is actuated.
Calculations of core average peaking factor for many plants and measurements from operating situations are associated with either or axial offset (AO) to place an upper bound on the peaking factor. For these correlations, AO is defined as:
AO = btbt+ (4.3-4) where: t and b are the top and bottom detector readings.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-10 Revision 23 December 2016 Representative axial power shapes for BOL, MOL , and EOL conditions covering a wide range, including power shape changes achieved by skewing xenon distributions, are shown in Figures 4.3-15 through 4.3-17.
4.3.3.2.5 Local Power Peaking Fuel densification causes fuel pellets to shrin k both axially and radially. Pellet shrinkage combined with random hang-up of fuel pellets results in gaps in the fuel column when
the pellets below the hung-up pellet settle in the fuel rod. The gaps vary in length and
location in the fuel rod. Because of decreased neutron absorption in the vicinity of the
gap, power peaking occurs in the adjacent fuel rods resulting in an increased power
peaking factor. A quantitative measure of this local power peaking is given by the
power spike factor S(z) where z is the axial location in the core.
In previous analyses of power peaking factors for DCPP Unit 1 and Unit 2, it was necessary to apply a penalty on calculated overpower transient F Q values to allow for interpellet gaps caused by pellet hang-ups a nd pellet shrinkage due to densification (Reference 22). This penalty is known as the densification spike factor. However, studies have shown (Reference 31) that this penalty can be eliminated for the fuel type present in the DCPP Unit 1 and Unit 2 cores.
4.3.3.2.6 Limiting Pow er Distributions
As discussed in Section 4.3, Condition I occurrences are those expected frequently or regularly in the course of power operation, m aintenance, or maneuvering of the plant.
Condition I occurrences are accommodated with margin between any plant parameter and the value of that parameter that would require either automatic or manual protective action. Since they occur frequently or regularly, Condition I occurrences affect the
consequences of Conditions II, III, and IV events. Analysis of each fault condition is
generally based on a conservative set of initial conditions corresponding to the most
adverse set of conditions that can occur during a Condition I event.
The list of steady state and shutdown conditions, permissible deviations, and
operational transients is given in Section 15.1. Implicit in the definition of normal
operation is proper and timely action by the reactor operator. That is, the operator
follows recommended operating procedures for maintaining appropriate power
distributions and takes any necessary remedial actions when alerted to do so by plant
instrumentation. Thus, as stated above, the worst or limiting power distribution that can
occur during normal operation is considered as the starting point for analysis of
Conditions II, III, and IV events.
Improper procedural actions or errors by the operator are assumed in the design as occurrences of moderate frequency (Condition II).
The limiting power shapes that result from such Condition II events are, therefore, those power shapes, which deviate from the normal operating condition at the recommended AO band. Power shapes that fall in DCPP UNITS 1 &
2 FSAR UPDATE 4.3-11 Revision 23 December 2016 this category are used to determine reactor protection system setpoints in order to maintain margin to overpower or DNB limits.
Maintaining power distributions within the required hot channel factor limits is discussed in the Technical Specifications. A complete discussion of power distribution control in
Westinghouse PWRs is included in References 2, 29, and 30. Detailed background information on the following design constraints on local power density in a
Westinghouse PWR, on the defined operating procedures, and on the measures taken to preclude exceeding design limits is presented in References 23, 29, and 30.
The upper bound on peaking factors, F T Q and F N H, includes all of the nuclear effects that influence the radial and/or axial power distributions throughout core life for various modes of operation, including load follow, reduced power operation, and axial xenon
Radial power distributions are calculated for full power, and fuel and moderator
temperature feedback effects are included for the average enthalpy plane of the reactor.
Steady state nuclear design calculations are done for normal flow with the same mass
flow in each channel and flow redistribution is calculated explicitly where it is important to the DNB analysis of accidents. The effect of xenon on radial power distribution is
small (compare Figures 4.3-7 and 4.3-8), but is included as part of the normal design
process.
The core average axial profile can experien ce significant changes that can occur rapidly as a result of rod motion and load changes, and more slowly due to xenon distribution.
To study points of closest approach to axial power distribution limits, several thousand
cases are examined. Since the nuclear design properties dictate what axial shapes can occur, the limits of interest can be set in terms of parameters that are readily observed.
Specifically, the following nuclear design parameters are significant to the axial power distribution analysis:
(1) Core power level (2) Core height (3) Coolant temperature and flow (4) Coolant temperature program as a function of reactor power (5) Fuel cycle lifetimes (6) Rod bank worths (7) Rod bank overlaps
Normal plant operation assumes compliance with the following conditions:
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-12 Revision 23 December 2016 (1) Control rods in a single bank move together with no individual rod insertion differing by more than 12 steps (indicated) from the bank demand position (2) Control banks are sequenced with overlapping banks (3) Control bank insertion limits are not violated (4) Axial power distribution procedures, which are given in terms of flux difference control and control bank position, are observed.
The above axial power distribution procedures are part of the normal plant operating procedures. Briefly, they require control of the AO (refer to Equation 4.3-4) at all power levels, within a permissible operating band. This minimizes xenon transient effects on the axial power distribution, since the procedures essentially keep the xenon distribution
in phase with the power distribution.
Calculations are performed for normal reactor operation at beginning, middle, and end
of cycle conditions. Different operation histories are implicitly included in the
methodology. These different histories cover both base loaded operation and extensive
load following.
These cases represent many possible reactor states in the life of one fuel cycle. They
are considered to be necessary and sufficient to generate a local power density limit which, when increased by 5 percent for conservatism, will not be exceeded with a 95 percent confidence level. Many of the points do not approach the limiting envelope.
However, they are generated as part of the process that leads to the shapes, which do
define the envelope.
Thus, it is not possible to single out any transient or steady state condition that defines
the most limiting case. It is not even possible to separate out a small number, which form an adequate analysis. The process of generating a myriad of shapes is essential
to the philosophy that leads to the required level of confidence. A set of parameters that
produces a limiting case for one reactor fuel cycle (defined as approaching the line of
Figure 4.3-23) is not necessarily a limiting case for another reactor or fuel cycle with
different control bank worths or insertion limits, enrichments, burnup, reactivity
coefficient, etc. The shape of the axial power distribution calculated for a particular time
depends on the operating history of the core up to that time, and on the manner in
which the operator conditioned xenon in the days immediately before that time.
The calculated points are synthesized from ax ial calculations combined with the radial factors appropriate for rodded and unrodded planes. In these calculations, the effects
on the radial peak of xenon redistribution tha t occur, following the withdrawal of a control bank (or banks) from a rodded region, are obtained from three-dimensional calculations. The factor to be applied to the radial peak is obtained from calculations in DCPP UNITS 1 &
2 FSAR UPDATE 4.3-13 Revision 23 December 2016 which the xenon distribution is preconditioned by the presence of control rods and then allowed to redistribute for several hours. A d etailed discussion of this effect may be found in References 23 and 29. In addition to the 1.05 conservatism factor, the calculated values are increased by a factor of 1.03 for the engineering factor F E Q.
The envelope drawn over the calculated (max F T Q x Power) points, as shown in Figure 4.3-23 is an example of an upper bound envelope on local power density versus elevation in the core.
Cycle-specific values are calculated each cycle.
Finally, this upper bound envelope is based on operation within an allowed range of axial flux difference limits. These limits are detailed in the Core Operating Limits Reports and rely only on excore surveillance supplemented by the required normal
monthly power distribution measurement. If the axial flux difference exceeds the allowable range, an alarm is actuated.
Allowing for fuel densification, the average linear power is 5.445 kW/ft for both units at
3,411 MWt. The conservative upper bound value of normalized local power density, including uncertainty allowances, is 2.58, corresponding to a peak linear power of
14.3 kW/ft at 102 percent power.
To determine reactor protection system setpoints, with respect to power distributions, three categories of events are considered: rod control equipment malfunctions, operator errors of commission, and operator errors of omission. In evaluating these three categories, the core is assumed to be operating within the four constraints
described above.
The first category is uncontrolled rod withdrawal (with rods moving in the normal bank
sequence). Also included are motions of the banks below their insertion limits, which
could be caused, for example, by uncontrolled dilution or primary coolant cooldown.
Power distributions were calculated, assuming short-term corrective action. That is, no
transient xenon effects were considered to result from the malfunction. The event was
assumed to occur from typical normal operating situations, which include normal xenon
transients. It was also assumed that the total power level would be limited by the reactor trip to below 118 percent. Results are given in Figure 4.3-21 in units of kW/ft.
The peak power density, which can occur in such events, assuming reactor trip at or
below 118 percent, is less than that required for fuel centerline melt, including
uncertainties.
The second category, also appearing in Figure 4.3-21, assumes that the operator
mispositions the rod bank in violation of insertion limits and creates short-term
conditions not included in normal operating conditions.
The third category assumes that the operator fails to take action to correct a flux difference violation. The results shown in Figure 4.3-22 are F T Q multiplied by 102 percent power, including an allowance for calorimetric error. The peak linear power DCPP UNITS 1 &
2 FSAR UPDATE 4.3-14 Revision 23 December 2016 does not exceed 22.0 kW/ft, provided the operator's error does not continue for a period which is long compared to the xenon time constant. It should be noted that a reactor
overpower accident is not assumed to occur coincident with an independent operator
error. Additional detailed discussion of these analyses is presented in Reference 23.
Analyses of possible operating power shapes for the DCPP reactor show that the appropriate hot channel factors F T Q and F N H for peak local power density, and for DNB analysis at full power, are the values given in Table 4.3-1 and addressed in the Technical Specifications.
The maximum allowable F T Q can increase with decreasing power, as shown in the Technical Specifications. Increasing F N H with decreasing power is permitted by the DNB protection setpoints and allows radial power shape changes with rod insertion to the insertion limits, as described in Section 4.4.3.13.
The allowances for increased F N H permitted is:
F N H = 1.65 [1 + 0.3 (1-P)] for VANTAGE+ fuel (4.3-5) This becomes a design basis criterion, which is used for establishing acceptable control rod patterns and control bank sequencing.
Likewise, fuel loading patterns for each cycle are selected with consideration of this design criterion. The worst values of F N H for possible rod configurations occurring in normal operation are used in verifying that this criterion is met. Typical radial factors and radial power distributions are shown in
Figures 4.3-7 through 4.3-12. The worst values generally occur when the rods are
assumed to be at their insertion limits. As discussed in Reference 3, it has been
determined that the Technical Specification limits are met, provided the above conditions (1) through (4) are observed. These limits are taken as input to the
thermal-hydraulic design basis, as described in Section 4.4.3.13.1.
If the possibility exists during normal operation of local power densities exceeding those assumed as the precondition for a subsequent hypothetical accident, but which would
not itself cause fuel failure, administrative controls and alarms are provided to return the
core to a safe condition. These alarms are described in Chapter 7 and in the Technical
Specifications.
4.3.3.2.7 Experimental Verification of Power Distribution Analysis This subject, which is discussed in depth in Reference 1, is summarized here.
To measure the peak local power density, F T Q , with the movable detector system described in Sections 4.4.7 and 7.7.2.9.2, the following uncertainties are considered:
(1) Reproducibility of the measured signal
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-15 Revision 23 December 2016 (2) Errors in the calculated relationship between detector current and local flux (3) Errors in the calculated relationship between detector flux and peak rod power some distance from the measurement thimble Allowance for (1) has been quantif ied by repetitive measurements made with several intercalibrated detectors using the common thimble features of the incore detector
system. This system allows more than one detector to access any thimble. Item (2) above is quantified to the extent possible by using the fluxes measured at one thimble
location to predict fluxes at another location, which is also measured. Local power
distribution predictions are verified in critical experiments on arrays of rods with
simulated guide thimbles, control rods, burnable poisons, etc.
Reference 1 concludes that the uncertainty associated with the peak nuclear heat flux factor, F T Q , is 4.58 percent at the 95 percent confidence level with only 5 percent of the measurements greater than the inferred value.
In comparing measured power distributions (or detector currents) against the
calculations for the same situations, it is not possible to subtract out the detector reproducibility. Thus, a comparison between measured and predicted power
distributions must consider measurement error. Such a comparison is illustrated in
Figure 4.3-25 for one of the maps of Reference 1, which is similar to hundreds of maps
taken since then on various reactors, confirming the adequacy of the 5 percent uncertainty allowance on F T Q. A similar analysis for the uncertainty in F N H (rod integral power) measurements results in an allowance of 3.68 percent at the equivalent of a 2 confidence level. For historical reasons, an 8 percent uncertainty factor is allowed in the nuclear design basis; that is, the predicted rod integrals at full power must not exceed the design F N H less 8 percent.
This 8 percent may be reduced in final design to 4 percent to allow a wider range of acceptable axial power distributions in the DNB analysis and still meet the acceptance criteria of Section 4.3.2.2.
A measurement in the second cycle of a 121-assembly, 12-foot core, was compared with a simplified one-dimensional core average axial calculation in Figure 4.3-26. This
calculation does not give explicit representation to the fuel grids.
The accumulated data on power distributions in actual operation is basically of three
types:
(1) Much of the data is obtained in steady state operation at constant power in the normal operating configuration.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-16 Revision 23 December 2016 (2) Data with unusual values of AO are obtained as part of the excore detector calibration exercise which is performed monthly.
(3) Special tests have been performed in load follow and other transient xenon conditions which have yielded useful information on power distributions.
These data are presented in detail in Reference 3. Figure 4.3-27 contains a summary of measured values of F T Q as a function of AO for five plants from that report.
4.3.3.2.8 Testing An extensive series of physics tests is performed on first cores. These tests and the
criteria for satisfactory results are described in detail in Chapter 14. Since not all
limiting situations can be created at BOL, the main purpose of the tests is to provide a
check on the calculation methods used in the predictions for the conditions of the test.
Physics testing is also performed at the beginning of each reload cycle to ensure that
the operating characteristics of the core are consistent with design predictions.
4.3.3.2.9 Monitoring Instrumentation The adequacy of instrument numbers, spatial deployment, and required correlations between readings and peaking factors, calibration, and errors is described in
References 1, 2, and 3. The relevant conclusions are summarized in Sections 4.3.3.2.7 and 4.4.7.
References 32 and 33 describe the instrumentation requirements and calibration of the PDMS, and the uncertainties applied to the calculated peaking factors.
If the limitations given in Section 4.3.3.2.6 on rod insertion and flux difference are observed, the excore detector system provi des adequate monitoring of power distributions.
Further details of specific limits on the observed rod positions and flux difference are
given in the Core Operating Limits Reports, together with a discussion of their bases.
Limits for alarms, reactor trip, etc., are given in the Technical Specifications. System
descriptions are provided in Section 7.7.
4.3.3.3 Reactivity Coefficients Reactor core kinetic characteristics determine the response of the core to changing
plant conditions, or to operator adjustments made during normal operation, as well as
the core response during abnormal or accidental transients. These kinetic characteristics are quantified in reactivity coefficients. The reactivity coefficients reflect changes in the neutron multiplication due to varying plant conditions such as power, DCPP UNITS 1 &
2 FSAR UPDATE 4.3-17 Revision 23 December 2016 moderator or fuel temperatures, or, less significantly, due to a change in pressure or void conditions. Since reactivity coefficients change during the life of the core, ranges
of coefficients are employed in transient analysis to determine the response of the plant
throughout life. The analytical methods and calculati onal models used in calculating the reactivity coefficients are given in Section 4.3.3.10.
4.3.3.3.1 Fuel Temperature (Doppler) Coefficient The fuel temperature (Doppler) coefficient is defined as the change in reactivity per
degree change in effective fuel temperature and is primarily a measure of the Doppler
broadening of U-238 and Pu-240 resonance absorption peaks. Doppler broadening of
other isotopes such as U-236, Np-237, etc., are also considered, but their contributions
to the Doppler effect is small. An increase in fuel temperature increases the effective
resonance absorption cross-sections of the fuel and produces a corresponding reduction in reactivity.
The fuel temperature coefficient is calculated by two-group two or three-dimensional
calculations. Moderator temperature is held constant and the power level is varied.
Spatial variation of fuel temperature is taken into account by calculating the effective
fuel temperature as a function of power density, as discussed in Section 4.3.3.10.1.
The Doppler temperature coefficient is shown in Figure 4.3-28 as a function of the
effective fuel temperature (at BOL and EOL conditions). The effective fuel temperature
is lower than the volume averaged fuel temperature since the neutron flux distribution is
nonuniform through the pellet and gives preferential weight to the surface temperature.
The Doppler-only contribution to the power coefficient (defined later) is shown in Figure 4.3-29 as a function of percent core power. The integral of the differential curve in Figure 4.3-29 is the Doppler contribution to the power defect and is shown in Figure 4.3-30 as a function of percent power. The Doppler coefficient changes as a function of core life, representing the combined effects of the fuel temperature reduction with burnup and the buildup of Pu-240 (refer to Section 4.3.3.10.1). The upper and lower limits of Doppler coefficient used in accident analyses are given in Chapter 15.
4.3.3.3.2 Moderator Coefficients The moderator coefficient is a measure of the change in reactivity due to a change in
specific coolant parameters such as density, temperature, pressure, or void.
4.3.3.3.2.1 Moderator Density and Temperature Coefficients The MTC (density) is defined as the change in reactivity per degree change in the
moderator temperature. Generally, the effect of the changes in moderator density, as well as the temperature, are considered together. A decrease in moderator density
means less moderation which results in a negative MTC. An increase in coolant
temperature, keeping the density constant, leads to a hardened neutron spectrum
resulting in greater resonance absorption in U-238, Pu-240, and other isotopes. The DCPP UNITS 1 &
2 FSAR UPDATE 4.3-18 Revision 23 December 2016 hardened spectrum also causes a decrease in the fission to capture ratio in U-235 and Pu-239. Both of these effects make the MTC more negative. Since water density decreases as temperature increases, the MTC (density) becomes more negative with increasing temperature.
The soluble boron also affects the MTC (density) since its density, like that of water, also decreases when the coolant temperature rises. Therefore, a decrease in the
soluble poison concentration introduces a positive component into the moderator
coefficient. Indeed, if the concentration of soluble poison is large enough, the net value
of the coefficient may be positive. With the burnable poison rods present, however, the
initial hot boron concentration is sufficiently low, making the MTC negative at full power
operating temperatures. The effect of control rods is to make the moderator coefficient more negative by reducing the required soluble boron concentration and by increasing "leakage" from the core.
With burnup, the MTC normally becomes more negative primarily as a result of boric
acid dilution, but also, to a significant extent, from the effects of plutonium and fission
products buildup.
The MTC is calculated for various plant conditions by performing two-group two or three
dimensional calculations, varying the moderator temperature (and density) by about
+/-5°F about each of the mean temperatures. The MTC is shown in Figures 4.3-31 through 4.3-33 as a function of core temperature and boron concentration for a typical reload unrodded and rodded core. The temperature range covered is from cold (68°F)
to about 600°F. The contribution due to Doppler coefficient (because of change in moderator temperature) has been subtracted from these results. Figure 4.3-34 shows
the hot, full power MTC as a function of cycle lifetime for the critical boron concentration condition based on the design boron letdown condition (refer to Figure 4.3-3) for a typical reload cycle.
4.3.3.3.2.2 Moderator Pressure Coefficient The moderator pressure coefficient relates the change in moderator density, resulting
from a reactor coolant pressure change, to the corresponding effect on neutron
production. This coefficient is of much less signific ance than the MTC. A change of 50 psi in pressure has approximately the same effect on reactivity as a half-degree
change in moderator temperature. This coefficient can be determined from the MTC by
relating change in pressure to the corresponding change in density. The moderator
pressure coefficient is negative over a portion of the moderator temperature range at
BOL (-0.004 pcm/psi, BOL) but is always positive at operating conditions and becomes
more positive during life (+0.3 pcm/psi, EOL).
4.3.3.3.2.3 Moderator Void Coefficient The moderator void coefficient relates the change in neutron multiplication to the
presence of voids in the moderator. In a PWR, this coefficient is not very significant DCPP UNITS 1 &
2 FSAR UPDATE 4.3-19 Revision 23 December 2016 because of the low void content in the coolant. The core void content is less than one-half of 1 percent and is due to local or statistical boiling. The void coefficient varies from 50 pcm/% void at BOL and low temperatures to -250 pcm/% void at EOL and at
operating temperatures. The negative void coefficient at operating temperature
becomes more negative with fuel burnup.
4.3.3.3.3 Power Coefficient The combined effect of moderator temperature and fuel temperature change as the core
power level changes is called the total power coefficient, and is expressed in terms of
reactivity change per percent power change. The power coefficient at BOL, MOL, and EOL conditions is given in Figure 4.3-35. It becomes more negative with burnup, reflecting the combined effect on moderator and fuel temperature coefficients of burnup.
The power defect (integral reactivity effect) at BOL, MOL, and EOL is given in Figure 4.3-36.
4.3.3.3.4 Comparison of Calculated and Experimental Reactivity Coefficients The accuracy of the current analytical model is discussed in Section 4.3.3.10.3.
Experimental verification of the calculated coefficients was performed during the physics startup tests described in Chapter 14.
4.3.3.3.5 Reactivity Coefficients Used in Transient Analysis Table 4.3-1 gives representative ranges for the reactivity coefficients used in the transient analysis. The exact values of the coefficient used in the analysis depend on whether the transient of interest is examined at the BOL or EOL, whether the most
negative or the most positive (least negative) coefficients are appropriate, and whether
spatial nonuniformity must be considered in the analysis. Conservative values of coefficients are always used in the transient analysis, as described in Chapter 15.
The values listed in Table 4.3-1, and illustrated in Figures 4.3-29 through 4.3-36, apply
to the core shown in Figure 4.3-1. Appropriate coefficients for use in other cycles
depend on the core's operating history, the number and enrichment of fresh fuel assemblies, the loading pattern of burned and fresh fuel, and the number and location
of any burnable poison rods. The need for a reevaluation of any accident in a subsequent cycle is contingent on whether or not the coefficients for that cycle fall within
the range used in the analysis presented in Chapter 15. For information only, control rod requirements are given in Tables 4.3-2 and 4.3-3 for a hypothetical equilibrium cycle. 4.3.3.4 Control Requirements To ensure SDM availability under cooldown to ambient temperature conditions, concentrated soluble boron is added to the coolant. Boron concentrations for several DCPP UNITS 1 &
2 FSAR UPDATE 4.3-20 Revision 23 December 2016 core conditions are listed in Table 4.3-1. They are all well below the solubility limit. The RCCAs are employed to bring the reactor to t he hot shutdown condition. The minimum SDM required is given in the Core Operating Limits Reports.
The ability to shut down from hot conditions is demonstrated in Tables 4.3-2 and 4.3-3 by comparing the difference between the reactivity available in the RCCA, allowing for
the rod with the highest worth being stuck, with that required for control and protection.
The SDM allows 10 percent for analytic uncertainties (refer to Section 4.3.3.4.9). The largest reactivity control requirement appears at EOL when the MTC reaches its peak
negative value as reflected in the larger power defect.
Control rods are required to provide sufficient reactivity to compensate for the power
defect from full power to zero power and the required SDM. The reactivity addition resulting from power reduction consists of contributions from Doppler, variable average
moderator temperature, flux redistribution, and reduction in void content.
4.3.3.4.1 Doppler Control requirements to compensate for the Doppler effect are listed in Tables 4.3-2 and
4.3-3, for DCPP Unit 1 and Unit 2, respectively.
4.3.3.4.2 Variable Average Moderator Temperature When the core is shut down to the hot zero power condition, the average moderator
temperature changes from the equilibrium full load value, determined by the steam
generator and turbine characteristics (such as steam pressure, heat transfer, and tube fouling), to the equilibrium no-load value, whi ch is based on the steam generator shell side design pressure. The design change in temperature is conservatively increased by 4°F to account for control dead band measurement errors.
Since the moderator coefficient is negative, there is a reactivity addition with power
reduction. The MTC becomes more negative as the fuel depletes because the boron
concentration decreases. This effect is the major contribution to the increased
requirement at EOL.
4.3.3.4.3 Redistribution During full power operation, the coolant density decreases with core height and this, together with partial insertion of control rods, results in less fuel depletion near the top of
the core. Under steady state conditions, the relative power distribution will be slightly
asymmetric towards the bottom of the core.
On the other hand, at hot zero power conditions, the coolant density is uniform and there is no flattening due to Doppler. The
result is a flux distribution that at zero power can be skewed toward the top of the core.
The reactivity insertion due to the skewed distribution is calculated with an allowance for
the most adverse effects of xenon distribution.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-21 Revision 23 December 2016 4.3.3.4.4 Void Content A small void content in the core is due to nucleate boiling at full power. The void
collapse that results from a power reduction makes a small reactivity contribution.
4.3.3.4.5 Rod Insertion Allowance At full power, the control bank is operated within a prescribed travel band to
compensate for small periodic changes in boron concentration, temperature, and very small changes in the xenon concentration not compensated for by a change in boron
concentration. When the control bank reaches either limit of this band, a change in
boron concentration is required to compensate for additional reactivity changes. Since
the insertion limit is set by a rod travel limit, a conservatively high calculation of the
inserted worth is made which exceeds the normally inserted reactivity.
4.3.3.4.6 Burnup Excess reactivity of 10 percent to 25 percent (hot) is installed at the beginning of each cycle to provide sufficient reactivity to compensate for fuel depletion and fission products buildup throughout the cycle. This reactivity is controlled by the addition of
soluble boron to the coolant and by burnable absorber. Representative soluble boron concentrations for several core configurations and the boron coefficient in the primary coolant are given in Table 4.3-1. Since the excess reactivity for burnup is controlled by soluble boron and/or burnable absorbers, it is not included in control rod requirements.
4.3.3.4.7 Xenon and Samarium Poisoning Changes in xenon and samarium concentrations in the core occur at a sufficiently slow rate, even following rapid power level changes, so that the resulting reactivity change is
controlled by changing the soluble boron concentration.
4.3.3.4.8 pH Effects Changes in reactivity due to a change in coolant pH, if any, are sufficiently small in
magnitude and occur slowly enough to be controlled by the boron system. Further
details are available in Reference 4.
4.3.3.4.9 Experimental Confirmation The most appropriate assessment of the experimental confirmation of the analytical methods calls for comparison of key physics parameter predictions against directly measured plant data. A total of seven reactor cores covering a diversified range of advanced fuel product features, modern fuel management schemes, and different reactor loop types formulate the basis for the qualification assessment. Three-dimensional Advanced Nodal Code (ANC) models employing PHOENIX-P based cross-sections were developed to predict all relevant physics parameters. To encompass the DCPP UNITS 1 &
2 FSAR UPDATE 4.3-22 Revision 23 December 2016 entire range of available measured quantities, hot zero power physics predictions are compared against measured data in addition to full power core analyses. Refer to Reference 27 for additional details of the experimental confirmation.
These and other measurements demonstrate the ability of the methods described in Section 4.3.3.10 to accurately predict the total shutdown reactivity of the core.
4.3.3.5 Control Core reactivity is controlled by means of a chemical neutron absorber (chemical shim)
dissolved in the coolant, RCCAs, and burnable poison rods as described below.
4.3.3.5.1 Chemical Shim Boron in solution as boric acid is used to control relatively slow reactivity changes
associated with:
(1) The moderator temperature defect in going from cold shutdown at ambient temperature to the hot operating temperature at zero power (2) Transient xenon and samarium poisoning, such as that following power changes or changes in RCCA position (3) The excess reactivity required to compensate for the effects of fissile inventory depletion and buildup of long-life fission products (4) The burnable absorber depletion
The boron concentrations for various core conditions are presented in Table 4.3-1.
4.3.3.5.2 Rod Cluster Control Assemblies As shown in Table 4.1-1, 53 RCCAs are used in these reactors. The RCCAs are used
for shutdown and control purposes to offset fast reactivity changes associated with:
(1) The required SDM in the hot zero power, stuck rods condition (2) The increase in power above hot zero power (power defect including Doppler and moderator reactivity changes)
(3) Unprogrammed fluctuations in boron concentration, coolant temperature, or xenon concentration (with rods not exceeding the allowable rod
insertion limits)
(4) Reactivity ramp rates resulting from load changes
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-23 Revision 23 December 2016 Control bank reactivity insertion at full power is limited to maintain shutdown capability.
As the power level is reduced, control rod reactivity requirements are reduced and more
rod insertion is allowed. The control bank position is monitored and the operator is
notified by an alarm if the limit is approached. The determination of the insertion limit
uses conservative xenon distributions and axi al power shapes. In addition, the RCCA withdrawal pattern obtained from these analyses is used in determining power
distribution factors, and in determining the maximum reactivity worth during an ejection
accident of an inserted RCCA. The Technical Specifications discuss rod insertion limits.
Power distribution, rod ejection, and rod misalignment analyses are based on the
arrangement of the shutdown and control RCCA groups shown in Figures 4.3-37 and
4.3-38, for Unit 1 and Unit 2, respectively. All shutdown RCCAs are withdrawn before control banks withdrawal is initiated. In going from zero to 100 percent power, control
banks A, B, C, and D are withdrawn sequentially. Rod position limits and the basis for
rod insertion limits are provided in the Core Operating Limits Reports.
4.3.3.5.3 Burnable Absorber Rods Burnable absorber rods (either discrete or integral type) provide partial control of excess
reactivity during the fuel cycle. These rods prevent the MTC from being positive at
normal operating conditions. They perform this function by reducing the requirement for
soluble boron in the moderator at the beginning of the fuel cycle, as described above.
The burnable absorber patterns, used together with a typical number of rods per assembly, are shown in Figure 4.3-6. The arrangements within an assembly for discrete and integral absorber types are displayed in Figures 4.3-4 and 4.3-5
respectively. The critical concentration of soluble boron resulting from the slow burnup of boron in the rods is such that the MTC remains negative at all times for full power operating conditions.
4.3.3.5.4 Peak Xenon Startup Peak xenon buildup is compensated by the boron control system. Startup from the peak xenon condition is accomplished with a combination of rod motion and boron
dilution. Boron dilution may be made at any time, including the shutdown period, provided the SDM is maintained.
4.3.3.5.5 Load Follow Con trol and Xenon Control The DCPP units are usually base loaded; however, it is expected that during certain
times of certain years some load following may be required.
Should load following become a desired mode of operation, then, during load follow
maneuvers, power changes would be accomplished using control rod motion, dilution or
boration by the boron systems as required, and reductions in coolant average temperature. Control rod motion limitations are discussed in Section 4.3.3.5.2 and the DCPP UNITS 1 &
2 FSAR UPDATE 4.3-24 Revision 23 December 2016 Technical Specifications. Reactivity changes due to the changing xenon concentration can be controlled by rod motion and/or soluble boron concentration changes.
4.3.3.5.6 Burnup The excess reactivity available for burnup is controlled with soluble boron and/or
burnable absorbers. The boron concentration must be limited during operating conditions to ensure the MTC is negative at full power. Sufficient burnable absorbers are installed at the beginning of a cycle to give the desired cycle lifetime without exceeding the boron concentration limit. The practical minimum boron concentration is
10 ppm.
4.3.3.6 Control Rod Patterns and Reactivity Worths The RCCAs are designated by function as the control groups and the shutdown groups.
The terms "group" and "bank" are used synonymously throughout this chapter to
describe a particular grouping of control assemblies. The RCCA patterns are displayed
in Figures 4.3-37 and 4.3-38 for Unit 1 and Unit 2, respectively. These patterns are not expected to change during the life of the units. The control banks are labeled A, B, C, and D, and the shutdown banks are labeled SA, SB, SC and SD.
The two criteria used to select the control groups are: (a) the total reactivity worth must be adequate to meet the requirements specified in Tables 4.3-2 and 4.3-3, and (b) because these rods may be partially inserted at power operation, the total power
peaking factor should be low enough to ensure that power capability requirements are
met. Analyses indicate that the first requirement can be met by one or more banks whose total worth equals at least the required amount. Since the shape of the axial power distribution would be more peaked foll owing movement of a single group of rods worth 3 to 4 percent , four banks, each worth approximately 1 percent , were selected.
The position of control banks for criticality under any reactor condition is determined by
the boron concentration in the coolant. On an approach to criticality, boron is adjusted
to ensure criticality will be achieved with control rods above the insertion limit set by
shutdown and other considerations (refer to t he Technical Specifications). Early in the cycle there may also be a withdrawal limit at low power to maintain an MTC more
negative than the Technical Specification limit. Usual practice is to adjust boron to
ensure that the rod position lies within the so-called maneuvering band so that an
escalation from zero power to full power does not require further adjustment of boron concentration.
Ejected rod worths are given in Section 15.4.6 for several different conditions.
Experimental confirmation of ejected rod worths can be found by reference to startup test reports such as Reference 5.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-25 Revision 23 December 2016 Allowable deviations due to misaligned control rods are discussed in the Technical Specifications.
A representative calculation for two banks of control rods withdrawn simultaneously (rod withdrawal accident) at EOL is shown in Figure 4.3-39. Calculation of control rod reactivity worth versus time following reactor trip involves both control rod velocity and
differential reactivity worth. Rod position versus time of travel after rod release is shown
in Figure 4.3-40. The reactivity worth versus rod position is calculated by a series of
steady state calculations at various control rod positions assuming all rods out of the
core as the initial position to minimize the initial reactivity insertion rate. To be
conservative, the rod of highest worth is assumed stuck out of the core and the flux
distribution (and thus reactivity importance) is assumed to be skewed to the bottom of
the core. The result of these calculations is shown in Figure 4.3-41.
The shutdown groups provide additional negative reactivity to ensure an adequate
SDM. SDM is defined as the instantaneous amount of reactivity by which the reactor is subcritical, or would be subcritical from its present condition, assuming:
(1) all RCCAs are fully inserted except for the single RCCA of highest reactivity worth, which is assumed to be fully withdrawn (with any RCCA not capable of being fully inserted, the reactivity worth of the RCCA must be accounted for in the determination of SDM) and (2) when in MODE 1 or 2, the fuel and moderator temperatures are changed to the hot zero power temperatures.
The loss of control rod worth due to material irradiation is negligible, since only bank D rods may be in the core under full power operating conditions.
Tables 4.3-2 and 4.3-3 show that the avail able reactivity in withdrawn RCCAs provides the design bases minimum SDM allowing for the highest worth cluster to be at its fully withdrawn position in DCPP Unit 1 and Unit 2, respectively. An allowance for uncertainty in the calculated worth of N-1 rods is made before determination of the
SDM.
4.3.3.7 Criticality of Fuel Assemblies
Criticality of fuel assemblies outside the reactor is precluded by adequate design of fuel
transfer and fuel storage facilities, and by administrative control procedures (refer to Section 9.1.1).
Verification that appropriate shutdown criteria, including uncertainties, are met during refueling is achieved using standard Westinghouse reactor design methods. Core subcriticality during refueling is continuously monitored as described in the Technical
Specifications.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-26 Revision 23 December 2016 4.3.3.8 Stability 4.3.3.8.1 Introduction The stability of PWR cores against xenon-in duced spatial oscillations, and the control of such transients, is discussed extensively in References 2, 6, 7, and 8.
Due to the negative power coefficient of reactivity, PWR cores are inherently stable to
oscillations in total power. In a large reactor core, however, xenon-induced oscillations can take place with no corresponding change in total core power. The oscillation may
be caused by a power shift in the core that occurs rapidly in comparison with the
xenon-iodine time constants. Such a power shift occurs in the axial direction when a plant load change is made by control rod motion, and results in a change in the
moderator density and fuel temperature distributions. Such a power shift in the
diametral plane of the core could result from abnormal control action.
4.3.3.8.2 Stability Index Power distributions, either in the axial directio n or in the X-Y plane, can undergo oscillations due to perturbations introduced in the equilibrium distributions without changing total core power. The xenon-induced oscillations are essentially limited to the first flux overtones in the current PWRs, and the stability of the core against xenon-induced oscillations can be determined in terms of the eigenvalues of the first flux harmonics. Writing the eigenvalue of the first flux harmonic, either in the axial
direction or in the X-Y plane, as:
();1i,icb 2=+= (4.3-6) where b is defined as the stability index and T = 2/c as the oscillation period of the first harmonic. The time-dependence of the first harmonic in the power distribution can now be represented as:
()ctcosaeeAtbtt== (4.3-7) where A and a are constants. The stability i ndex can also be obtained approximately by:
+n A1n A ln T 1 = b (4.3-8) where A n , A n+1 are the successive peak amplitudes of the oscillation, and T is the time period between the successive peaks.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-27 Revision 23 December 2016 4.3.3.8.3 Prediction of the Core Stability The stability of the DCPP cores in relation to xenon-induced spatial oscillations is expected to be equal to that of earlier desig ns because: (a) the overall core size is unchanged and spatial power distributions are similar, (b) the MTC is expected to be
similar, and (c) the Doppler coefficient of reactivity is expected to be similar at full
power.
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
4.3.3.8.4 Stability Measurements (1) Axial Measurements Two axial xenon transient tests conducted in a PWR with a core height of 12 feet and 121 fuel assemblies, at approximately 10 and 50 percent of
cycle life, are reported in Reference 9.
The AO of power was obtained as a function of time for both tests as shown in Figure 4.3-42. The total core power was maintained constant during these spatial xenon tests, and the stability index and the oscillation period were obtained from a least-square fit of the AO data to Equation
4.3-8. The conclusions of the tests are as follows:
(a) The core was stable against induced axial xenon transients both at the core average burnups of 1550 MWD/MTU and 7700 MWD/MTU.
(b) The reactor core becomes less stable as fuel burnup progresses, and the axial stability index was essentially zero at 12,000
MWD/MTU. (2) Measurements in the X-Y Plane Two X-Y xenon oscillation tests were performed at a PWR plant with a
core height of 12 feet and 157 fuel asse mblies. This plant had the highest power output of any Westinghouse PWR ope rating in 1972. The first test was conducted at a core average burnup of 1540 MWD/MTU and the
second at a core average burnup of 12900 MWD/MTU. Both of the X-Y
xenon tests show that the core was stable in the X-Y plane at both
burnups. The second test shows that the core became more stable as the
fuel burnup increased and all Westinghouse PWRs with 121 and 157
assemblies are expected to be stable throughout their burnup cycles.
In each of the two X-Y tests, a perturbation was introduced to the
equilibrium power distribution through an impulse motion of one RCCA located along the diagonal axis. Following the perturbation, the DCPP UNITS 1 &
2 FSAR UPDATE 4.3-28 Revision 23 December 2016 uncontrolled oscillation was monitored using the movable detector and thermocouple system and the excore power range detectors. The quadrant tilt difference (QTD) is the quantity that properly represents the diametral oscillation in the X-Y plane of the reactor core in that the
difference of the quadrant average powers over two symmetrically
opposite quadrants essentially eliminates the contribution to the oscillation
from the azimuthal mode. The Q TD data were least-square fitted to the form of Equation 4.3-8. A stability index of -0.076 hr-1 with a period of 29.6 hours6.944444e-5 days <br />0.00167 hours <br />9.920635e-6 weeks <br />2.283e-6 months <br /> was obtained from the thermocouple data shown in
Figure 4.3-43.
In the second X-Y xenon test, the PWR core with 157 fuel assemblies became more stable due to increased fuel depletion.
4.3.3.8.5 Comparison of Calculations with Measurements
Axial xenon transient tests were analyzed in an axial slab geometry using a flux synthesis technique. The PANDA code (Reference 11) was used for direct simulation
of the AO data. X-Y xenon transient tests analyses were performed with the modified TURTLE code (Reference 12). Both the PANDA and TURTLE codes solve the two-group time-dependent neutron diffusion equation with time-dependent xenon and iodine concentrations. The fuel temperature and moderator density feedback is limited to a
steady state model. All the X-Y calcul ations were performed in an average enthalpy plane.
The basic nuclear cross-sections used in this study were generated from a unit cell depletion program that evolved from the codes LEOPARD (Reference 13) and CINDER (Reference 14). The detailed experimental data during the tests, including the reactor power level, enthalpy rise, and the impulse m otion of the control rod assembly, as well as the plant follow burnup data, were closely simulated in the study.
The results of the stability calculation for the axial tests are compared with the experimental data in Table 4.3-4. The calculations show conservative results for both of
the axial tests with a margin of approximately 0.01 hr
-1 in the stability index.
An analytical simulation of the first X-Y xenon oscillation test shows a calculated stability index of -0.081 hr
-1 , in good agreement with the measured value of -0.076 hr
-1. As indicated earlier, the second X-Y xenon test showed that the core had become more
stable compared to the first test. The increase in the core stability in the X-Y plane due
to increased fuel burnup is due mainly to the increased magnitude of the negative MTC.
Previous studies of the physics of xenon oscill ations, including three-dimensional analysis, are reported in References 6, 7, 8, 9, and Section 1 of Reference 10.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-29 Revision 23 December 2016 4.3.3.8.6 Stability Control and Protection The excore detector system provides indicati ons of xenon-induced spatial oscillations.
The readings from the excore detectors are available to the operator and also form part
of the protection system.
(1) Axial Power Distribution To maintain proper axial power distributions, the operator is instructed to
maintain an AO within a prescribed operating band, based on the excore detector readings. Should the AO move far enough outside this band, the protection limit will be reached and the power will be automatically cut
back. (2) Radial Power Distribution The DCPP cores are calculated to be stable with respect to xenon-
induced oscillations in the X-Y plane during the plant's lifetime.
The X-Y stability of large PWRs has been further verified as part of the
startup physics test program at a PWR core with 193 fuel assemblies.
The measured X-Y stability of the PWR core with 157 assemblies, and the
good agreement between the calculated and measured stability index for
this core, as discussed in Sections 4.3.3.8.4 and 4.3.3.8.5, make it very unlikely that a sustained X-Y oscillation can occur in a core with 193
assemblies. In the unlikely event that X-Y oscillations occur, backup actions are possible and would be implemented, if necessary, to increase the natural stability of the core until tests demonstrate a suitable stability, by making the MTC more negative.
A more detailed discussion of the power distribution control in PWR cores
is presented in Reference 2.
4.3.3.9 Vessel Irradiation Pressure vessel irradiation and the corresponding material surveillance program are
discussed in Sections 5.2.2.4 and 5.4.1. A brief review of the methodology used to determine neutron and gamma flux attenuation between the core and pressure vessel
follows.
The primary shielding material used to attenuate high energy neutron and gamma flux
originating in the core consists primarily of th e core baffle, core barrel, the thermal shield for Unit 1 and the neutron pads for Unit 2, and associated water annuli, all of
which are within the region between the core and the pressure vessel.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-30 Revision 23 December 2016 In general, few group neutron diffusion theory and nodal analysis codes are used to determine flux and fission power density distributions within the active core, and the accuracy of these analyses is verified by incore measurements on operating reactors.
Refer to Section 5.2.2.4 for methods used outside the active core.
The neutron flux distribution and spectrum in the various structural components varies
significantly from the core to the pressure vessel. Representative values of the neutron
flux distribution and spectrum are presented in Table 4.3-5. The values listed are based
on equilibrium cycle reactor core parameters and power distributions and are thus suitable for long-term neutron fluence projections and for correlation with radiation
damage estimates.
4.3.3.10 Analytical Methods Calculations required in nuclear design consi st of the following three distinct types, which are performed in sequence:
(1) Determination of effective fuel temperatures (2) Generation of macroscopic few-group parameters (3) Space-dependent, few-group diffusion calculations 4.3.3.10.1 Fuel Temperature (Doppler) Calculations Temperatures vary radially within the fuel rod, depending on heat generation rate in the pellet, the conductivity of the materials in the pellet, gap and cladding, and coolant temperature.
The FIGHTH code (Reference 34) performs a simplified calculation of effective temperatures in low enrichment, sintered UO 2 fuel rods for use in nuclear design. The model includes radial variations of heat generation rate, thermal conductivity, and thermal expansion in the fuel pellet, elastic deflection of the cladding, and a pellet-clad gap conductance which depends on the kind of initial fill gas, the hot open gap dimension, and the fraction of the pellet circumference over which the gap is effectively closed due to pellet cracking. The steady-state radial temperature distribution in the fuel rod is calculated at a specified burnup, given the local value of the linear heat generation rate in the pellet and the moderator temperature and flow rate. The effective resonance temperatures of U-238 and Pu-240 are obtained by appropriate radial weighting of the temperature distribution. An effective flat pellet temperature for expansion which reproduces the hot pellet outer radius is also determined.
The observed burnup dependence of the Doppler defects and Doppler coefficients in operating plants was used to construct an empirical model of progressive pellet cracking which, primarily through the increased gap conductance due to gap closure, produces effective temperatures which lead to adequate predictions of the measurements. The DCPP UNITS 1 &
2 FSAR UPDATE 4.3-31 Revision 23 December 2016 effects of fission gas release, clad creep, and pellet swelling are not treated explicitly in this simplified model, described in Section 4.2.1.2.2.5.
Fuel temperatures for use in some past nuclear design Doppler calculations were obtained from a simplified version of the Westinghouse fuel rod design model described in Section 4.2.1.2.2, which considers the effect of radial variation of pellet conductivity, expansion-coefficient and heat generation rate, elastic deflection of the cladding, and a
gap conductance which depends on the initial fil l gas, the hot open gap dimension, and the fraction of the pellet over which the gap is closed. The fraction of the gap assumed
closed represents an empirical adjustment to produce good agreement with observed
reactivity data at BOL. Further gap closure occurs with burnup and accounts for the
decrease in Doppler defect with burnup which has been observed in operating plants.
For detailed calculations of the Doppler coefficient, such as for use in xenon stability
calculations, a more sophisticated temperat ure model is used which accounts for the effects of fuel swelling, fission gas release, and plastic cladding deformation.
Radial power distributions in the pellet as a function of burnup were obtained from LASER (Reference 15) calculations.
The effective U-238 temperature for resonance absorption was obtained from the radial temperature distribution by applying a radiall y dependent weighting function. The weighting function was determined from REPAD (Reference 16) Monte Carlo
calculations of resonance escape probabil ities in several steady state and transient temperature distributions. In each case, a flat pellet temperature was determined which
produced the same resonance escape probability as the actual distribution. The
weighting function was empirically determined from these results.
The effective Pu-240 temperature for resonance absorption was determined by a convolution of the radial distribution of Pu-240 number densities from LASER burnup calculations and the radial weighting function. The resulting temperature is burnup
dependent, but the difference between U-238 and Pu-240 temperatures, in terms of
reactivity effects, is small.
The effective pellet temperature for pellet dimensional change is that value which
produces the same outer pellet radius in a virgin pellet as that obtained from the
temperature model. The effective cladding temperature for dimensional change is its
average value.
The temperature calculational model has been valid ated by plant Doppler defect data as shown in Table 4.3-6 and Doppler coefficient data as shown in Figure 4.3-44. Stability index measurements also provide a sensitive measure of the Doppler coefficient near
full power (refer to Section 4.3.3.8). It can be seen that Doppler defect data are typically within 0.2 percent of prediction.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-32 Revision 23 December 2016 4.3.3.10.2 Macroscopic Group Constants There are two lattice codes used for the generation of macroscopic group constants for
use in the spatial few group diffusion codes. They are a version of the LEOPARD and
CINDER codes and PHOENIX-P. A detailed description of each follows. Macroscopic
few-group constants and analogous microscopic cross-sections (needed for feedback and microscopic depletion calculations) can be generated for fuel cells by a
Westinghouse version of the LEOPARD and CINDER codes, which are linked internally and provide burnup-dependent cross-sections. Normally, a simplified approximation of the main fuel chains is used; however, where needed, a complete solution for all the
significant isotopes in the fuel chains from Th-232 to Cm-244 is available (Reference 17). Cross-section library tapes contain microscopic cross-sections from the ENDF/B (Reference 18) library, with a few exceptions, where other data provide better agreement with critical experiments, isotopic measurements, and plant critical
boron values.
The effect on the unit fuel cell of nonlattice components in the fuel assembly is obtained
by supplying an appropriate volume fraction of these materials in an extra region which
is homogenized with the unit cell in the fast (MUFT) and thermal (SOFOCATE) flux
calculations. In the thermal calcu lation, the fuel rod, cladding, and moderator are homogenized by energy-dependent disadvantage factors derived from an analytical fit
to integral transport theory results.
Group constants for burnable absorber cells, guide thimbles, instrument thimbles, and
interassembly gaps are generated in a manner analogous to the fuel cell calculation.
Reflector group constants are taken from infinite medium LEOPARD calculations.
Baffle group constants are calculated from an average of core and radial reflector microscopic group constants for stainless steel.
Group constants for control rods are calculated in a linked version of the HAMMER (Reference 19) and AIM (Reference 20) codes to provide an improved treatment of self-
shielding in the broad resonance structure of the appropriate isotopes at epithermal
energies than is available using LEOPAR D. The Doppler broadened cross-sections of the control rod material are represented as smooth cross-sections in the 54-group LEOPARD fast group structure and in 30 thermal groups. The four-group constants in
the rod cell and appropriate extra region are generated in the coupled space-energy
transport HAMMER calculation. A corresponding AIM calculation of the homogenized
rod cell with extra region is used to adjust the absorption cross-sections of the rod cell to match the reaction rates in HAMMER. These transport-equivalent group constants
are reduced to two-group constants for use in space-dependent diffusion calculations.
In discrete X-Y calculations only one mesh interval per cell is used, and the rod group
constants are further adjusted for use in this standard mesh by reaction rate matching the standard mesh unit assembly to a fine-mesh unit assembly calculation.
Validation of the cross-section method is based on analysis of critical experiments (refer to Table 4.3-7), isotopic data (refer to Table 4.3-8), plant critical boron (C B) values at hot DCPP UNITS 1 &
2 FSAR UPDATE 4.3-33 Revision 23 December 2016 zero power (HZP), BOL (refer to Table 4.3-9), and at HFP as a function of burnup (refer to Figures 4.3-45 through 4.3-47). Control rod worth measurements are shown in Table 4.3-10. Confirmatory critical experiments on burnable absorbers are described in Reference 21.
The PHOENIX-P computer code is a two-dimensional, multi-group, transport based
lattice code capable of providing all necessary data for PWR analysis. Being a dimensional lattice code, PHOENIX-P does not rely on pre-determined spatial/spectral
interaction assumptions for a heterogeneous fuel lattice, hence, will provide a more
accurate multi-group flux solution than versions of LEOPARD/CINDER. The
PHOENIX-P computer code is approved by the USNRC as the lattice code for
generating macroscopic and microscopic few group cross-sections for PWR analysis (Reference 27).
The solution for the detailed spatial flux an d energy distribution is divided into two major steps in PHOENIX-P (Reference 27). In the first step, a two-dimensional fine energy group nodal solution is obtained which coup les individual subcell regions (pellet, cladding and moderator) as well as surrounding pins. PHOENIX-P uses a method
based on the Carlvik's collision probabi lity approach and heterogeneous response fluxes which preserves the heterogeneity of the pin cells and their surroundings. The nodal solution provides accurate and detailed local flux distribution, which is then used to spatially homogenize the pin cells to fewer groups.
The second step in the solution process solves for the angular flux distribution using a
standard S4 discrete ordinates calculation. This step is based on the group-collapsed
and homogenized cross-sections obtained from the first step of the solution. The S4 fluxes are then used to normalize the detailed spatial and energy nodal fluxes. The
normalized nodal fluxes are used to compute reaction rates, power distribution and to deplete the fuel and burnable absorbers. A standard B1 calculation is employed to
evaluate the fundamental mode critical spectrum and to provide an improved fast
diffusion coefficient for the core spatial codes.
The PHOENIX-P code employs an energy group library, which has been derived mainly from ENDF/B (Reference 18) files. The PHOENIX-P cross-sections library was designed to properly capture integral properties of the multi-group data during group
collapse, and enabling proper modeling of important resonance parameters. The library contains all neutronic data necessary for modeling fuel, fission products, cladding and
structural data, coolant, and control/burnable absorber materials present in Light Water
Reactor cores.
Group constants for burnable absorber cells, guide thimbles, instrument thimbles, control rod cells and other non-fuel cells can be obtained directly from PHOENIX-P
without any adjustments such as those required in the cell or 1D lattice codes.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-34 Revision 23 December 2016 4.3.3.10.3 Spatial Few-Group Diffusion Calculations Spatial few-group diffusion calculations have primarily consisted of two group X-Y calculations using an updated version of the TURTLE code, and two-group axial
calculations using an updated version of the PANDA code. However, with the advent of VANTAGE+ and hence axial features such as axial blankets and part length burnable absorbers, there is a greater reliance on three-dimensional nodal codes such as 3D PALADON (Reference 25) and APOLLO code (Reference 35) which performs one-dimensional, two group calculations using typical finite difference techniques, and 3D ANC (References 26 and 27) which provides both the radial and axial power distributions.
Nodal three-dimensional calculations are carried out to determine the critical boron concentrations and power distributions.
The moderator coefficient is evaluated by varying the inlet temperature in the same calculations used for power distribution and
reactivity predictions.
Axial calculations are used to determine differential control rod worth curves (reactivity versus rod insertion) and axial power shapes during steady state and transient xenon conditions. Group constants are obtained from three-dimensional nodal calculations homogenized by flux volume weighting.
Validation of the spatial codes for calculatin g power distributions involves the use of incore and excore detectors, and is discussed in Section 4.3.3.2.7.
The agreement in the PHOENIX-P methodology and PHOENIX-P/ANC core model qualification demonstrates the high accuracy of the PHOENIX-P/ANC advanced design system for multidimensional nucl ear analysis of PWR cores. This qualification data base demonstrates the performance of this system for a wide range of applications performed in the design, safety, licensing and operational follow of PWR cores. Refer to Reference 27 for additional details on experimental verification.
The accuracy of APOLLO predictions for reactivity and axial power shapes is comparable to that for 3D ANC-based calculations (References 26 and 27).
4.3.4 SAFETY
EVALUATION 4.3.4.1 General Design Criterion 10, 1971 - Reactor Design The reactor core and associated coolant, control, and protection systems are designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation, including the effects of anticipated operational occurrences.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-35 Revision 23 December 2016 4.3.4.1.1 Fuel Burnup Fuel burnup is a measure of fuel depletion that represents the integrated energy output
of the fuel (MWD/MTU) and is a conveni ent means for quantifying fuel exposure.
The core design lifetime or design discharge burnup is achieved by installing sufficient initial excess reactivity in each fuel region, and by following a fuel replacement program (such as that described in Section 4.3.3) that meets all safety-related criteria in each cycle of operation.
Initial excess reactivity in the fuel, although not a design basis, must be sufficient to
maintain core criticality at full power operating conditions throughout cycle life with
equilibrium xenon, samarium, and other fission products present. The end of design
cycle life is defined to occur when the chemical shim concentration is essentially zero, with control rods present to the degree neces sary for operational requirements (e.g., the controlling bank at the "bite" position). In terms of chemical shim boron concentration, this represents approximately 10 ppm with no control rod insertion.
4.3.4.1.2 Control of Power Distribution
Calculation of the extreme power shapes that affect fuel design limits is performed with proven methods as described in Section 4.3.3.10 and verified frequently with results from measurements in operating reactors. The conditions under which limiting power shapes are assumed to occur are chosen conservatively with regard to any permissible
operating state.
Even though there is good agreement between peak power calculations and measurements, a nuclear uncertainty margin is applied to calculated peak local power.
Such a margin is provided both for the analysis of normal operating states and for
anticipated transients.
4.3.4.2 General Design Criterion 11, 1971 - Reactor Inherent Protection The reactor core and associated coolant systems is designed so that in the power operating range the net effect of the prompt inherent nuclear feedback characteristics tend to compensate for a rapid increase in reactivity.
When compensation for a rapid increase in reactivity is considered, there are two major effects. These are the resonance absorption effects (Doppler) associated with changing fuel temperature, and the spectrum effect resulting from changing moderator density.
These basic physics characteristics are often identified by reactivity coefficients. The
use of slightly enriched uranium ensures that the Doppler coefficient of reactivity, which
provides the most rapid reactivity compensation, is negative. The core is also designed
to have an overall negative MTC of reactivity at full power so that average coolant
temperature or void content provides another, slower, compensatory effect. A small
positive MTC is allowed at low power. The negative MTC at full power can be achieved DCPP UNITS 1 &
2 FSAR UPDATE 4.3-36 Revision 23 December 2016 through use of fixed burnable absorbers and/or boron coated fuel pellets and/or control rods by limiting the reactivity held down by soluble boron.
Burnable absorber content (quantity and distribution) is not stated as a design basis
other than as it relates to achieving a nonpositive MTC at power operating conditions, as discussed above.
4.3.4.3 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations The reactor core and associated coolant, control, and protection systems are designed to assure that power oscillations which can result in conditions exceeding SAFDLs are not possible or can be reliably and readily detected and suppressed.
Oscillations in total core power output, from whatever cause, are readily detected by loop temperature sensors and by nuclear instrumentation. If power increased unacceptably, a reactor trip would occur, thus preserving margins to fuel design limits.
The stability of the turbine/steam generator/core syste ms and the reactor control system ensure that core power oscillations do not normally occur. Protection circuits'
redundancy ensures an extremely low probability of exceeding design power levels.
The core is designed so that diametral and azimuthal oscillations due to spatial xenon effects are self-damping, and no operator action or control action is required to
suppress them. Stability against diametral oscillations is so great that this excitation is
highly improbable. Convergent azimuthal oscillations can be excited by prohibited
motion of individual RCCAs. Such oscill ations are readily observable and alarmed, using the excore long ion chambers.
Indications are also continuously available from incore thermocouples and loop temperature measurements. The MIDS can be activated to provide more detailed information. In all presently proposed cores, these
horizontal plane oscillations are self-damping by virtue of reactivity feedback effects
designed into the core.
Axial xenon spatial power oscillations can be excited by power level changes or by control rod motion/misalignments. The oscillations are inherently convergent at the
beginning of core life, but become divergent as the core ages. The time in core life
when oscillations may become divergent depends on core characteristics. Xenon
oscillations studies performed for plants similar to DCPP concluded that oscillations can
diverge as early as 50 EFPD. The magnitude of oscillations increases with increasing
core burnup, although the period is unaffected. The type of oscillation (convergence or
divergence) does not depend on the amplitude of the initial oscillation but is a function of initial conditions at the start of the transient.
The excore detectors provide monitoring of axial power distribution. The operator actions (control rod movement or power level changes) are expected to suppress and
control axial xenon transients.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-37 Revision 23 December 2016 The limits on measured axial flux difference assure that the fuel design limits (F q) are not exceeded during either normal operation or a xenon transient. The measured axial flux difference is also used as an input to the OTT trip function so that the DNB design bases are not exceeded.
4.3.4.4 General Design Criterion 25, 1971 - Protection System Requirements for Reactivity Control Malfunctions The protection system is designed to assure t hat SAFDLs are not exceeded for any single malfunction of the reactivity control systems, such as accidental withdrawal (not ejection or dropout) of control rods.
Reactivity addition associated with an accidental withdrawal of a control bank (or banks) is limited by the maximum rod speed (or tr avel rate) and by the worth of the bank(s).
For this reactor the maximum control rod speed is 45 inches per minute and the maximum rate of reactivity change considering two control banks moving is less than
75 pcm/sec. The reactivity rate used in the boron dilution analysis at power is discussed in Section 15.2.4.3.4.
4.3.4.5 General Design Criterion 26, 1971 - Reactivity Control System Redundancy and Capability Two independent reactivity control systems are provided: control rods and soluble boron in the coolant.
The control rod system can compensate for the reactivity effects of the fuel and water
temperature changes accompanying power level changes over the range from full load
to no load. In addition, the control rod system provides the minimum SDM under Condition I events and is capable of making t he core subcritical rapidly enough to
prevent exceeding acceptable fuel damage limits, assuming that the highest worth
control rod is stuck out upon trip.
The boron system can compensate for all xe non burnout reactivity changes and will maintain the reactor in cold shutdown. Thus, backup and emergency shutdown
provisions are provided by a mechanical and a chemical shim control system.
When fuel assemblies are in the pressure vessel and the vessel head is not in place, k eff will be maintained at or below 0.95 with control rods and soluble boron. Further, the fuel will be maintained sufficiently subcritical that removal of all RCCAs will not result in criticality.
4.3.4.6 General Design Criterion 28, 1971 - Reactivity Limits The reactivity control system is designed with appropriate limits on the potential amount and rate of reactivity increase to assure that the effects of postulated reactivity accidents can neither (1) result in damage to the reactor coolant pressure boundary DCPP UNITS 1 &
2 FSAR UPDATE 4.3-38 Revision 23 December 2016 greater than limited local yielding nor (2) sufficiently disturb the core, its support structures or other reactor pressure vessel internals to impair significantly the capability to cool the core. These postulated reactivity accidents shall include consideration of rod ejection (unless prevented by positive means), rod dropout, steam line rupture, changes in reactor coolant temperature and pressure, and cold water addition.
The maximum control rod reactivity worth and the maximum rates of reactivity insertion using control rods are limited to preclude either rupture of the coolant pressure boundary or disruption of the core internals to a degree that would impair core cooling
capacity in the event of a rod withdrawal or ejection accident (refer to Chapter 15).
Following any Condition IV event (such as rod ejection and steam line break), the
reactor can be brought to the shutdown condition and the core will maintain acceptable
heat transfer geometry.
4.
3.5 REFERENCES
- 1. F. L. Langford and R. J. Nath, Jr., Evaluation of Nuclear Hot Channel Factor Uncertainties, WCAP-7308-L, April 1969 (Westinghouse Proprietary) and WCAP-7810, December 1971.
- 2. J. S. Moore, Power Distribution Control of Westinghouse Pressurized Water Reactors, WCAP-7208, September 1968 (Westinghouse Proprietary) and WCAP-7811, December 1971.
- 3. A. F. McFarlane, Power Peaking Factors, WCAP-7912-P-A, January 1975 (Westinghouse Proprietary) and WCAP-7912-A, January 1975.
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- 5. J. E. Outzs, Plant Startup Test Report, H. B. Robinson Unit No. 2, WCAP-7844, January 1972.
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- 7. F. B. Skogen and A. F. McFarlane, Control Procedures for Xenon-Induced X-Y Instabilities in Large PWRs, WCAP-3680-21, (EURAEC-2111), February 1969.
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- 9. J. C. Lee, et al, Axial Xenon Transient Tests at the Rochester Gas and Electric Reactor, WCAP-7964, June 1971.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-39 Revision 23 December 2016
- 10. C. J. Kubit, Safety Related Research and Development for Westinghouse Pressurized Water Reactors, Program Summaries, Fall 1972, WCAP-8004, January 1973..
- 11. S. Altomare, et al., The PANDA Code, WCAP-7048-P-A, February 1975 (Westinghouse Proprietary) and WCAP-7757-A, February 1975.
- 12. S. Altomare and R. F. Barry, The TURTLE 24.0 Diffusion Depletion Code, WCAP-7213-P-A, February 1975 (Westinghouse Proprietary) and WCAP-7758-A, February 1975.
- 13. R. F. Barry, LEOPARD - A Spectr um Dependent Non-Spatial Depletion Code for the IBM-7094, WCAP-3269-26, September 1963.
- 14. T. R. England, CINDER - A One-Point Depletion and Fission Product Program.
WAPD-TM-334, August 1962.
- 15. C. G. Poncelet, LASER - A Depletion Program for Lattice Calculations Based on MUFT and THERMOS, WCAP-6073, April 1966.
- 16. J. E. Olhoeft, The Doppler Effect f or a Non-Uniform Temperature Distribution in Reactor Fuel Elements, WCAP-2048, July 1962.
- 17. R. J. Nodvik, et al, Supplementary Report on Evaluation of Mass Spectrometric and Radiochemical Analyses of Yankee Cor e I Spent Fuel, Including Isotopes of Elements Thorium Through Curium, WCAP-6086, August 1969.
- 18. M. K. Drake, (Ed), Data Formats and Procedure for the ENDF Neutron Cross Section Library, BNL-50274, ENDF-102, Vol. I, 1970.
- 19. J. E. Suich and H. C. Honeck, Th e HAMMER System, Heterogeneous Analysis by Multigroup Methods of Exponentials and Reactors, DP-1064, January 1967.
- 20. H. P. Flatt and D. C. Baller, AIM
-5, A Multigroup, One Dimensional Diffusion Equation Code, NAA-SR-4694, March 1960.
- 21. J. S. Moore, Nuclear Design of Westinghouse Pressurized Water Reactors with Burnable Poison Rods, WCAP-7806, December 1971.
- 22. J. M. Hellman, (Ed), Fuel Densification Experimental Results and Model for Reactor Application, WCAP-8218-P-A, March 1975 (Westinghouse Proprietary) and WCAP-8219-A, March 1975.
- 23. T. Morita, et al., Power Distribution Control and Load Following Procedures, WCAP-8385, September 1974 (Westinghouse Proprietary) and WCAP-8403, September 1974.
DCPP UNITS 1 &
2 FSAR UPDATE 4.3-40 Revision 23 December 2016
- 24. Deleted.
- 25. T. M. Camden. et al., PALADON - Westinghouse Nodal Computer Code, WCAP-9485-P-A. December 1979 and Supplement 1, September 1981.
- 26. S. L. Davidson, (Ed), et al., ANC: A Westinghouse Advanced Nodal Computer Code, WCAP-10965-P-A, September 1986 (Westinghouse Proprietary) and WCAP-10966-A, September 1986.
- 27. T. Q. Nguyen, et al, Qualification of the PHOENIX-P/ANC Nuclear Design System for Pressurized Water Reactor Cores, WCAP-11596-P-A, June 1988.
- 28. Deleted.
- 29. S. L. Davidson, et al., Relaxation of Constant Axial Offset Control F Q Surveillance Technical Specification, WCAP-10216-P-A, Revision 1A, February 1994. 30. S. L. Davidson, et al., Westingho use Reload Safety Evaluation Methodology, WCAP-9272-P-A, July 1985.
- 31. P.J. Kersting, et al., Assessment of Clad Flattening and Densification Power Spike Factor Elimination in Westinghouse Nuclear Fuel, WCAP-13589-A, March 1995 (Westinghouse Proprietary) and WCAP-14297-A, March 1995.
- 32. C. L. Beard, et al., BEACON Core Monitoring and Operations Support System, WCAP-12472-P-A, August 1994.
- 33. W.A. Boyd, et al., BEACON Core Monitoring and Operation Support System, WCAP-12472-P-A, Addendum 4, Revision 0, September 2012.
- 34. W.B. Henderson, et al., FIGHTH - A Simplified Calculation of Effective Temperatures in PWR Fuel Rods for Use in Nuclear Design, WCAP-9522, Revision 1, October 1985.
- 35. M. B. Yarbrough, et al., APOLLO - A One Dimensional Neutron Diffusion Theory Program, WCAP-13524-P-A, Revision 1-A, September 1997.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-1 Revision 23 December 2016
4.4 THERMAL
AND HYDRAULIC DESIGN This section discusses the thermal and hydraulic design of the DCPP reactors.
The objective of the thermal and hydraulic design of the reactor core is to provide
adequate heat transfer that is compatible with the heat generation distribution in the
core, so that heat removal by the RCS or the ECCS (when applicable) meets the following performance and safety criteria:
(1) Fuel damage is not expected during normal operation and operational transients (Condition I) or any transient conditions arising from faults of moderate frequency (Condition II). It is not possible, however, to preclude
a very small number of rod failures. These will be within the capability of
the plant cleanup system and are consistent with the plant design bases.
(2) The reactor can be brought to a safe state following a C ondition III event with only a small fraction of fuel rods damaged although sufficient fuel damage might occur to preclude resumption of operation without
considerable outage time.
(3) The reactor can be brought to a safe state and the core can be kept subcritical with acceptable heat transfer geometry following transients
arising from Condition IV events.
Note that fuel damage as used here is defined as penetration of the fission product barrier (i.e., the fuel rod cladding).
4.4.1 DESIGN
BASES
4.4.1.1 General Design Criterion 10, 1971 - Reactor Design The reactor core is designed with appropriate margin to assure that SAFDLs are not exceeded during any condition of normal operation or anticipated operational occurrences.
4.4.1.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations The reactor core is designed to assure that power oscillations that could result in conditions exceeding SAFDLs are not possible or can be reliably and readily detected and suppressed.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-2 Revision 23 December 2016
4.4.2 THERMAL
AND HYDRAULIC DESIGN ACCEPTANCE CRITERIA 4.4.2.1 Departure from Nucleate Boiling Acceptance Criteria There will be at least a 95 percent probability that DNB will not occur on the limiting fuel rods during normal operation and operational transients and any transient conditions arising from faults of moderate frequency (Conditio ns I and II events) at a 95 percent confidence level.
4.4.2.2 Fuel Temperature Acceptance Criteria During Condition I and Condition II events, the maximum fuel temperature shall be less than the melting temperature of UO
- 2. The UO 2 melting temperature for at least 95 percent of the peak kW/ft fuel rods will not be exceeded at the 95 percent confidence level. 4.4.2.3 Core Flow Acceptance Criteria A minimum of 92.5 percent (Unit 1) and 91 percent (Unit 2) of the thermal flowrate (refer to Section 5.1) will pass through the fuel rod region of the core and be effective for fuel rod cooling. Coolant flow through the thimble tubes, as well as leakage from the core
barrel-baffle region into the core, is not effective for heat removal.
4.4.2.4 Hydrodynamic Stability Acceptance Criteria Modes of operation associated with Condition I and Condition II events shall not lead to hydrodynamic instability.
4.4.3 SYSTEM
DESCRIPTION 4.4.3.1 Summary Comparison The core design parameters of the DCPP Unit 1 and Unit 2 reactors are presented in Table 4.1-1.
The reactor core is designed to a minimum DNBR greater than or equal to the design
limit DNBR as well as no fuel centerline melting during normal operation, operational
transients, and faults of moderate frequency.
4.4.3.2 Fuel Cladding Temperatures A discussion of fuel cladding integrity is presented in Section 4.2.1.2.2.
The thermal-hydraulic design ensures that the maximum fuel pellet temperature is
below the melting point of UO 2 (refer to Section 4.4.2.2). To preclude center melting and establish overpower protection system setpoints, a calculated centerline fuel DCPP UNITS 1 &
2 FSAR UPDATE 4.4-3 Revision 23 December 2016 temperature of 4700°F has been selected as the overpower limit. The temperature distribution within the fuel pellet is predomina ntly a function of the local power density and UO 2 thermal conductivity. However, the computation of radial fuel temperature distributions combines crud, oxide, cladding, gap, and pellet conductances. The factors
that influence these conductances, such as gap size (or contact pressure), internal gas
pressure, gas composition, pellet density, and radial power distribution within the pellet, etc., have been combined into a semiempirical thermal model (refer to Section 4.4.3.2.4) with modifications for time-dependent fuel densification (Reference 68). The temperature predictions have been compared to incore fuel
temperature measurements (References 3 through 9) and melt radius data (References
10 and 11) with good results.
4.4.3.2.1 Effect of Fuel Densification on Fuel Rod Temperatures
Fuel densification results in fuel pellet shrinkage.
This affects the fuel temperatures in the following ways:
(1) Pellet radial shrinkage increases the pellet diametral gap that results in increased thermal resistance of the gap and thus higher fuel temperatures (refer to Section 4.2.1.2.2).
(2) Pellet axial shrinkage may produce pellet-to-pellet gaps that result in local power spikes, described in Section 4.3.3.2.1, and thus higher total heat flux hot channel factor, F T Q and local fuel temperatures. However, studies have shown that this penalty can be eliminated for the fuel type present in the DCPP Unit 1 and Unit 2 cores (refer to Section 4.3.3.2.5).
(3) Pellet axial shrinkage results in a fuel stack height reduction and an increase in the linear power generation rate (kW/ft) for a constant core
power level. Using the methods of Reference 68, the increase in linear
power for the fuel rod specifications listed in Table 4.1-1 is 0.2 percent.
Fuel rod thermal parameters (fuel centerline, average, and surface temperatures) are
determined throughout its lifetime considering time-dependent densification. Maximum fuel average and surface temperatures, shown in Figure 4.4-1 as a function of linear
power density (kW/ft), are peak values attained during the fuel lifetime. Similarly, Figure 4.4-2 presents the peak value of fuel centerline temperature versus linear power
density, attained during its lifetime.
The maximum pellet temperature at the hot spot during full power steady state and at the maximum overpower T trip point is shown in Table 4.1-1 for Unit 1 and Unit 2. The principal factors employed in fuel temperature determinations are discussed below.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-4 Revision 23 December 2016 4.4.3.2.2 UO 2 Thermal Conductivity The thermal conductivity of UO 2 was evaluated from data reported in References 7 and 12 through 24.
At the higher temperatures, thermal conductivity is best obtained by utilizing the integral
conductivity to melt, which can be determined with more certainty. From an
examination of the data, it has been conclud ed that the best estimate for the value of kdTC2800 0 o is 93 watts/cm. This conclusion is based on the integral values reported in References 10 and 24 through 28.
The design curve for the thermal conductivity is shown in Figure 4.4-3. The section of the curve at temperatures between 0 and 1300°C is in excellent agreement with the
recommendation of the International Atomic Energy Agency (IAEA) panel (Reference 29). The section of the curve above 1300°C is derived for an integral value of 93 watts/cm (Reference 89).
Thermal conductivity for UO 2 at 95 percent theoretical density can be represented best by the following equation:
()313T10 8.775 0.0238T 11.8 1 kx++= (4.4-1) where:
k is in watts/cm-°C, and T is in °C 4.4.3.2.3 Radial Power Distribution in UO 2 Fuel Rods An accurate radial power distribution as a function of burnup is needed to determine the
power level for incipient fuel melting and other important performance parameters, e.g., pellet thermal expansion, fuel swel ling, and fission gas release rates.
This UO 2 fuel rods radial power distribution as a function of core burnup is determined using a 3D ANC calculation (refer to Sections 4.3.3.10.3 and 15.1.2.4) or with the neutron transport theory LASER (Reference 81) code that has been validated by
comparing code predictions on radial burnup and isotopic distributions with measured
radial microdrill data (References 30 and 31). "Microdrill data" are data obtained from the physical examination of irradiated pellets in a hot cell. Small core samples are removed from different radial positions in a pellet (using a "microdrill"). Isotopic measurements of the fuel samples determine actual UO 2 burnups at the sample points.
A "radial power depression factor," f, is determined using radial power distribution predicted by LASER (Reference 81).
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-5 Revision 23 December 2016 4.4.3.2.4 Gap Conductance The temperature drop across the pellet-cladding gap is a function of the gap size and
the thermal conductivity of the gas in the gap. The gap conductance model is selected
such that when combined with the UO 2 thermal conductivity model, the calculated fuel centerline temperatures reflect the inpile temperature measurements. A more detailed discussion of the gap conductance model is presented in Reference 101.
4.4.3.2.5 Surface Heat Transfer Coefficients The fuel rod surface heat transfer coefficients during subcooled forced convection and
the outer cladding wall temperature for the onset of nucleate boiling is presented in
Section 4.4.3.8.1.
4.4.3.2.6 Fuel Cladding Temperatures
The fuel rod outer surface at the hot spot operates at a temperature of approximately
660°F for steady state operation at rated po wer throughout core life, due to the onset of nucleate boiling. At BOL, this temperature is that of the cladding metal outer surface.
During operation over the life of the core, the build up of oxides and crud on the fuel rod cladding outer surface causes the cladding surface temperature to increase. Allowance is made in the fuel center melt evaluation for this temperature rise. The
thermal-hydraulic DNB limits ensure that adequate heat transfer is provided between
the fuel cladding and the reactor coolant so that cladding temperature does not limit
core thermal output. Figure 4.4-4 shows the axial variation of average cladding temperature for a representative average power rod both at BOL and EOL.
4.4.3.2.7 Treatment of Peaking Factors The total heat flux hot channel factor, F T Q , is defined by the ratio of the maximum to core average heat flux. The design value of F T Q for normal operation is 2.58, allowing for fuel densification effects, as shown in Table 4.3-1. This results in a peak local linear power density of 14.3 kW/ft at full power. The corresponding peak local power at the maximum overpower trip point (118 percent total power) is 16.6 kW/ft. Centerline
temperature at this kW/ft must be below the UO 2 melt temperature over the lifetime of the rod including allowances for uncertainties. From Figure 4.4-2, the centerline temperature at the maximum overpower trip point is well below that required to produce melting. Fuel centerline and average temperature at rated (100 percent) power and at
the maximum overpower trip point for Unit 1 and Unit 2 are presented in Table 4.1-1.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-6 Revision 23 December 2016 4.4.3.3 Departure from Nucleate Boiling Ratio The minimum DNBRs for the rated power, and anticipated transient conditions are given in Table 4.1-1 for Unit 1 and Unit 2. The minimum DNBR in the limiting flow channel will occur downstream of the peak heat flux location (hot spot) due to the increased
downstream enthalpy rise.
DNBRs are calculated by using the correlation and definitions described in
Section 4.4.3.3.1. The THINC-IV (Reference 47) computer code (discussed in Section 4.4.3.15.1) determines the flow distribution in the core and the local conditions in the hot channel for use in the DNB correlation.
The use of hot channel factors is discussed in Section 4.4.3.13.1 (nuclear hot channel factors) and in Section 4.4.3.3.4 (engineering hot channel factors).
4.4.3.3.1 Departure from Nucleate Boiling Technology
The WRB-2 DNB correlation (Reference 85) was developed to take credit for the
VANTAGE+ fuel assembly mixing vane design.
A DNBR limit of 1.17 is also applicable for the WRB-2 correlation. Figure 4.4-20 shows measured critical heat flux (CHF) plotted against predicted CHF using the WRB-2 correlation.
In several cases, the W-3 DNB correlation is used where the WRB-2 is not applicable.
For example, Section 15.2.14.1 uses the W-3 DNB correlation since the system pressure for the limiting statepoint is below 1,000 psia.
The W-3 DNB correlation, and several modifications, have been used in Westinghouse CHF calculations. The W-3 DNB was origin ally developed from single tube data (Reference 34), but was subsequently modified to apply to the 0.422 inch, OD rod low parasitic reinforced grid (R-grid) (References 35 and 92) and low parasitic grid (L-grid) (Reference 36), as well as the 0.374 inch OD (References 37 and 38) rod bundle data.
These modifications to the W-3 DNB correlation have been demonstrated to be adequate for reactor rod bundle design.
A description of the 17 x 17 fuel assembly test program and a summary of the results
are described in detail in Reference 37.
Figure 4.4-5 shows the data obtained in this test program. The test results indicate that
a reactor core using this geometry may operate with a minimum DNBR of 1.28 and
satisfy the design criterion.
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
The WRB-1 correlation (Reference 84) was developed based exclusively on the large bank of mixing vane grid rod bundle CHF data (over 1100 points) that Westinghouse
has collected. The WRB-1 correlation, based on local fluid conditions, represents the
rod bundle data with better accuracy over the wide range of variables than the previous DCPP UNITS 1 &
2 FSAR UPDATE 4.4-7 Revision 23 December 2016 correlation used in design. This correlation accounts directly for both typical and thimble cold wall cell effects, uniform and non-uniform heat flux profiles, and variations in rod heated length and in grid spacing.
Figure 4.4-19 shows measured CHF plotted against predicted CHF using the WRB-1 correlation.
CHF tests which model the 17x17 optimized fuel assembly have been performed with the results described in detail in Reference 87. It was concluded that the CHF
characteristics of the 17x17 optimized fuel asse mbly design are not significantly different from those of 17x17 LOPAR design, and can be adequately described by the "R" grid form of the WRB-1 CHF correlation. Furthermore, the new data can be
incorporated into the "R" grid data base such that the WRB-1 correlation can be applied
to 17x17 LOPAR fuel design without changi ng the DNBR design criterion of 1.17.
4.4.3.3.2 Definition of Departure from Nucleate Boiling Ratio The DNBR, as applied to this design for both typical and thimble cold wall cells is:
" actual"Predicted DNB, q q DNBR= (4.4-5) For the W-3 DNB (R-Grid) correlation, FFq'""S3WEU, Predicted DNB, qx= (4.4-6) when all flow cell walls are heated and q" EU, W-3 is the uniform DNB heat flux as predicted by W-3 DNB correlation and F is the flux shape factor which accounts for non-uniform axial heat flux distributions (Reference 39) with the "C" term modified as in
Reference 34.
F'S is the modified spacer factor described in Reference 37 using an axial grid spacing coefficient, K S = 0.046, and a thermal diffusion coefficient (TDC) of 0.038, based on the 26-inch grid spacing data. Since the actual grid spacing is approximately 20 inches, these values are conservative since the DNB performance was found to improve and
TDC increase as axial grid spacing is decreased (References 35 and 40).
When a cold wall is present for the W-3 DNB correlation, 'F" q" q SCW3,WEU, Predicted DNB,x= (4.4-7)
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-8 Revision 23 December 2016 where: CWF F" q" qDh3,WEU,CW3,WEU,x= (4.4-7A)
"Dh3,WEU, q is the uniform DNB heat flux as predicted by the W-3 DNB cold wall correlation (Reference 34) when not all flow cell walls are heated (thimble cold wall cell).
The cold wall factor (CWF) is provided in References 34 and 39. For the WRB-2 correlation, F q" q"2WRB Predicted DNB,= (4.4-8)
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
F q"1WRB Predicted DNB," q= for WRB1 correlation
where:
F is the same flux shape factor that is used with the W-3 DNB correlation.
4.4.3.3.3 Mixing Technology The rate of heat exchange by mixing betwee n flow channels is proportional to the difference in the local mean fluid enthalpy of the respective channels, the local fluid
density, and the flow velocity. The proportionality is expressed by the dimensionless
TDC, which is defined as:
w'TDC= (4.4-9) where:
w' = flow exchange rate per unit length, lbm/ft-sec = fluid density, lbm/ft 3 V = fluid velocity, ft/sec a = lateral flow area between channels per unit length, ft 2/ft The application of the TDC in the THINC analysis for determining the overall mixing
effect or heat exchange rate is presented in Reference 41.
The TDC is determined by comparing the THINC code predictions with the measured
subchannel exit temperatures. Data for 26-inch axial grid spacing are presented in Figure 4.4-6 where the TDC is plotted versus the Reynolds number. The TDC is found DCPP UNITS 1 &
2 FSAR UPDATE 4.4-9 Revision 23 December 2016 to be independent of the Reynolds number, mass velocity, pressure, and quality over the ranges tested.
The two-phase data (local and subcooled boiling) fell within the scatter of the
single-phase data. The effect of two-phase flow on the value of TDC has been
demonstrated by Cadek (Reference 40), Rowe and Angle (References 42 and 43), and
Gonzalez-Santalo and Griffith (Reference 44). In the subcooled boiling region, the values of TDC were indistinguishable from t he single-phase values. In the quality region, Rowe and Angle show that in the case with rod spacing similar to that in PWR
reactor core geometry, the value of TDC increased with quality to a point and then
decreased but never below the single-phase value. Gonzalez-Santalo and Griffith
showed that the mixing coefficient increased as the void fraction increased.
The data from these tests on the R-grid showed that a design TDC value of 0.038 (for 26 inch grid spacing) can be used in determining the effect of coolant mixing in the
THINC analysis. A mixing test program similar to the one described above was conducted at Columbia University for the 17 x 17 geometry and mixing vane grids on 26-inch spacing (Reference 45). The mean value of TDC obtained from these tests was 0.059, and all data were well above the current design value of 0.038.
Because the reactor grid spacing is approximately 20 inches, additional margin is
available for this design, as the value of TDC increases as grid spacing decreases (Reference 40).
The inclusion of three IFM grids in the upper span of the VANTAGE+ fuel assembly results in a grid spacing of approximately 10 inches. Therefore, the design value of 0.038 for TDC is a conservatively low value for use in VANTAGE+ to determine the effect of coolant mixing in the core thermal performance analysis.
4.4.3.3.4 Hot Channel Factors The total hot channel factors for heat flux and enthalpy rise are defined as the
maximum-to-core average ratios of these quantities. The heat flux hot channel factor
considers the local maximum linear heat generation rate at a point (the "hot spot"), and
the enthalpy rise hot channel factor involves the maximum integrated value along a
channel (the "hot channel").
Each of the total hot channel factors considers a nuclear hot channel factor (refer to Section 4.4.3.13) describing the neutron pow er distribution and an engineering hot channel factor, which allows for variations in flow conditions and fabrication tolerances.
The engineering hot channel factors are made up of subfactors that account for the
influence of the variations of fuel pellet diameter, density, enrichment and eccentricity;
fuel rod diameter pitch and bowing; inlet flow distribution; flow redistribution; and flow
mixing.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-10 Revision 23 December 2016 4.4.3.3.4.1 Heat Flux Engineering Hot Channel Factor, F E Q The heat flux engineering hot channel factor is used to evaluate the maximum heat flux.
This subfactor is determined by statistically combinin g the tolerances for the fuel pellet diameter, density, enrichment, eccentricity, and the fuel rod diameter, and has a value
of 1.03. Measured manufacturing data on Westinghouse fuel verify that this value was
not exceeded for 95 percent of the limiting fuel rods at a 95 percent confidence level.
As shown in Reference 99, no DNB penalty need be taken for the short, relatively low
intensity heat flux spikes caused by variations in the above parameters.
4.4.3.3.4.2 Enthalpy Rise Engineering Hot Channel Factor, F E The effect of variations in flow conditions and fabrication tolerances on the hot channel
enthalpy rise is directly considered in the THINC core thermal subchannel analysis (refer to Section 4.4.3.15.1) under any reacto r operating condition. The following items contribute to the enthalpy rise engineering hot channel factor:
(1) Pellet Diameter, Density and Enrichment, Fuel Rod Diameter, Pitch, and Bowing Design values employed in the THINC analysis are based on applicable limiting tolerances such that design values are met for 95 percent of the
limiting channels at a 95 percent confidence level. The effect of variations
in pellet diameter and enrichment is employed in the THINC analysis as a
direct multiplier on the hot channel enthalpy rise, while the fuel rod
diameter, pitch, and bowing variation, including incore effects, enter in the
preparation of the THINC input values.
(2) Inlet Flow Maldistribution Inlet flow maldistribution in the core thermal performances is discussed in
Section 4.4.3.12.2. A design basis of 5 percent reduction in coolant flow to the hot assembly is used in the THINC-IV analysis.
(3) Flow Redistribution The flow redistribution accounts for the flow reduction in the hot channel
resulting from the high flow resistance in the channel due to the local or
bulk boiling. The effect of the non-uniform power distribution is inherently considered in the THINC analysis.
(4) Flow Mixing The subchannel mixing model incorporated in the THINC code and used
in reactor design is based on experimental data (Reference 46), as
discussed in Section 4.4.3.15.1. The mixing vanes incorporated in the DCPP UNITS 1 &
2 FSAR UPDATE 4.4-11 Revision 23 December 2016 spacer grid design induce additional flow mixing between the various flow channels in a fuel assembly, as well as between adjacent assemblies.
This mixing reduces the enthalpy rise in the hot channel resulting from
local power peaking or unfavorable mechanical tolerances.
4.4.3.3.5 Effects of Rod Bow on Departure from Nucleate Boiling Ratio The phenomenon of fuel rod bowing, as described in Reference 79, must be accounted
for in the DNBR safety analysis of Condition I and Condition II events for each plant
application. Applicable generic credits for margin resulting from retained conservatism
in the evaluation of DNBR and/or margin obtained from measured plant operating parameters (such as F N or core flow), which are less limiting than those required by the plant safety analysis, can be used to offset the effect of rod bow.
The safety analysis for DCPP cor es maintains sufficient margin between the safety analysis DNBR limits and the design DNBR limits. The design DNBR limits are shown below to accommodate full flow and low flow DNBR penalties identified in Reference 80, which are applicable to 17x17 VANTAGE+
fuel assembly analysis utilizing the WRB-2 correlation.
However, for the upper assembly span of VANTAGE+ fuel where additional restraint is provided with the IFM grids, the grid-to-grid s pacing in DNB limiting span is approximately 10 inches . Using the rod bow topical report methods (Reference 79), and scaling with the NRC approved factor results in predicted channel closure in the limiting spans of less than 50 percent closure; no rod bow DNBR penalty is required in the 10 inch spans in the VANTAGE+ safety analyses.
VANTAGE+ Design Limit Typical Cell 1.34 Thimble Cell 1.32
Safety Limit Typical Cell 1.71 Thimble Cell 1.68
The maximum rod bow penalties accounted for in the design safety analysis are based
on an assembly average burnup of 24,000 MWD/MTU based on Reference 100. At burnups greater than 24,000 MWD/MTU, credit is taken for the effect of F N burndown.
Due to the decrease in fissionable isotopes and the buildup of fission product inventory, no additional rod bow penalty is required.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-12 Revision 23 December 2016
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
4.4.3.3.6 Transition Core
The Westinghouse transition core DNB methodology is given in References 89 and 90 and has been approved by the NRC via Reference 91. Using this methodology, transition cores are analyzed as if they were full cores of one assembly type (full
LOPAR or full VANTAGE 5), applying the applicable transition core penalties. This penalty was included in the safety analysis limit DNBRs such that sufficient margin over the design limit DNBR existed to acc ommodate the transition core penalty and the appropriate rod bow DNBR penalty. However, since the transition to a full VANTAGE 5 core has been completed, various analyses, such as large break and small LOCA analysis, have assumed a full VANTAGE 5 core and no longer assume a transition core
penalty.
The LOPAR and VANTAGE 5 designs have been shown to be hydraulically compatible in Reference 85.
4.4.3.4 Flux Tilt Considerations Significant quadrant power tilts are not anticipated during normal operation since this
phenomenon is caused by asymmetric pert urbations. A dropped or misaligned RCCA could cause changes in hot channel factors. These events are analyzed separately in
Chapter 15.
Other possible causes for quadrant power tilts include X-Y xenon transients, inlet
temperature mismatches, enrichment variations within tolerances, and so forth.
In addition to unanticipated quadrant power tilts, other readily expl ainable asymmetries may be observed during calibration of the excore detector quadrant power tilt alarm.
During operation, at least one power distribution measurement is taken per effective-
full-power month. Each of these power distribution measurements is reviewed for
deviations from the expected power distributions. The acceptability of an observed
asymmetry, planned or otherwise, depends solely on meeting the required accident
analyses assumptions. In practice, once acceptability has been established by review
of the power distribution measurements, the quadrant power tilt alarms and related
instrumentation are adjusted to indicate zero quadrant tilt, 1.00 quadrant power tilt ratio, as the final step in the calibration process. Proper functioning of the quadrant power tilt
alarm is significant because no allowances are made in the design for increased hot
channel factors due to unexpecte d developing flux tilts since all likely causes are prevented by design or procedures or specifically analyzed. Finally, in the event that
unexplained flux tilts do occur, the Technical Specification (Reference 82) stipulates
appropriate corrective actions to ensure continued safe operation of the reactor.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-13 Revision 23 December 2016 4.4.3.5 Void Fraction Distribution The calculated core average and the hot subchannel maximum and average void
fractions are presented in Tables 4.4-1 and 4.4-2 for operation at full power with design
hot channel factors for Unit 1 and Unit 2, respectively. The void fraction distribution in the core is presented in Reference 47. The void fraction as a function of
thermodynamic quality is shown in Figure 4.4-10. The void models used in the THINC-
IV computer code are described in Section 4.4.3.8.3.
4.4.3.6 Core Coolant Flow Distribution Coolant enthalpy rise and flow distributions are shown for the 4-foot elevation
(1/3 of core height) in Figure 4.4-7, 8-foot elevation (2/3 of core height) in Figure 4.4-8, and at the core exit in Figure 4.4-9. These distributions correspond to a representative
Westinghouse 4-loop plant. The THINC code analysis for this case utilized a uniform
core inlet enthalpy and inlet flow distribution.
4.4.3.7 Core Pressure Drops and Hydraulic Loads
4.4.3.7.1 Core Pressure Drops The analytical model and experimental data used to calculate the pressure drops, for
the full power conditions given in Table 4.1-1 , are described in Section 4.4.3.8.2. The core pressure drop consists of the fuel assembly, lower core plate, and upper core plate
pressure drops. These pressure drops are based on the best estimate flow, as
described in Section 5.1.6. Section 5.1.6 also defines the thermal design flow (minimum flow), which is the basis for reactor core thermal performance, and the mechanical design flow (maximum flow), which is used in the mechanical design of the
reactor vessel internals and fuel assemblies. Since the best estimate flow is that which
is most likely to exist in an operating plant, the calculated core pressure drops in
Table 4.1-1 are greater than pressure drops previously quoted using the thermal design
flow. The relation between best estimate flow, thermal design flow, and mechanical
design flow is illustrated in Figure 5.1-2.
4.4.3.7.2 Hydraulic Loads Maximum flow conditions are limiting because hydraulic loads are a maximum. The most adverse flow conditions occur during a LOCA, as discussed in Section 15.4.1.
Hydraulic loads at normal operating conditio ns are calculated considering the best estimate flow and accounting for the best estimate core bypass flow. Core hydraulic loads at cold plant startup conditions are based on the cold best estimate flow, but are adjusted to account for the coolant density difference. Conservative core hydraulic
loads for a pump overspeed transient, which are based on flowrates 20 percent greater than the mechanical design flow (refer to Section 5.1.6), are evaluated to be greater than twice the fuel assembly weight.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-14 Revision 23 December 2016 The hydraulic verification tests are discussed in References 48 and 87.
4.4.3.8 Correlation and Physical Data
4.4.3.8.1 Surface Heat Transfer Coefficients Forced convection heat transfer coefficients are obtained from the familiar Dittus-Boelter
correlation (Reference 49), with the properties evaluated at bulk fluid conditions:
0.4 kµp C 0.8 G e D 0.023 k e hD=µ (4.4-10) where:
h = heat transfer coefficient, Btu/hr-ft 2-°F D e = equivalent diameter, ft k = thermal conductivity, Btu/hr-ft-°F G = mass velocity, lbm/hr-ft 2 µ = dynamic viscosity, lbm/ft-hr Cp = heat capacity, Btu/lbm-°F
This correlation has been shown to be conservative (Reference 50) for rod bundle
geometries with pitch-to-diameter ratios in the range used by PWRs.
The onset of nucleate boiling occurs when the cladding wall temperature reaches the
amount of superheat predicted by Thom's (Reference
- 51) correlation. After this occurrence, the outer cladding wall temperature is determined by:
T sat = [0.072 exp (-P/1260)] (q")
0.5 (4.4-11) where:
TSAT = wall superheat, T w - Tsat , °F q" = wall heat flux, Btu/hr-ft 2 P = pressure, psia
T w = outer cladding wall temperature, °F T SAT = saturation temperature of coolant at P, °F 4.4.3.8.2 Total Core and Vessel Pressure Drop Pressure losses occur as a result of viscous drag (friction) and/or geometry changes (form) in the fluid flowpath. The flow field is assumed to be incompressible, turbulent, single-phase water. Two-phase consideratio ns are neglected in the vessel pressure DCPP UNITS 1 &
2 FSAR UPDATE 4.4-15 Revision 23 December 2016 drop evaluation because the core average void is negligible (refer to Section 4.4.3.5 and Tables 4.4-1 and 4.4-2).
Two-phase flow considerations in the core thermal subchannel analyses are considered and the models are discussed in Section 4.4.3.12.3. Core and vessel pressure losses are calculated by equations of the form:
(144)c 2g 2 e D FL K L+= (4.4-12) where: P L = pressure drop, lb f/in 2 = fluid density, lbm/ft 3 L = length, ft D e = equivalent diameter, ft V = fluid velocity, ft/sec g c = 2 sec f 1b ft m 1b 32.174 K = form loss coefficient, dimensionless F = friction loss coefficient, dimensionless
Fluid density is assumed to be constant at an appropriate value for each component in
the core and vessel. Because of the complex core and vessel flow geometry, precise
analytical values for the form and friction loss coefficients are not available. Therefore, experimental values for these coefficients are obtained from geometrically similar
models.
The results of full-scale tests of core components and fuel assemblies were utilized in
developing the core pressure loss characteristics. The pressure drop for the vessel was
obtained by combining the core pressure loss with correlation of 1/7th scale model
hydraulic test data on a number of vessels (References 52 and 53) and form loss relationships (Reference 54). Moody (Reference 55) curves were used to obtain the single-phase friction factors.
Tests of the primary coolant loop flowrates are made (refer to Section 4.4.6.1) prior to initial criticality to verify that the flowrates used in the design are conservative.
4.4.3.8.3 Void Fraction Correlation Three separate void regions are considered in flow boiling in a PWR as illustrated in
Figure 4.4-10. They are the wall void region (no bubble detachment), the subcooled
boiling region (bubble detachment), and the bulk boiling region.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-16 Revision 23 December 2016 In the wall void region, local boiling begins at the point where the cladding temperature reaches the amount of superheat predicted by Thom's (Reference 51) correlation (refer to Section 4.4.3.8.1). The void fraction in this region is calculated using Maurer's (Reference 56) relationship. The bubble detachment point, where the superheated
bubbles break away from the wall, is determined by using Griffith's (Reference 57)
relationship.
The void fraction in the subcooled boiling region (i.e., after the detachment point) is
calculated from the Bowring (Reference 58) correlation. This correlation predicts the
void fraction from the detachment point to the bulk boiling region.
The void fraction in the bulk boiling region is predicted by using homogeneous flow
theory and assuming no slip. The void fraction in this region is, therefore, a function of
steam quality only.
4.4.3.9 Thermal Effects of Operational Transients DNB core safety limits are generated as a function of coolant temperature, pressure, core power, and axial power imbalance. Steady state operation within these safety
limits ensures that the minimum DNBR is not less than the safety limit DNBR.
Figure 15.1-1 shows lines at the safety limit DNBR and the resulting overtemperature T trip lines (which are part of the Technical Specifications), plotted as T versus T-average for various pressures. This system provides adequate protection against anticipated operational transients that are slow with respect to fluid transport delays in
the primary system. In addition, for fast transients (e.g., uncontrolled rod bank withdrawal at power incident) (refer to Section 15.2.2), specific protection functions are provided as described in Section 7.2; their use is described in Chapter 15 (refer to Table 15.1-2). Fuel rod thermal response is discussed in Section 4.4.3.18.
4.4.3.10 Uncertainties in Estimates
4.4.3.10.1 Uncertainties in Fuel and Cladding Temperatures As discussed in Section 4.4.3.2, the fuel temperature is a function of crud, oxide, cladding, gap, and pellet conductance. Uncertainties in the fuel temperature calculation are essentially of two types: fabrication uncertainties, such as variations in the pellet
and cladding dimensions and the pellet density; and model uncertainties, such as variations in the pellet conductivity and the gap conductance. These uncertainties have
been quantified by comparison of the thermal model to the incore thermocouple
measurements (References 3 through 9), by out-of-pile measurements of the fuel and
cladding properties (References 7 and 12 through 23), and by measurements of the fuel and cladding dimensions during fabrication.
The effect of densification on fuel temperature uncertainties is presented in Reference 68.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-17 Revision 23 December 2016 In addition, the measurement uncertainty in determining the local power, and the effect of density and enrichment variations on local power, are considered in establishing the
heat flux hot channel factor.
Uncertainty in determining cladding temperature results from uncertainties in the crud
and oxide thickness. Because of the excellent heat transfer between the surface of the
rod and the coolant, the film temperature drop does not appreciably contribute to the
uncertainty.
Reactor trip setpoints, as specified in the Technical Specifications, include allowance for
instrument and measurement uncertainties such as calo rimetric error, instrument drift, and channel reproducibility.
4.4.3.10.2 Uncertainties in Pressure Drops Core and vessel pressure drops based on the best estimate flow, as described in
Section 5.1, are quoted in Table 4.1-1. The uncertainties quoted are based on the
uncertainties in both the test results and the analytical extension of these values to the
reactor application.
4.4.3.10.3 Uncertainties Due to Inlet Flow Maldistribution Uncertainties in the inlet flow maldistribution criteria used in the core thermal analyses
are discussed in Section 4.4.3.12.2.
4.4.3.10.4 Uncertainty in Departure from Nucleate Boiling Correlation The uncertainty in the DNB correlation (refer to Section 4.4.3.3) can be written as a statement on the probability of not being in DNB based on the DNB data statistics. This
is discussed in Section 4.4.3.3.2.
4.4.3.10.5 Uncertainties in Departure from Nucleate Boiling Ratio Calculations The uncertainties in the DNBRs calculated by THINC analysis (refer to Section 4.4.3.15.1) due to uncertainties in the nuclear peaking factors are accounted for by applying conservatively high values of the nuclear peaking factors and including measurement error allowances in the statistical evaluation of the limit DNBR (refer to Section 4.4.4.1) using the Improved Thermal Design Procedure (ITDP) (Reference 86).
In addition, conservative values for the engineering hot channel factors are used (refer to Section 4.4.3.3.4). The results of a sensitivity study with THINC-IV show that the minimum DNBR in the hot channel is relatively insensitive to variations in the core-wide radial power distribution (for the same value of F N).
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-18 Revision 23 December 2016 The ability of the THINC-IV computer code to accurately predict flow and enthalpy distributions in rod bundles is discussed in Section 4.4.3.15.1 and in Reference 59. The sensitivity of the minimum DNBR in the hot channel to the void fraction correlation (refer to Section 4.4.3.8.3), the inlet velocity and exit pressure distributions, and the grid pressure loss coefficients have been studied (Reference 47). The results show that the
minimum DNBR in the hot channel is relatively insensitive to variations in these
parameters.
4.4.3.10.6 Uncertainties in Flowrates The uncertainties associated with loop flowrates are discussed in Section 5.1. For core
thermal performance evaluations, a thermal design loop flow is used which is less than
the best estimate loop flow (by approximately 4 percent). In addition, another
7.5 percent
(Unit 1) and 9.0 percent (Unit 2) of the thermal design flow is assumed to be ineffective for core heat removal capability because it bypasses the core through the
various available flowpaths described in Section 4.4.3.12.1.
4.4.3.10.7 Uncertainties in Hydraulic Loads As discussed in Section 4.4.3.7.2, hydraulic loads on the fuel assembly are evaluated for a pump overspeed transient that creates f lowrates 20 percent greater than the mechanical design flow.
4.4.3.10.8 Uncertainty in Mixing Coefficients The value of the mixing coefficient, TDC, use d in THINC analyses for this application is 0.038. The mean value of TDC obtained in the R-grid mixing tests described in Section 4.4.3.3.2 was 0.042 (for 26-inch grid spacing). The value of 0.038 is one standard deviation below the mean value and 90 percent of the data gives values of
TDC greater than 0.038 (Reference 40).
The results of the mixing tests discussed in Section 4.4.3.3.3, had a mean TDC value of 0.059 and standard deviation of = 0.007. Hence, the current design TDC value is almost three standard deviations below the mean for 26-inch grid spacing.
Since the value of TDC increases as grid spacing decreases, the design value of 0.038 for TDC is a conservatively low value for use in VANTAGE+ to determine the effect of coolant mixing in the core thermal performance analysis. Refer to Section 4.4.3.3.3 for a discussion of the current reactor grid spacing of approximately 20 inches and IFM grid spacing of approximately 10 inches.
4.4.3.11 Plant Configuration Data
Plant configuration data for the thermal-hydraulic and fluid systems external to the core
are provided in Chapters 5, 6, and 9. Implementation of the ECCS is discussed in
Chapters 6 and 15. Some specific areas of interest are:
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-19 Revision 23 December 2016 (1) Total coolant flow rate for the RCS is provided in Table 5.1-1.
(2) Total RCS volume is given in Table 5.1-1.
(3) The flowpath length through each volume is calculated from physical data and the component pressure drops as provided in Table 5.1-1.
(4) The height of fluid in each component of the RCS may be determined from the physical data and data provided in Table 5.1-1. The RCS components are water-filled during power operation with the pressurizer being approximately 60 percent water-filled.
(5) ECCS components are located to meet the criteria for net positive suction head described in Section 6.3.
(6) Line lengths and sizes for the safety injection system are determined so as to guarantee a total system resistance that will provide, as a minimum, the fluid delivery rates assumed in the safety analyses described in Chapter 15.
(7) The design data for RCS components, including volumes (diameter), flows, and pressure and temperature, are presented in Section 5.5.
(8) RCS steady state pressure and temperature distribution are presented in Table 5.1-1.
4.4.3.12 Core Hydraulics
4.4.3.12.1 Flowpaths Considered in Core Pressure Drop and Thermal Design The following flowpaths are considered:
(1) Flow through the spray nozzles i nto the upper head for cooling purposes (2) Flow entering the RCCA guide thimbles to cool core components
(3) Leakage flow from the vessel inl et nozzle directly to the vessel outlet nozzle through the gap between vessel and barrel (4) Flow entering the core from the baffle-barrel region through the gaps between the baffle plates (5) Flow introduced between baffle and barrel to cool these components (6) Flow through the empty guide thimble tubes DCPP UNITS 1 &
2 FSAR UPDATE 4.4-20 Revision 23 December 2016 The above contributions are evaluated to confirm that the design basis value of
7.5 percent
(Unit 1) and 9.0 percent (Unit 2) core bypass flow is met.
4.4.3.12.2 Inlet Flow Distribution Data from several 1/7 scale hydraulic reactor model tests (References 52, 53, and 60)
have been considered in arriving at the core inlet flow maldistribution criteria to be used
in the THINC analyses (refer to Section 4.4.3.15.1). THINC (Reference 41) analyses have indicated that a conservative design basis is to consider a 5 percent reduction in
the flow to the hot assembly (Reference 61).
The experimental error in the inlet velocity distribution has been estimated in
Reference 47. The sensitivity of changes in inlet velocity distributions to hot channel
thermal performance is shown to be small.
The effect of the total flowrate on the inlet velocity distribution was studied in the
experiments of Reference 52. As expected, no significant variation could be found in
inlet velocity distribution with reduced flowrate.
4.4.3.12.3 Empirical Friction Factor Correlations, F E Q Two empirical friction factor correlations are used in the THINC-IV computer code (refer to Section 4.4.3.15.1).
The friction factor in the axial direction, parallel to the fuel rod axis, uses the
Novendstern-Sandberg (Reference 62) correlation. This correlation consists of the
following:
(1) For isothermal conditions, this correlation uses the Moody (Reference 55) friction factor, including surface roughness effects.
(2) Under single-phase heating conditions, a factor is applied based on the values of the coolant density and viscosity at the temperature of the
heated surface and at the bulk coolant temperature.
(3) Under two-phase flow conditions, the homogeneous flow model proposed by Owens (Reference 63) is used with a modification to account for a
mass velocity and heat flux effect.
The flow in the lateral directions, normal to the fuel rod axis, views the reactor core as a
large tube bank. Thus, the lateral friction factor proposed by Idel'chik (Reference 54) is applicable. This correlation is of the form:
0.2ReAF L L= (4.4-13)
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-21 Revision 23 December 2016 where: A is a function of the rod pitch and diameter as given in Reference 54
Re L is the lateral Reynolds number based on rod diameter
Extensive comparisons of THINC-IV predictions using these correlations to
experimental data are given in Reference 59, and verify the applicability of these correlations in PWR design.
4.4.3.13 Influence of Power Distribution The core power distribution, which at BOL is largely established by fuel enrichment, loading pattern, and core power level, is also a function of variables such as control rod worth and position and fuel depletion throughout lifetime. Although radial power
distributions in various planes of the core are often illustrated for general interest, the
core radial enthalpy rise distribution, as determined by the integral of power over each
channel, is of greater importance for DNB analyses. These radial power distributions, characterized by F N (defined in Section 4.3.3.2.2), as well as axial heat flux profiles, are discussed in the following two sections.
4.4.3.13.1 Nuclear Enthalpy Rise Hot Channel Factor, F N Given the local power density q' (kW/ft) at a point x, y, z in a core with N fuel rods and
height H:
()dzz)y,(x,q' N ldzz,y,xq'Maxpower rod averagepower rod hot H o rods alloo H o N F== (4.4-14)
The location of minimum DNBR depends on the axial profile and its magnitude depends on the enthalpy rise up to that point. The maximum value of the rod integral is used to identify the most likely rod for minimum DNBR. An axial power profile is obtained which, when normalized to the design value of F N , recreates the axial heat flux along the limiting rod. The surrounding rods are assumed to have the same axial profile with rod average powers that are typical of distributions found in hot assemblies. In this
manner, worst case axial profiles can be combined with worst case radial distributions
for reference DNB calculations.
Local heat fluxes are obtained by using hot channe l and adjacent channe l explicit power shapes which take into account variations in horizontal power shapes throughout the
core. The sensitivity of the THINC-IV analysis to radial power shapes is discussed in
Reference 47.
For operation at a fraction P of full power, the design F N is given by:
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-22 Revision 23 December 2016 F N = 1.59 [1 + 0.3 (1-P)] (VANTAGE+) (4.4-15)
HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
F N = 1.56 [1 + 0.3 (1-P)] (LOPAR)
The permitted relaxation of F N is included in the DNB protection setpoints and allows radial power shape changes with rod insertion to the insertion limits (Reference 64), thus allowing greater flexib ility in the nuclear design.
4.4.3.13.2 Axial Heat Flux Distributions As discussed in Section 4.3.3.2, the axial he at flux distribution can vary as a result of rod motion, power change, or due to spatial xenon transients that may occur in the axial
direction. Consequently, it is necessary to measure the axial power imbalance by means of the excore nuclear detectors (refe r to Section 4.3.3.2.7) and protect the core from excessive axial power imbalance.
The reactor trip system provides automatic reduction of the trip setpoint in the overtemperature T channels on excess ive axial power imbalance, i.e., when an extremely large AO corresponds to an axial shape that could lead to a DNBR, which is less than that calculated for the reference DNB design
axial shape.
The reference DNB design axial shape is a chopped cosine with a peak-to-average ratio of 1.55.
4.4.3.14 Core Thermal Response A general summary of the steady state the rmal-hydraulic design parameters including thermal output, flowrates, etc., is provided in Table 4.1-1. As stated in Section 4.4.2, the acceptance criteria are to prevent DNB and to prevent fuel melting for Conditions I and II events. The protective systems described in Chapter 7 (Instrumentation and Controls) are designed to meet these bases. The response of the core to Condition II
transients is given in Chapter 15.
4.4.3.15 Analytical Techniques
4.4.3.15.1 Core Analysis The objective of reactor core thermal analysis is to determine the maximum heat
removal capability in all flow subchannels, and to show that the core safety limits, as
presented in the Technical Specifications, are not exceeded. The thermal design
considers local variations in dimensions, power generation, flow redistribution, and
mixing. THINC-IV is a realistic three-dimensi onal matrix model developed to account for hydraulic and nuclear effects on the enthalpy rise in the core (References 47 and DCPP UNITS 1 &
2 FSAR UPDATE 4.4-23 Revision 23 December 2016 59). The behavior of the hot assembly is determined by superimposing the power distribution among the assemblies upon the inlet flow distribution, while allowing for flow mixing and distribution between assemblies.
The average flow and enthalpy in the
hottest assembly is obtained from the core-wide assembly-by-assembly analysis. The
local variations in power, fuel rod and pel let fabrication, and mixing within the hottest assembly are then superimposed on the average conditions of the hottest assembly to
determine conditions in the hot channel.
The following sections describe the use of the THINC code in the thermal-hydraulic
design evaluation.
4.4.3.15.1.1 Steady State Analysis The THINC-IV computer program determines coolant density, mass velocity, enthalpy, vapor void, static pressure, and DNBR distributions al ong parallel flow channels within a reactor core under all expected operating conditions. The core region being studied is
made up of a number of contiguous elements in a rectangular array extending the full
length of the core. An element may represent any region of the core from a single
assembly to a subchannel.
The momentum and energy exchange between elements in the array are described by
the conservation of energy and mass equations, the axial momentum equation, and two
lateral momentum equations that couple each element with its neighbors. The
momentum equations used in THINC-IV incorporate f rictional loss terms that represent
the combined effects of frictional and form drag due to the presence of the grids and
fuel assembly nozzles in the core. The cross flow resistance model used in the lateral momentum equations was developed from experimental data for flow normal to tube banks (Reference 54). The energy equation for each element also contains additional
terms that represent the energy gain or loss due to the cross flow between elements.
The unique feature in THINC-IV is that lateral momentum equations, which include both inertial and cross flow resistance terms, are incorporated into the calculation scheme.
Another important consideration in THINC-IV is that the entire velocity field is solved, en
masse, by a field equation. The solution method is complex and some simplifying techniques must be employed. Because the reactor flow is chiefly in the axial direction, the core flow field is primarily one-dimensional, and it is reasonable to assume that the
lateral velocities and the parameter gradients are larger in the axial direction than the
lateral direction. Thus, a perturbation technique is used to represent separately the
axial and lateral parameters in the conservation equations.
Three THINC-IV computer runs constitute one design run: a core-wide analysis, a hot-
assembly analysis, and a hot subchannel analysis.
The first computation is a core-wide assembly-by-assembly analysis that uses an inlet
velocity distribution modeled from experimental reactor models (References 52, 53, and
- 60) (refer to Section 4.4.3.12.2). The core is made up of a number of contiguous fuel DCPP UNITS 1 &
2 FSAR UPDATE 4.4-24 Revision 23 December 2016 assemblies divided axially into increments of equal length. The system of perturbed and unperturbed equations is solved for this array giving the flow, enthalpy, pressure drop, temperature, and void fraction in each assembly. This computation determines the inter-assembly energy and flow exchange at each elevation for the hot assembly.
THINC-IV stores this information, then uses it for the subsequent hot assembly analysis.
In the second computation, each computational element represents one-fourth of the hot assembly. The inlet flow and the amount of momentum and energy interchange at
each elevation are known from the previous core-wide calculation. The same solution technique is used to solve for the local parameters in the hot one-quarter assembly.
The third computation further divides the hot assembly into channels consisting of
individual fuel rods to form flow channels. The local variations in power, fuel rod and pellet fabrication, fuel rod spacing and mixing (engineering hot channel factors) within
the hottest assembly are imposed on the average conditions of the hottest fuel
assembly to determine the conditions in the hot channel. Engineering hot channel
factors are described in Section 4.4.3.3.4.
4.4.3.15.1.2 Experimental Verification An experimental verification (Reference 59) of the THINC-IV analysis for core-wide
assembly-by-assembly enthalpy rises, as well as enthalpy rises in a non-uniformly heated rod bundle, have been obtained. In these tests, system pressure, inlet
temperature, mass flowrate, and heat fluxes were typical of present PWR core designs.
During reactor operation, various incore monitoring systems obtain measured data indicating core performance. Assembly power distributions and assembly mixed mean temperature are measured and can be converted into the proper three-dimensional
power input needed for the THINC programs. These data can then be used to verify the
Westinghouse thermal-hydraulic design codes.
One standard startup test is the natural circulation test in which the core is held at a
very low power (2 percent) and the pumps are turned off. The core will then be cooled by the natural circulation currents created by the power differences in the core. During natural circulation, a thermal siphoning effect occurs, resulting in the hotter assemblies
gaining flow, thereby creating significant inte r-assembly cross flow. Tests with significant cross flow are of more value in code verification.
Inter-assembly cross flow is caused by radial variations in pressure that are caused in turn by variations in the axial pressure drops in different assemblies. Under normal operating conditions (subcooled forced convection), the axial pressure drop is due mainly to friction losses. Because all assemblies have the same geometry, all
assemblies have nearly the same axial pressure drops, and cross flow velocities are
small. However, under natural circulation conditions (low flow) the axial pressure drop
is due primarily to the difference in elevation head (or coolant density) between
assemblies. This phenomenon can result in relatively large radial pressure gradients DCPP UNITS 1 &
2 FSAR UPDATE 4.4-25 Revision 23 December 2016 and, therefore, in higher cross flow velocities than at normal reactor operating conditions.
Incore instrumentation was used to obtain the assembly-by-assembly core power
distribution during a natural circulation test.
Assembly exit temperatures during the
natural circulation test on a 157-assembly three-loop plant were predicted using
THINC-IV. The predicted data points were plotted as assembly temperature rise versus
assembly power, and a least squares fitting program was used to generate an equation
that best fits the data. The result is the straight line presented in Figure 4.4-11 and is
predicted closely by THINC-IV. This agreement verifies the lateral momentum
equations and the cross flow resistance model used in THINC-IV.
Data have been obtained for Westinghouse plants operating from 67 to 101 percent of
full power. A representative cross-section of the data obtained from a two-loop and a three-loop reactor was analyzed to verify the THINC-IV predictions that are compared
with the experimental data in Figures 4.4-12 and 4.4-13.
The predicted assembly exit temperatures were compared with the measured exit
temperatures for each data run. The standa rd deviations of the measured and predicted assembly exit temperatures are compared for both THINC-IV and THINC-I, and are given in Table 4.4-3. THI NC-IV generally fits the data somewhat more accurately than THINC-I. Both codes are conservative and predict exit temperatures
higher than measured values for the high-powered assemblies. Experimental verification of the THINC-IV subchannel calculation has been obtained from exit
temperature measurements in a non-uniformly heated rod bundle (Reference 66).
Figure 4.4-14 compares, for a typical run, the measured and predicted temperature rises as a function of the power density in the channel. The THINC-IV results correctly
predict the temperature gradient across the bundle.
In Figure 4.4-15, the measured and predicted temperature rises are compared for a
series of runs at different pressures, flows, and power levels. Again, the measured points represent the average of the measurements taken in the various quadrants. The
THINC-IV predictions provide a good representation of the data.
Thus, the THINC-IV analysis provides a realistic evaluation of the core performance and
is used in the thermal analyses as described above.
4.4.3.15.1.3 Transient Analysis The THINC-III thermal-hydraulic computer co de (Reference 41) is the third section of the THINC program and has transient DNB analysis capability.
The conservation equations needed for the transient analysis are included in THINC-III
by adding the necessary accumulation terms to the conservation equations used in the DCPP UNITS 1 &
2 FSAR UPDATE 4.4-26 Revision 23 December 2016 steady state analysis. The input description must now include one or more of the following time arrays:
(1) Inlet flow variation (2) Heat flux distribution (3) Inlet pressure history
At the beginning of the transient, the calculation procedure is carried out as in the
steady state analysis. The THINC-III code is first run in the steady state mode to
ensure conservatism with respect to THINC-IV and to provide the steady state initial
conditions at the start of the transient.
The time is incremented by an amount determined either by the user or by the program. At each new time step, the
accumulation terms are evaluated using the information from the previous time step.
This procedure is continued until a preset maximum time is reached.
At various times during the transient, steady state THINC-IV is applied to show that the
application of THINC-III is conservative. The THINC-III code does not have the
capability for evaluating fuel rod thermal response. This is treated by the methods
described in Section 15.1.9.
4.4.3.15.2 Fuel Temperatures As discussed in Section 4.4.3.2, fuel rod behavior is evaluated with a semiempirical thermal model that considers, in addition to the thermal aspects, such items as cladding creep, fuel swelling, fission gas release, release of absorbed gases, cladding corrosion, elastic deflection, and helium solubility.
A detailed description of the thermal model can be found in References 67 and 83 with
the modifications for the time-dependent densification given in Reference 68.
4.4.3.16 Hydrodynamic and Flow-Power Coupled Instability Boiling flow may be susceptible to thermohydrodynamic instabilities (Reference 69).
These instabilities may cause a change in th ermo-hydraulic conditions that may lead to a reduction in the DNB heat flux relative to that observed during a steady flow condition, or to undesired forced vibrations of core components. Thus, the thermo-hydraulic design criterion states that operation during Condition I and Condition II events shall not lead to thermohydrodynamic instabilities.
Two specific types of flow instabilities are considered by Westinghouse for PWR
operation. These are the Ledinegg, or flow excursion, type of static instability and the density wave type of dynamic instability.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-27 Revision 23 December 2016 A Ledinegg instability involves a sudden change in flowrate from one steady state to another. This instability occurs (Reference 69) when the slope of the RCS pressure drop-flowrate curve becomes algebraically smaller than the slope of the loop supply (pump head) pressure drop-flowrate curve. The Westinghouse pump head curve has a
negative slope whereas the RCS pressure drop-flow curve has a positive slope over the
Conditions I and II operational ranges. Thus, Ledinegg instability will not occur.
The mechanism of density wave oscillations in a heated channel has been described by Lahey and Moody (Reference 70).
The method developed by Ishii (Reference 71) for parallel closed channel systems
evaluates if a given condition is stable with respect to the density wave type of dynamic
instability. This method had been used to as sess the stability of typical Westinghouse reactor designs (References 72, 73, and 74) under operating Conditions I and II. The results indicate that a large margin to density wave instability exists (e.g., an increase in
the order of 200 percent of rated reactor power would be required) for the inception of
this type of instability.
Flow instabilities that have been observed have occurred almost exclusively in closed channel systems operating at low pressures relative to the Westinghouse PWR
operating pressures. Kao, Morgan, and Parker (Refer ence 75) analyzed parallel closed channel stability experiments simulating a reactor core flow. These experiments were conducted at pressures up to 2200 psia. The results showed that for flow and power
levels typical of power reactor conditions, no flow oscillations could be induced above
1200 psia. Additional evidence that flow instabilities do not adversely affect thermal margin is provided by data from rod bundle DNB tests.
In summary, it is concluded that thermo-hydrodynamic instabilities will not occur under Conditions I and II events for Westinghouse PWR designs. A large power margin exists to predicted inception of such instabilities. Analysis has been performed and shows that
minor plant-to-plant differences in Westinghouse reactor designs such as fuel assembly
arrays, core power flow ratios, fuel assembly length, etc., will not result in gross
deterioration of the above power margins.
4.4.3.17 Temperature Transient Effects Analysis Waterlogging damage of a fuel rod could occ ur as a consequence of a power increase on a rod after water has entered the fuel rod through a cladding defect and will continue
until the fuel rod internal pressure equals the reactor coolant pressure. A subsequent
power increase raises the temperature and, hence, could raise the pressure of the water contained within the fuel rod. Zirconium alloy-clad fuel rods, which have failed due to waterlogging (References 76 and 77) indicate that very rapid power transients
are required for fuel failure. Normal operational transients are limited to about 40 cal/gm-min. (peak rod) while the Spert tests (Reference 76) indicate that 120 to 150 cal/gm is required to rupture the clad even wit h very short transients (5.5 msec. period).
Release of the internal fuel rod pressure is expected to have a minimal effect on the DCPP UNITS 1 &
2 FSAR UPDATE 4.4-28 Revision 23 December 2016 RCS (Reference 76) and is not expected to result in failure of additional fuel rods (Reference 77). Ejection of fuel pellet fragments into the coolant stream is not expected (References 76 and 77). A cladding breach due to waterlogging is thus expected to be similar to any fuel rod failure mechanism that exposes fuel pellets to the reactor coolant
stream. Waterlogging has not been identified as the mechanism for cladding distortion
or perforation of any Westinghouse Zirconium alloy-clad rods.
An excessively high fuel rod internal gas pressure could cause cladding failure. During
operational transients, fuel rod cladding rupture due to high internal gas pressure is
precluded by adopting a design basis that the fuel rod internal gas pressure remains
below the value that causes the fuel-cladding diametral gap to increase due to outward
cladding creep.
4.4.3.18 Potentially Damaging Temperature Effects During Transients A fuel rod experiences many operational transients (intentional maneuvers) while in the
core. Several thermal effects must be considered when designing and analyzing fuel rod performance.
The cladding can be in contact with the fuel pellet at some time in the fuel lifetime.
Cladding-pellet interaction occurs if fuel pellet temperature is increased after the cladding is in contact with the pellet.
Cladding-pellet interaction is discussed in Section 4.2.1.2.3.
Increasing fuel temperature results in an increased fuel rod internal pressure. One of
the fuel rod acceptance criteria is that the fuel rod internal pressures remain below values that can cause the fuel-cladding diametral gap to increase due to outward
cladding creep (refer to Section 4.2.1.2.1).
The potential effects of operation with waterlogged fuel were discussed in
Section 4.4.3.17, which concluded that waterlogging is not a concern during operational transients.
Clad flattening, as noted in Section 4.2.1.2.3, has been observed in some operating power reactors. Thermal expansion (axial) of the fuel rod stack against a flattened section of cladding could cause cladding failure. This is no longer a concern because clad flattening is precluded by pre-pressurization.
A differential thermal expansion between the fuel rods and the guide thimbles can occur during a transient. Excessive bowing of fuel rods can occur if the grid assemblies do
not allow axial movement of the fuel rods relative to the grids. Thermal expansion of
fuel rods is considered in the grid design so that axial loads imposed on the fuel rods
during a thermal transient will not result in excessively bowed fuel rods (refer to Section 4.2.1.3.2).
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-29 Revision 23 December 2016 4.4.3.19 Energy Release During Fuel Element Burnout As discussed in Section 4.4.3.14, the core is protected from going through DNB over the full range of possible operating conditions. At full power operation, the typical
minimum DNBR was calculated for VANTAGE+ fuel for Unit 1 and for Unit 2 and is listed in Table 4.1-1. This means that, for these conditions, the probability of a rod
going through DNB is less than 0.1 percent at 95 percent confidence level based on the
statistics of the WRB-2 correlations (References 84 and 85). In the extremely unlikely
event that DNB should occur, cladding temperature will rise due to steam blanketing the
rod surface and the consequent degradation in heat transfer. During this time a
potential for a chemical reaction between the cladding and the coolant exists. Because
of the relatively good film boiling heat transfer following DNB, the energy release from this reaction is insignificant compared to the power produced by the fuel.
These results have been confirmed in DNB tests conducted by Westinghouse (References 66 and 78).
4.4.3.20 Energy Release During Rupture of Waterlogged Fuel Elements
A full discussion of waterlogging including energy release is contained in
Section 4.4.3.17.
4.4.3.21 Fuel Rod Behavior Effects from Coolant Flow Blockage Coolant flow blockage can occur within the coolant channels of a fuel assembly or
external to the reactor core. The effect of coolant flow blockage within the fuel assembly on fuel rod behavior is more pronounced than external blockages of the same magnitude. In both cases, the flow blockages cause local reductions in coolant flow.
The amount of local flow reduction, its location in the reactor, and how far downstream
reduction persists, are considerations that influence fuel rod behavior. Coolant flow blockage effects in terms of maintaining rated core performance are determined both by
analytical and experimental methods. The experimental data are usually used to
augment analytical tools such as the THINC-IV program. Inspection of the DNB
correlation (refer to Section 4.4.3.3) shows that the predicted DNBR depends on local values of quality and mass velocity.
The THINC-IV code can predict the effects of local flow blockages on DNBR within the
fuel assembly on a subchannel basis, regardless of where the flow blockage occurs.
THINC-IV accurately predicts the flow distribution within the fuel assembly when the
inlet nozzle is completely blocked (Reference 59). For the DCPP reactors operating at
nominal full power conditions as specified in Table 4.1-1, the effects of an increase in
enthalpy and decrease in mass velocity in the lower portion of the fuel assembly would
not result in the reactor reaching the safety limit DNBR.
The analyses, which assume fully developed flow along the full channel length, show
that a reduction in local mass velocity greater than approximately 53 percent would be DCPP UNITS 1 &
2 FSAR UPDATE 4.4-30 Revision 23 December 2016 required before the safety limit DNBRs are reached. In reality, a local flow blockage is expected to promote turbulence and thus would likely not affect DNBR.
Coolant flow blockages induce local cross flows as well as promoting turbulence. Fuel
rod vibration could occur, caused by this cross flow component, through vortex
shedding or turbulent mechanisms. If the cross flow velocity exceeds the limit established for fluid elastic stabili ty, large amplitude whirling will result in, and can lead to, mechanical wear of the fuel rods at the grid support locations. The limits for a
controlled vibration mechanism are established from studies of vortex shedding and
turbulent pressure fluctuations. Fuel rod wear due to flow-induced vibration is
considered in the fuel rod fretting evaluati on (refer to Section 4.2.1.3.2.7).
4.4.4 THERMAL
AND HYDRAULIC DESIGN EVALUATION 4.4.4.1 Departure from Nucleate Boiling DNB will not occur on at least 95 percent of the limiting fuel rods during normal operation and operational transients and any transient conditions arising from faults of moderate frequency (Condition I and Conditio n II events) at a 95 percent confidence level.
This criterion has been conservatively met by adhering to the following thermal design
basis: there must be at least a 95 percent probability that the minimum DNBR of the limiting power rod during Condition I and II events is greater than or equal to the DNBR limit of the DNB correlation being used. The DNBR limit for the correlation is
established based on the variance of the cor relation such that there is a 95 percent probability with 95 percent confidence that DNB will not occur when the calculated
Historically, this DNBR limit has been 1.30 for Westinghouse applications. In this application the WRB-1 correlation (Reference 84) for LOPAR fuel and the WRB-2 correlation (Reference 85) for VANTAGE 5 fuel are employed (refer to Section 15.1.4.2). With the significant improvement in the accuracy of the CHF prediction by using these correlations instead of previous DNB correlations, a DNBR limit of 1.17 is
applicable in this application. For 17 x 17 VANTAGE+ fuel, a DNBR limit of 1.17 is applicable to thermal-hydraulic analyses performed with the WRB-2 correlation.
The design method employed to meet the DNB design basis is the ITDP (Reference 86). Uncertainties in plant operating parameters, nuclear and thermal parameters, and
fuel fabrication parameters are considered statistically such that there is at least a
95 percent probability that the minimum DNBR will be greater than or equal to 1.17 for
the limiting power rod. Plant parameter uncertainties are used to determine the plant
DNBR uncertainties. These DNBR uncertainties, combined with the DNBR limit, establish a design DNBR value, which must be met in plant safety analyses. Since the
parameter uncertainties are considered in determining the design DNBR value, the
plant safety analyses are performed using values of input parameters without DCPP UNITS 1 &
2 FSAR UPDATE 4.4-31 Revision 23 December 2016 uncertainties. Table 4.4-4 lists the Chapter 15 non-LOCA accident analyses and the applicable DNB design method.
This design procedure is illustrated in Figure 4.4-18. For this application, the minimum required DNBR design limits for the VANTAGE+ fuel analysis are 1.32 for thimble cells (three fuel rods and a thimble tube) and 1.34 for typical cells (four fuel rods).
In addition to the above considerations, a plant-specific DNBR margin has been
considered in the analyses. In particular, safety analysis DNBR limits of 1.68 for thimble cells and 1.71 for typical cells for the VANTAGE+ fuel, were employed in the safety analyses. The plant allowance available bet ween the DNBRs used in the safety analyses and the design DNBR values is not required to meet the design basis discussed earlier. This allowance is used for the flexibility in the design, operation, and analyses of DCPP.
By preventing DNB, adequate heat transfer is ensured between the fuel cladding and
the reactor coolant, thereby preventing cladding damage. Maximum fuel rod surface
temperature is not a design basis because it will be within a few degrees of coolant
temperature during operation in the nucleate boiling region. Limits provided by the
nuclear control and protection systems are such that t his design basis will be met for
transients associated with Condition II events including overpower transients. The
DNBR margin at rated power operation and during normal operating transients is
substantially larger (refer to Table 4.1-1).
4.4.4.2 Fuel Temperature During Conditions I and II events, the maximum fuel temperature shall be less than the melting temperature of UO
- 2. The UO 2 melting temperature for at least 95 percent of the peak kW/ft fuel rods will not be exceeded at the 95 percent confidence level.
The melting temperature of UO 2 is taken as 5080°F (Reference 1) unirradiated, and decreasing 58°F per 10,000 megawatt days per metric ton of uranium (MWD/MTU). By precluding UO 2 melting, the fuel geometry is preserved and possible adverse effects of molten UO 2 on the cladding are eliminated. To preclude center melting and establish overpower protection system setpoints, a calculated centerline fuel temperature of
4700°F has been selected as the overpower limit, thus providing sufficient margin for
uncertainties. The peak linear power value used in the design evaluation is 22.0 kW/ft.
This value corresponds to a peak centerline temperature which is less than 4700°F.
Fuel rod thermal evaluations are performed at rated power, maximum overpower, and
during transients at various burnups. These analyses ensure that this design basis, as
well as the fuel integrity design bases given in Section 4.2, are met. They also provide input for the evaluation of Conditions III and IV faults given in Chapter 15.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-32 Revision 23 December 2016 4.4.4.3 Core Flow A minimum of 92.5 percent (Unit 1) and 91 percent (Unit 2) of the thermal flowrate (refer to Section 5.1) will pass through the fuel rod region of the core and be effective for fuel rod cooling. Coolant flow through the thimble tubes, as well as leakage from the core barrel-baffle region into the core, is not effective for heat removal.
Core cooling evaluations are based on the thermal flowrate (minimum flow) entering the
reactor vessel. On Unit 1 the design core bypass flow is 7.5%, which accounts for thimble plugs removed, intermediate flow mixing vanes, and allowance for possible future upflow conversion. On Unit 2 the design core bypass flow is 9.0%, which accounts for thimble plugs removed, intermediate flow mixing vanes, upflow conversion and upper head temperature reduction.
4.4.4.4 Hydrodynamic Stability Operation during Condition I and Condition II events shall not lead to hydrodynamic instability.
4.4.5 SAFETY
EVALUATION 4.4.5.1 General Design Criterion 10, 1971 - Reactor Design The preceding evaluations show that the SAFDLs are not exceeded during any condition of normal operation or anticipated operational occurrence. Specifically:
- Section 4.4.4.1 shows that the DNB limits are not exceeded;
- Section 4.4.4.2 shows that the maximum fuel temperature limits are not exceeded; and
- Section 4.4.4.3 shows that the minimum core flow is met.
The above design bases, together with the fuel cladding and fuel assembly design bases given in Section 4.2.1.1, are sufficient. Fuel cladding integrity criteria cover
possible effects of cladding temperature limitations. As noted in Section 4.2.1.2.3, the fuel rod conditions change with time. A single cladding temperature limit for Conditions I or II events is not appropriate since of necessity it would be overly conservative. A
cladding temperature limit is applied to the LOCA (refer to Section 15.4.1), control rod ejection accident (Reference 2), and locked rotor accident (Reference 67).
4.4.5.2 General Design Criterion 12, 1971 - Suppression of Reactor Power Oscillations Thermo-hydrodynamic instabilities (i.e., oscillations) will not occur under Condition I and Condition II events for DCPP. A large power margin exists to predicted inception of DCPP UNITS 1 &
2 FSAR UPDATE 4.4-33 Revision 23 December 2016 such instabilities. Analyses have been performed and show that in Westinghouse reactor designs, parameters such as fuel assembly arrays, core power flow ratios, fuel assembly length, etc., do not result in gross deterioration of the above power margins (refer to Section 4.4.3.16).
4.4.6 TESTS
AND INSPECTIONS 4.4.6.1 Testing Prior to Initial Criticality Reactor coolant flow tests, as noted in Tests 3.9 and 3.10 of Table 14.1-2, are
performed following fuel loading, but prior to initial criticality. Coolant loop pressure drop data are obtained in this test. These data, in conjunction with coolant pump
performance information, allow determination of the coolant flowrates at reactor
operating conditions. This test verifies that p roper coolant flowrates have been used in the core thermal and hydraulic analysis.
4.4.6.2 Initial Power Plant Operation Core power distribution measurements are made at several core power levels (refer to Section 4.3.3.2.7) during startup and initial p ower operation. These tests are used to verify that conservative peaking factors were used in the core thermal and hydraulic
design and analysis.
4.4.6.3 Component and Fuel Inspections Inspections performed on the manufactured fuel are delineated in Section 4.2.1.6.
Fabrication measurements critical to thermal and hydraulic analysis are obtained to verify that the engineering hot channel factors employed in the design analyses (refer to Section 4.4.3.3.4) are met.
4.4.7 INSTRUMENTATION
APPLICATIONS
4.4.7.1 Incore Instrumentation Instrumentation is located in the core so that by correlating movable neutron detector
information with fixed thermocouple information the radial core characteristics may be
obtained for all core quadrants.
The incore instrumentation system is comprised of thermocouples, positioned to measure fuel assembly coolant outlet temperatures at preselected positions, and
movable fission chamber detectors positioned in guide thimbles that run the length of
selected fuel assemblies to measure the neutron flux distribution. Figures 4.4-16 and
4.4-17 show the number and location of instrumented assemblies in the core for Unit 1 and Unit 2, respectively. In the Unit 1 reacto r, four of these thermocouples have been moved to the upper head for monitoring conditions in the upper head.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-34 Revision 23 December 2016 The core exit thermocouples provide a backup for the flux monitoring instrumentation to monitor power distribution. The routine, systematic collection of thermocouple readings
provides a data base. From this data base, abnormally high or abnormally low
readings, quadrant temperature tilts, or systematic departures from a prior reference
map can be deduced.
The movable incore neutron detector system is used for more detailed mapping should
the thermocouple system indicate an abnormality. These two complementary systems
are more useful when taken together than taken alone. The incore instrumentation
system is described in more detail in Section 7.7.2.9.
Incore instrumentation is provided to obtain data from which fission power density
distribution in the core, coolant enthalpy distribution in the core, and fuel burnup
distribution may be determined.
4.4.7.2 Overtemperature and Overpower T Instrumentation
The overtemperature T trip protects the core against low DNBR. The overpower T trip protects against excessive power (fuel rod rating protection).
As discussed in Section 7.2.2.1.2, factors included in establishing the overtemperature T and overpower T trip setpoints include the reactor coolant temperature in each loop. The axial distribution of core power, as determined by the two-section (upper and
lower) excore neutron detectors, is also a factor in establishing the overtemperature T trip. 4.4.7.3 Instrumentation to Limit Maximum Power Output The output of the three ranges (source, intermediate, and power) of detectors, with the
associated nuclear instrumentation electronics, is used to limit the maximum power output of the reactor.
Eight instrument wells are located around the reactor periphery in the primary shield, 45° apart from each other, at an equal distance from the reactor vessel.
Two of the positions, on opposite flat portions of the core, directly across from the secondary neutron source positions, each contain a BF 3 proportional counter to cover the source range, and a compensated ionization chamber for the intermediate range.
The source range detector is located at an elevation of approximately one-fourth of the
core height; the compensated ionization chambers are positioned at an elevation
corresponding to one-half of the core height.
The two positions opposite the other two flat portions of the core house the post-accident neutron flux monitor detectors.
Four dual-section uncompensated ionization chamber assemblies are installed vertically in the instrumentation wells directly across from the four corners of the core. They are used as power range detectors. To minimize neutron flux pattern distortions, they are DCPP UNITS 1 &
2 FSAR UPDATE 4.4-35 Revision 23 December 2016 placed within 1 foot of the reactor vessel. Each dual-section uncompensated ionization chamber assembly provides two signals that correspond to the neutron flux in the upper and in the lower positions of a core quadrant, thus permitting the determination of
relative axial power production.
Signals from the detectors in the three ranges (source, intermediate, and power)
provide inputs which, when combined, monitor neutron flux from a completely shutdown
condition to 120 percent of full power, with th e capability of recording overpower excursions up to 200 percent of full power.
The difference in neutron flux readings between the upper and lower sections of the power range detectors is used to limit the overtemperature T and overpower T trip setpoints and to provide the operator with an indication of the core power AO. In addition, the output of the power r ange channels is used as follows:
(1) For the rod speed control function
(2) To alert the operator to an excessive power unbalance between the quadrants (3) To protect the core against rod ejection accidents (4) To protect the core against adverse power distributions resulting from dropped rods
Details of the neutron detectors and nuclear instrumentation design and the control and
trip logic are given in Chapter 7. The limits on neutron flux operation and trip setpoints are given in the Technical Specifications.
4.
4.8 REFERENCES
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DCPP UNITS 1 &
2 FSAR UPDATE 4.4-36 Revision 23 December 2016
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DCPP UNITS 1 &
2 FSAR UPDATE 4.4-37 Revision 23 December 2016
- 19. T. G. Godfrey, et al, Thermal Conductivity of Uranium Dioxide and Armco Iron by an Improved Radial Heat Flow Technique, ORNL-3556, June 1964.
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- 32. R. A. Dean, Thermal Contact Conductance Between UO 2 and Zircaloy-2, CVNA-127, May 1962.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-38 Revision 23 December 2016
- 33. A. M. Ross and R. L. Stoute, Heat Transfer Coefficient Between UO 2 and Zircacloy-2, AECL-1552, June 1962.
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- 37. F. E. Motley, et al, Critical Heat Flux Testing of 17 x 17 Fuel Assembly Geometry with 22-Inch Grid Spacing, WCAP-8536, May 1975 (Westinghouse Proprietary) and WCAP-8537, May 1975.
- 38. K.W. Hill, et al, Effect of 17 x 17 Fuel Assembly Geometry on DNB, WCAP-8296-P-A, February 1975 (Westinghouse Proprietary) and WCAP-8297-A, February 1975.
- 39. L. S. Tong, "Prediction of Departure from Nucleate Boiling for an Axially Non-Uniform Heat Flux Distribution," J. Nucl. Energy, 21, 1967, pp. 241-248.
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- 41. H. Chelemer, et al, Subchannel Thermal Analysis of Rod Bundle Core, WCAP-7015, Revision 1, January 1969.
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DCPP UNITS 1 &
2 FSAR UPDATE 4.4-39 Revision 23 December 2016
- 46. F. F. Cadek, Interchannel Thermal Mixing with Mixing Vane Grids, WCAP-7667-P-A, January 1975 (Westinghouse Proprietary), and WCAP-7755-A, January 1975.
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DCPP UNITS 1 &
2 FSAR UPDATE 4.4-40 Revision 23 December 2016
- 60. F. D. Carter, Inlet Orificing of Open PWR Cores, WCAP-9004, January 1969, (Westinghouse Proprietary), and WCAP-7836, January 1972.
- 61. J. Shefcheck, Application of the THINC Program to PWR Design, WCAP-7359-L, August 1969 (Westinghouse Proprietary), and WCAP-7838, January 1972.
- 62. E. H. Novendstern and R. O. Sandberg, Sin gle Phase Local Boiling and Bulk Boiling Pressure Drop Correlatio ns, WCAP-2850, April 1966 (Westinghouse Proprietary), and WCAP-7916, April 1966.
- 63. W. L. Owens, Jr., "Two-Phase Pressure Gradient," International Developments in Heat Transfer, Part II, ASME, New York, 1961, pp. 363-368.
- 64. A. F. McFarlane, Power Peaking Factors, WCAP-7912-P-A, January 1975 (Westinghouse Proprietary) and WCAP-7912-A, January 1975.
- 65. Deleted.
- 66. J. Weisman, et al, "Experimental Determination of the Departure from Nucleate Boiling in Large Rod Bundles at High Pressures," Chem. Eng. Prog. Symp.
Ser. 64, No. 82, 1968, pp. 114-125.
- 67. Supplemental information on fuel design transmitted from R. Salvatori, Westinghouse NES, to D. Knuth, AEC, as attachments to Letters NS-SL-518 (12/22/72), NS-SL-521 (1/4/73), NS-SL-524 (1/4/73), and NS-SL-543 (1/12/73) (Westinghouse Proprietary), and supplemental information on fuel design transmitted from R. Salvatori, Westinghouse NES, to D. Knuth, AEC, as attachments to Letters NS-SL-527 (1/4/73), and NS-SL-544 (1/12/73).
- 68. J. M. Hellman (ed), Fuel Densific ation Experimental Results and Model for Reactor Application, WCAP-8218-P-A, March 1975 (Westinghouse Proprietary) and WCAP-8219-A, March 1975.
- 69. J. A. Boure, et al, Review of Two-Phase Flow Instability, ASME Paper 71-HT-42, August 1971.
- 70. R. T. Lahey and F.J. Moody, The Thermal Hydraulics of a Boiling Water Reactor, American Nuclear Society, 1977.
- 71. M. Ishii, et al, "An Experimental Investigation of the Thermally Induced Flow Oscillations in Two-Phase Systems," J. of Heat Transfer, November 1976, pp. 616-622.
- 72. Virgil C. Summer FSAR, Docket #50-395.
- 73. Byron/Braidwood FSAR, Docket #50-456.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-41 Revision 23 December 2016
- 75. H. S. Kao, et al., "Prediction of Flow Oscillation in Reactor Core Channel," Trans. ANS. Vol. 16, 1973, pp. 212-213.
- 76. L. A. Stephan, The Effects of Cladding Material and Heat Treatment on the Response of Waterlogged UO 2 Fuel Rods to Power Bursts, IN-ITR-111, January 1970.
- 77. Western New York Nuclear Research Center Correspondence with the AEC on February 11 and August 27, 1971, Docket 50-57.
- 78. L. S. Tong, et al., Critical Heat Flux (DNB) in Square and Triangular Array Rod Bundles, presented at the Japan Society of Mechanical Engineers Semi-International Symposium held at Tokyo, Japan, September 1967, pp. 25-
- 34.
- 79. J. Skaritka, (Ed.), Fuel Rod Bow Evaluati on, WCAP-8691, Revision 1 July 1979.
- 80. "Partial Response to Request Number 1 for Additional Information on WCAP-8691, Revision 1" Letter, E. P. Rahe, Jr., (Westinghouse) to J. R. Miller (NRC), NS-EPR-2515, dated October 1981; "Remaining Response to Request Number 1 for Additional Information on WCAP-8691, Revision 1" Letter, E. P. Rahe, Jr., (Westinghouse) to J.R. Miller (NRC), NS-EPR-2572, dated March 1982.
- 81. C. G. Poncelet, LASER - A Depletion Program for Lattice Calculations Based on MUFT and THERMOS, WCAP-6073, April 1966.
- 82. Technical Specifications, Diablo Canyon Power Plant Units 1 and 2, Appendix A to License Nos. DPR-80 and DPR-82, as amended.
- 83. Deleted in Revision 23.
- 84. F. E. Motley, K. W. Hill, F. F. Cadek and J. Shefcheck, New Westinghouse Correlation WRB-1 for Predicting Critical Heat Flux in Rod Bundles with Mixing Vane Grids, WCAP-8762-P-A, July 1984 (Westinghouse Proprietary) and WCAP-8763-A, July 1984.
- 85. S. L. Davidson and W. R. Kramer, (Ed.), Reference Core Report VANTAGE 5 Fuel Assembly, WCAP-10444-P-A, September 1985 (Westinghouse Proprietary) and WCAP-10445-NP-A, September 1985.
DCPP UNITS 1 &
2 FSAR UPDATE 4.4-42 Revision 23 December 2016
- 86. H. Chelemer, L. H. Boman and D. R. Sharp, Improved Thermal Design Procedure, WCAP-8567-P-A, February 1989 Westinghouse Proprietary) and WCAP-8568-NP-A (Non-Proprietary), February 1989.
- 87. S. L. Davidson, F. E. Motley, Y. C. Lee, T. Bogard and W. J. Bryan, Verification Testing and Analyses of the 17x 17 Optimized Fuel Assembly, WCAP-9401-P-A, August 1981 (Westinghouse Proprietary) and WCAP-9402-A, August 1981.
- 88. Deleted.
- 89. S. L. Davidson, J. A. Iorii, (Ed.) Reference Core Report - 17x17 Optimized Fuel Assembly, WCAP-9500-A, May 1982.
- 90. Letter from E. P. Rahe (Westinghouse) to Miller (NRC), NS-EPR-2573, WCAP-9500 and WCAPs 9401/9402 NRC S ER Mixed Core Compatibility Items, March 1982.
- 91. Letter from C. O. Thomas (NRC) to Rahe (Westinghouse) - Supplemental Acceptance No. 2 for Referencing Topical Report, WCAP-9500, January 1983.
- 92. F. E. Motley and F. F. Cadek, DNB Test Results for R Grid Thimble Cold Wall Cells, WCAP-7695-P-A, Addendum 1, January 1975 (Westinghouse Proprietary) and WCAP-7958-A1-A, January 1975.
- 93. Deleted.
- 94. Deleted.
- 95. Deleted.
- 96. Deleted.
- 97. Deleted.
- 98. Deleted.
- 99. K. W. Hill, et al., Effect of Local Heat Flux Spikes on DNB in Non Uniformly Heated Rod Bundles, WCAP-8174-P-A, February 1975 (Westinghouse Proprietary) and WCAP-8202-A, February 1975.
100. S. L. Davidson (Ed.), et al., VANTAGE+ Fuel Assembly Reference Core Report, WCAP-12610-P-A, April 1995.
101. J.P. Foster, et al., Westinghouse Improved Performance Analysis and Design Model (PAD 4.0), WCAP-15063-P-A, Revision 1, with Errata, July 2000.
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 1 of 7 Revision 23 December 2016 REACTOR DESIGN COMPARISON Thermal and Hydraulic Design Parameters Unit 1 Unit 2 (Using ITDP)(a) Reactor Core Heat Output, MWt 3,411 3,411 Reactor Core Heat Output, 10 6 Btu/hr 11,639 11,639 Heat Generated in Fuel, %
97.4 97.4 Reactor Coolant Pressure, psia 2,250 2,250 Fuel Type Vantage+ Vantage+ Design DNBR Limit Typical Cell 1.34 1.34 Thimble Cell 1.32 1.32 Safety Analysis DNBR Limit Typical Cell 1.71 1.71 Thimble Cell 1.68 1.68 DNB Correlation WRB-2 WRB-2
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 2 of 7 Revision 23 December 2016 Unit 1 Unit 2 Vessel Minimum Measured Flow Rate (including Bypass) gpm 359,200 362,500
Vessel Thermal Design Flow (e) Rate (including Bypass) gpm 350,800 354,000
Thermal and Hydraulic Design Parameters (Based on Thermal Design Flow)
Core Flow Rate (excluding Bypass) 10 6 lbm/hr 122.3 123.4 gpm 324,490 327,450 Effective Core Flow Area for Heat Transfer, ft 2 54.13 54.13 Average Velocity along Fuel (k) Rods, ft/sec 14.0 14.2 Core Inlet Mass Velocity, 10 6 lbm/hr-ft (V-5) 2.26 2.28
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 3 of 7 Revision 23 December 2016 Unit 1 Unit 2 Nominal Vessel/Core Inlet Temperature, °F 531.7 - 544.5 531.9 -545.1 Vessel Average Temperature, °F 565.0 - 577.3 565.0 - 577.6 Core Average Temperature, °F 569.1 - 581.5 569.6 - 582.3 Vessel Outlet Temperature, °F 598.3 - 610.1 598.1 - 610.1 Average Temperature Rise in Vessel, °F 66.6 - 65.6 66.2 - 65.0 Average Temperature Rise in Core, °F 71.6 - 70.4 72.1 - 70.7 Heat Transfer Active Heat Transfer Surface Area, ft 2 57,505 57,505 Average Heat Flux, Btu/hr-ft 2 197,180 197,180 Maximum Heat Flux for Normal (h) Operation, Btu/hr-ft 2 508,720 508,720 Average Linear Power, kW/ft 5.445 5.445 Peak Linear Power for Normal Operation, (h) kW/ft 14.3 14.3 Peak Linear Power for Prevention of Centerline Melt, kW/ft 22.0 (i) 22.0 (i) Pressure Drop (j) Across Core, psi
- 25.5 + 2.6 27.2 + 2.7 Across Vessel, (n) including nozzle, psi
- 52.8 + 5.3 48.2 + 4.8 Thermal and Hydraulic Design Parameters (Fuel Rod Design)
Heat Flux Hot Channel Factor, F Q T 2.58 2.58 Temperature at Peak Linear Power for 4,700 4,700 Prevention of Centerline Melt, °F Fuel Centerline Temperature, °F Peak at 102% power
<3,360 <3,360 Peak at maximum thermal output for maximum overpower DT trip point
<3,770 <3,770
- Pressure drop values for mechanical design flow and low inlet temperatures of 531.7°F and 531.9°F for Unit 1 and Unit 2.
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 4 of 7 Revision 23 December 2016 Core Mechanical Design Parameters Unit 1 Unit 2 Fuel Assemblies Design RCC Canless RCC Canless Number of fuel assemblies 193 193 Rod array 17 X 17 17 X 17 U0 2 rods per assembly 264 264 Rod pitch, in 0.496 0.496 Overall dimensions, in 8.424 x 8.424 8.424 x 8.424 Fuel weight (as UO
- 2) lb 200,720/205,159 200,720/205,159 Zirconium alloy weight, lb 51,917 51,917 Number of grids per assembly 12 2 non-mixing vane type
6 mixing vane type
3 IFM; 1 P-Grid 12 2 non-mixing vane type
6 mixing vane type
3 IFM; 1 P-Grid Composition of grids Inconel Alloy 718 or ZIRLO Inconel Alloy 718 or ZIRLO Weight of grids, lb 1841/2820 1841/2820 Number of guide thimbles per assembly 24 24 Composition of guide thimbles ZIRLO ZIRLO Diameter of guide thimbles (ID x OD), in.
Upper part 0.442 x 0.474 0.442 x 0.474 Lower part 0.397 x 0.430 0.397 x 0.430 Diameter of instrument guide thimbles, in.
0.442 x 0.474 0.442 x 0.474 DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 5 of 7 Revision 23 December 2016 Core Mechanical Design Parameters (Cont'd)
Unit 1 Unit 2 Fuel Rods Number 50,952 50,952 Outside diameter, in 0.360 0.360 Diametral gap, in 0.0062 0.0062 Cladding thickness, in 0.0225 0.0225 Cladding material ZIRLO ZIRLO Gap material Helium Helium Fuel Pellets Material UO 2 sintered UO 2 sintered Density, % of theoretical 95 95 Diameter, in 0.3088 +/- 0.0005 0.3088 +/- 0.0005 Length, in Enriched or IFBA Pellets 0.370 +/- 0.025 0.370 +/- 0.025 Axial Blanket Pellets (refer to Section 4.2.1.2.2) 0.500 +/- 0.025 0.500 +/- 0.025 Mass of UO 2 , lb/ft of fuel rod 0.334 0.334 Rod Cluster Control Assemblies Neutron absorber, Ag-In-Cd Ag-In-Cd Composition 80%, 15%, 5% 80%, 15%, 5%
Diameter, in 0.341 +/- 0.001*
0.341 +/- 0.001* Nominal length of absorber material, in. 142 142 Density, lb/in 3 0.367 0.367 Cladding material Framatome RCCAs Ion-nitrided, cold worked, Type 316L SS Ion-nitrided, cold worked, Type 316L SS Westinghouse RCCAs Chrome Plated, cold worked, Type 304 SS Chrome Plated, cold worked, Type 304 SS Cladding thickness, in 0.0185 0.0185 Number of RCCAs 53 53 Number of absorber rods per cluster 24 24 Core Structure Core barrel, ID/OD, in 148.0/152.5 148.0/152.5 Thermal shield, ID/OD, in 158.5/164.0 Neutron pad Design
- Diameter reduced to 0.336
+/- 0.001 over bottom 12 inches.
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 6 of 7 Revision 23 December 2016 Nuclear Design Parameters Unit 1 Unit 2 Structure Characteristics Core diameter, in (equivalent) 132.7 132.7 Core average active fuel height, in.
144 144 Reflector Thickness and Composition Top - water plus steel, in.
~10 ~10 Bottom - water plus steel, in.
~10 ~10 Side - water plus steel, in
~15 ~15 H 2 O/U, cold molecular ratio lattice 2.73 2.73 Fuel Enrichment, Wt%
Maximum feed enrichment 5.0 5.0 Burnable Absorbers Type IFBA IFBA Number (typical range) 2000 - 15000 2000 - 15000
Material ZrB 2 ZrB 2 B10 Loading, mg/inch (typical) 2.25 2.25
(a) Includes the effect of fuel densification
(b) Deleted
(c) Based on T in = 545.1°F (Unit 1) and T in = 545.7°F (Unit 2) corresponding to Minimum Measured Flow of each unit
(d) Deleted
(e) Includes 0 to 10 percent steam generator tube plugging
(f) Deleted
(g) Deleted (h) This limit is associated with the value of F Q T= 2.58 (i) Refer to Section 4.3.3.2.6
(j) Based on best estimate reactor flow rate(refer to Section 5.1)
(k) At core average temperature
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-1 Sheet 7 of 7 Revision 23 December 2016 (l) Deleted (m) Deleted
(n) Deleted
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 1 of 3 Revision 23 December 2016 ANALYTICAL TECHNIQUES IN CORE DESIGN Analysis Technique Computer Code Section Referenced Mechanical Design of Core Internals Loads, deflections, and stress analysis Static and dynamic WECAN; ANSYS; MULTIFLEX 3.0; 3.7, 3.9 modeling BLODWN-2; LATFORC; WEGAP Fuel Rod Design Fuel performance characteristics Semiempirical thermal Westinghouse fuel rod 4.2.1.2.2.5 (temperature, internal pressure, model of fuel rod with design model; PAD 4.0 4.4.3.15.2 cladding stress, etc.)
consideration of fuel density changes, heat transfer, fission gas release, etc.
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 2 of 3 Revision 23 December 2016 Analysis Technique Computer Code Section Referenced Nuclear Design (1) Cross sections and group Microscopic data Modified ENDF/B library 4.3.3.10.2 constants Macroscopic constants for LEOPARD /CINDER type 4.3.3.10.2 homogenized core regions and PHOENIX-P
Group constants for control rods with self-shielding HAMMER-AIM and PHOENIX-P/ANC 4.3.3.10.2 4.3.3.10.3 (2) X-Y power distributions, fuel 2-D, 2-group diffusion TURTLE and ANC 4.3.3.10.3 depletion, critical boron theory concentrations, X-Y xenon distributions, reactivity coefficients and control rod worths (3) X-Y-Z power distributions, fuel 3-D, 2-group diffusion 3D PALADON 4.3.3.10.3 depletion, critical boron theory and ANC concentrations, X-Y-Z xenon distributions, reactivity coefficients and control rod worths (4) Axial power distributions 1-D, 2-group diffusion PANDA/APOLLO 4.3.3.10.3 and axial xenon distributions theory (5) Fuel rod power Integral transport theory LASER / 3D ANC 4.4.3.2.3 (6) Effective resonance Radial weighting REPAD / FIGHTH 4.3.3.10.1 temperature function DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.1-2 Sheet 3 of 3 Revision 23 December 2016 Analysis Technique Computer Code Section Referenced Thermal-Hydraulic Design (1) Steady state Subchannel analysis of THINC-IV 4.4.3.3 local fluid conditions in 4.4.3.5 rod bundles, including 4.4.3.10.5 inertial and crossflow 4.4.3.12 resistance terms, solution 4.4.3.13 progresses from core-wide 4.4.3.15 to hot assembly to hot 4.4.3.21 channel (2) Transient DNB analysis Subchannel analysis of THINC-III 4.4.3.15.1.3 local fluid conditions in rod bundles during transients by including accumulation terms in con-servation equations; solution progresses from core-wide to hot assembly to hot channel
DCPP UNITS 1 & 2 FSAR UPDATE Revision 12 September 1998 TABLE 4.1-3 DESIGN LOADING CONDITIONS FO R REACTOR CORE COMPONENTS (1) Fuel assembly weight (2) Fuel assembly spring forces (3) Internals weight (4) Control rod scram (equivalent static load)
(5) Differential pressure (6) Spring preloads (7) Coolant flow forces (static)
(8) Temperature gradients (9) Differences in thermal expansions (a) Due to temperature differences (b) Due to expansion of different materials (10) Interference between components (11) Vibration (mechanically or hydraulically induced) (12) One or more loops out of service (13) All operational transi ents listed in Table 5.2-4 (14) Pump overspeed (15) Seismic loads (DE and DDE)
(16) Blowdown forces (due to RCS branch line breaks)(a)
(a) In the original analysis, the blowdown forces used were those resulting from breaks in the RCS cold and hot legs. However, with the acceptance of the DCPP leak-before-break analysis by the NRC, the blowdow n forces resulting from pipe rupture events in the main reactor coolant loop pi ping no longer have to be considered in the design basis structural analyses and included in the loading combinations. Only the
much smaller forces from RCS branch line breaks have to be considered (see
Section 3.6.2.1.1.1).
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.3-1 Sheet 1 of 2 Revision 23 December 2016 NUCLEAR DESIGN PARAMETERS (Typical)
Core Average Linear Power, kW/ft, including densification effects 5.445 (a) Total Heat Flux Hot Channel Factor, F Q T 2.58 Nuclear Enthalpy Rise Hot Channel Factor,
F H N 1.65 VANTAGE+
Reactivity Coefficients
Doppler coefficient Refer to 4.3-29
Moderator temperature coefficient at operating conditions, pcm/°F (b) +5 to -40
Boron coefficient in primary coolant, pcm/ppm -16 to -8
Delayed Neutron Fraction and Lifetime eff BOL, (EOL) 0.0069, (0.0051)
l* BOL, (EOL), µsec 19.2, (18.6)
Control Rod Worths
Rod requirements Refer to Table 4.3-2
Maximum bank worth, pcm < 2000
Maximum ejected rod worth Refer to Chapter 15
DCPP UNITS 1 & 2 FSAR UPDATE TABLE 4.3-1 Sheet 2 of 2 Revision 23 December 2016 Boron Concentrations (ppm)
Refueling 2000 k eff = 0.95, cold, rod cluster control assemblies in 2000 Full power, no xenon, k eff = 1.0, hot, rod cluster control assemblies out 1876 (d)
Full power, equilibrium xenon, k eff = 1.0, hot, rod cluster control assemblies out 1536 (d)
Reduction with fuel burnup Typical reload cycle, ppm/GWD/MTU (c) Refer to Figure 4.3-3 (a) Data in table based on Unit 1 and Unit 2
(b) 1 pcm = percent mille = 10-5 where is calculated from two state point values of k eff by ln (k 2/k 1 ) (c) Gigawatt day (GWD) = 1000 megawatt days (1000 MWD)
(d) These values are representative values used for analytical purposes only.
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.3-2 UNIT 1 - REACTIVITY REQUIREMENTS FOR ROD CLUSTER CONTROL ASSEMBLIES HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED Reactivity Effects, Beginning of Life End of Life End of Life
% (First Cycle) (First Cycle) (Equilibrium Cycle)
(Typical) 1. Control Requirements Fuel temperature (Doppler) 1.39 (a) 1.12 (a) 1.00 Moderator temperature(includes void) 0.16 0.89 0.80 Redistribution 0.50 0.85 0.90 Rod insertion allowance 0.50 0.50 0.50 2. Total Control 2.55 3.36 3.20 3. Estimated Rod Cluster Control Assembly Worth (53 Rods)
All but one (highest worth) assemblies inserted 7.18 7.05 6.50 4. Estimated Rod Cluster Control Assembly-Credit with 10% adjustment to accommodate uncertainties 6.46 6.34 5.85 5. Shutdown Margin Available (Section 4.2) 3.91 2.98 2.65 (b) (a) Includes 0.1 percent uncertainty
(b) The design basis minimum shutdown margin is 1.6%
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.3-3 UNIT 2 - REACTIVITY REQUIREMENTS FOR ROD CLUSTER CONTROL ASSEMBLIES HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED Reactivity Effects, Beginning of Life End of Life End of Life
% (First Cycle) (First Cycle) (Equilibrium Cycle)
(Typical) 1. Control Requirements Fuel temperature (Doppler) 1.39 (a) 1.12 (a) 1.00 Moderator temperature (includes void) 0.29 0.96 0.94 Redistribution 0.50 0.85 0.90 Rod insertion allowance 0.50 0.50 0.50 2. Total Control 2.68 3.43 3.34 3. Estimated Rod Cluster Control Assembly Worth (53 Rods)
All but one (highest worth) assemblies inserted 6.48 6.38 5.70 4. Estimated Rod Cluster Control Assembly (Credit with 10% adjustment to accommodate uncertainties 5.83 5.74 5.13 5. Shutdown Margin Available (Section 4.2) 3.15 2.31 1.79 (b) (a) Includes 0.1% uncertainty
(b) The design basis minimum shutdown margin is 1.6%
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
TABLE 4.3-4 AXIAL STABILITY INDEX PWR CORE WITH A 12-FT HEIGHT Burnup Stability Index, hr
-1 (MWD/MTU)
F Z C B (ppm) Exp. Calc.
1550 1.34 1065
-0.041 -0.032 7700 1.27 700
-0.014 -0.006 Difference:
+0.027 +0.026
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-5 TYPICAL NEUTRON FLUX LEVELS (n/cm 2-sec) AT FULL POWER E 1 MeV 5.53 keV E 1 MeV 0.625 eV E 5.53 keV E 0.625 eV (nv) 0 Core center 6.51 x 10 13 1.12 x 10 14 8.50 x 10 13 3.00 x 10 13 Core outer radius 3.23 x 10 13 5.74 x 10 13 4.63 x 10 13 8.60 x 10 12 at midheight
Core top, on axis 1.53 x 10 13 2.42 x 10 13 2.10 x 10 13 1.63 x 10 13 Core bottom, on axis 2.36 x 10 13 3.94 x 10 13 3.50 x 10 13 1.46 x 10 13 Pressure vessel inner wall, 2.77 x 10 10 5.75 x 10 10 6.03 x 10 10 8.38 x 10 10 azimuthal peak, core midheight
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-6 COMPARISON OF MEASURED AND CALCULATED DOPPLER DEFECTS Core Burnup Measured Calculated
Plant Fuel Type (MWD/MTU) (pcm)(a) (pcm) 1 Air filled 1800 1700 1710
2 Air filled 7700 1300 1440
3 Air and 8460 1200 1210 helium filled (a) pcm = 10
-5 . See footnote in Table 4.3-1
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-7 BENCHMARK CRITICAL EXPERIMENTS Description of No. of LEOPARD k eff Using Experiments Experiments Experimental Bucklings UO 2 Al clad 14 1.0012 SS clad 19 0.9963 Borated H 2O 7 0.9989 Total 40 0.9985
U-metal Al clad 41 0.9995 Unclad 20 0.9990
Total 61 0.9993
Grand Total 101 0.9990
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-8 SAXTON CORE II ISOTOPICS ROD MY, AXIAL ZONE 6
Atom Ratio Measured 2 Precision, %
LEOPARD Calculation
U-234/U 4.65 x 10
-5 29 4.60 x 10-5 U-235/U 5.74 x 10
-3 0.9 5.73 x 10-3 U-236/U 3.55 x 10
-4 5.6 3.74 x 10-4 U-238/U 0.99386 0.01 0.99385 Pu-238/Pu 1.32 x 10
-3 2.3 1.222 x 10
-3 Pu-239/Pu 0.73971 0.03 0.74497 Pu-240/Pu 0.19302 0.2 0.19102 Pu-241/Pu 6.014 x 10
-2 0.3 5.74 x 10-2 Pu-242/Pu 5.81 x 10
-3 0.9 5.38 x 10-3 Pu/U (a) 5.938 x 10
-2 0.7 5.970 x 10
-2 Np-237/U-238 1.14 x 10
-4 15 0.86 x 10-4 Am-241/Pu-239 1.23 x 10
-2 15 1.08 x 10-2 Cm-242/Pu-239 1.05 x 10
-4 10 1.11 x 10-4 Cm-244/Pu-239 1.09 x 10
-4 20 0.98 x 10-4 (a) Weight ratio
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-9 CRITICAL BORON CONCENTRA TIONS, AT HZP, BOL
Plant Type Measured Calculated
2-loop, 121 assemblies, 10-foot core 1583 1589
2-loop, 121 assemblies, 12-foot core 1625 1624
2-loop, 121 assemblies, 12-foot core 1517 1517
3-loop, 157 assemblies, 12-foot core 1169 1161
3-loop, 157 assemblies, 12-foot core 1344 1319
4-loop, 193 assemblies, 12-foot core 1370 1355
4-loop, 193 assemblies, 12-foot core 1321 1306
DCPP UNITS 1 & 2 FSAR UPDATE Revision 11 November 1996 TABLE 4.3-10 COMPARISON OF MEASURED AND CALCULATED ROD WORTH
2-Loop Plant, 121 Assemblies, 10-foot core Measured, pcm Calculated, pcm
Group B 1885 1893 Group A 1530 1649 Shutdown group 3050 2917
ESADA Critical, 0.69-in pitch,
2 wt.% PuO 2 , 8% Pu 240 , 9 Control Rods 6.21-in rod separation 2250 2250 2.07-in rod separation 4220 4160 1.38-in rod separation 4100 4010
CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
TABLE 4.3-11 COMPARISON OF MEASURED AND CALCULATED MODERATOR TEMPERATURE COEFFICIENTS AT HZP, BOL Measured iso (a) Calculated iso Plant Type/Control Bank Configuration pcm/°F pcm/°F 3-Loop, 157 Assemblies, 12-foot core D at 160 steps
-0.50 -0.50 D in, C at 190 steps
-3.01 -2.75 D in, C at 28 steps
-7.67 -7.02 B, C, and D in
-5.16 -4.45 2-Loop, 121 Assemblies, 12-foot core D at 180 steps
+0.85 +1.02 D in, C at 180 steps
-2.40 -1.90 C and D in, B at 165 steps
-4.40 -5.58 B, C, and D in, A at 174 steps
-8.70 -8.12 (a) Isothermal coefficients, which include the Doppler effect in the fuel iso = 10 5 ln(k 2 k 1)/T(°F)
CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-1 UNIT 1 VOID FRACTIONS AT NOMINAL REACTOR CONDITIONS WITH DESIGN HOT CHANNEL FACTORS
Average Maximum Core (VANTAGE+)
0.17% --
Hot subchannel (VANTAGE+)
0.89% 2.11%
CPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-2 UNIT 2 VOID FRACTIONS AT NOMINAL REACTOR CONDITIONS WITH DESIGN HOT CHANNEL FACTORS
Average Maximum Core (VANTAGE+)
0.19% --
Hot subchannel (VANTAGE+)
3.92% 14.51%
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 HISTORICAL INFORMATION IN ITALICS BELOW NOT REQUIRED TO BE REVISED.
TABLE 4.4-3 COMPARISON OF THINC-IV AND THINC-I PREDICTIONS WITH DATA FROM REPRESENTATIVE WESTINGHOUSE TWO- AND THREE-LOOP REACTORS Improvement, °F Power, % Full Measured Inlet rms , °F , °F for THINC-IV Reactor MWt Power Temp, °F THINC-I THINC-IV over THINC-1 Ginna 847 65.1 543.7 1.97 1.83 0.14 854 65.7 544.9 1.56 1.46 0.10 857 65.9 543.9 1.97 1.82 0.15 947 72.9 543.8 1.92 1.74 0.18 961 74.0 543.7 1.97 1.79 0.18 1091 83.9 542.5 1.73 1.54 0.19 1268 97.5 542.0 2.35 2.11 0.24 1284 98.8 240.2 2.69 2.47 0.22 1284 98.9 541.0 2.42 2.17 0.25 1287 99.0 544.4 2.26 1.97 0.29 1294 99.5 540.8 2.20 1.91 0.29 1295 99.6 542.0 2.10 1.83 0.27
Robinson 1427.0 65.1 548.0 1.85 1.88 0.03 1422.6 64.9 549.4 1.39 1.39 0.00 1929.0 88.0 550.0 2.35 2.34 0.01 2207.3 100.7 534.0 2.41 2.41 0.00 2213.9 101.0 533.8 2.52 2.44 0.08
DCPP UNITS 1 & 2 FSAR UPDATE Revision 23 December 2016 TABLE 4.4-4 NON-LOCA DNB ANALYSIS METHOD UFSAR Section(s)
Event DNB Analysis Method (a) 15.2.1 RCCA Bank Withdrawal from Subcritical Non-ITDP 15.2.2 RCCA Bank Withdrawal at Power ITDP 15.2.3 RCCA Misoperation (Dropped Rod)
ITDP 15.2.4 Uncontrolled Boron Dilution Not Applicable (b) 15.2.5 Partial Loss of Flow ITDP 15.2.6 Startup of an Inactive Loop (c) Non-ITDP 15.2.7 Loss of Electrical Load / Turbine Trip ITDP 15.2.8, 15.2.9 Loss of Normal Feedwater / Loss of Offsite Power Not Applicable (Non-DNB) 15.2.10 Feedwater Malfunction (excess flow)
ITDP 15.2.11 Sudden Feedwater Temperature Reduction ITDP 15.2.12 Excessive Load Increase ITDP 15.2.13 Accidental RCS Depressurization ITDP 15.2.14 Accidental MSS Depressurization (d) Non-ITDP 15.2.15 Spurious SI Actuation at Power ITDP 15.3.4 Complete Loss of Flow ITDP 15.3.5 Single RCCA Withdrawal at Power ITDP 15.4.2.1 Rupture of a Main Steam Line (HZP)
Non-ITDP 15.4.2.2 Rupture of a Main Feedwater Pipe Not Applicable (Non-DNB) 15.4.2.3 Steam Break at Full Power ITDP 15.4.4 Locked Rotor ITDP 15.4.6 RCCA Ejection Not Applicable (Non-DNB)
(a) The DNB analysis method specified (ITDP or non-ITDP) refers to the method used to analyze for the DNB criterion. This is not applicable for cases analyzed for other acceptance criteria (e.g., peak RCS pressure) or for events that are not explicitly analyzed for DNB.
(b) For the time period from the start of dilution until reactor trip the Boron Dilution at Power case with the reactor in manual control is bounded by the DNB analysis for RCCA Bank Withdrawal at Power (refer to Section 15.2.2).
(c) Precluded by Technical Specifications; no longer analyzed.
(d) Bounded by Section 15.4.2.1; no longer analyzed.
Revision 11 November 1996 FIGURE 4.2-1 FUEL ASSEMBLY CROSS SECTION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-2 FUEL ASSEMBLY OUTLINE (LOPAR) UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-3 FUEL ROD SCHEMATIC (LOPAR) UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-4 TYPICAL CLAD AND PELLET DIMENSIONS AS A FUNCTION OF EXPOSURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-5 REPRESENTATIVE FUEL ROD INTERNAL PRESSURE AND LINEAR POWER DENSITY FOR THE LEAD BURNUP ROD AS A FUNCTION OF TIME UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.2-6 REMOVABLE ROD COMPARED TO STANDARD ROD UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE HISTORICALRevision23December2016 Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-7 REMOVABLE FUEL ROD ASSEMBLY OUTLINE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision23December2016 HISTORICAL Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-8 LOCATION OF REMOVABLE RODS WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision23December2016 HISTORICAL Revision 11 November 1996 FIGURE 4.2-9 LOWER CORE SUPPORT ASSEMBLY UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-10 LOWER CORE SUPPORT ASSEMBLY UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-11 NEUTRON SHIELD PAD LOWER CORE SUPPORT STRUCTURE UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-12 UPPER CORE SUPPORT STRUCTURE UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November Revision 11 November 1996 FIGURE 4.2-13 UPPER CORE SUPPORT STRUCTURE UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-14 PLAN VIEW OF UPPER CORE SUPPORT STRUCTURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 Revision 11 November 1996 FIGURE 4.2-15 ROD CLUSTER CONTROL AND DRIVE ROD ASSEMBLY WITH INTERFACING COMPONENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE
1.840 DIA.
NOM. (1)SPRING SPIDER BODY 0.361 DIA. (3) 0.381 DIA.
.88 TRAV.SPRING RETAINER 1.25 DIA. (2) 150.574 161.0 142.00 ABSORBER LENGTH ABSORBER 80% SILVER, 15% INDIUM, 5% CADMIUM NOTE: DIMENSIONS SHOWN FOR ALL MODELS ANNOTATED DIMENSIONS ARE WESTINGHOUSE MODEL WITH FRAMATOME MODEL HAVING THE FOLLOWING DIMENSIONS: (1) 1.804 (2) 1.240 (3) 0.354
Revision 14 November 2001 FSAR UPDATEUNITS 1 AND 2 DIABLO CANYON SITE FIGURE 4.2-16 ROD CLUSTER CONTROL ASSEMBLY OUTLINE
80% Ag, 15% In, 5% Cd 151.73 (SEE NOTE) 0.381 DIA. NOM.
NOTE: WESTINGHOUSE DIMENSION SHOWN.
FRAMATOME ROD LENGTH IS 153.658-154.468.
Revision 14 November 2001 FSAR UPDATEUNITS 1 AND 2 DIABLO CANYON SITE FIGURE 4.2-17 ABSORBER ROD Revision 11 November 1996 FIGURE 4.2-18A WET ANNULAR BURNABLE ABSORBER ROD UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-21 SECONDARY SOURCE ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.2-22 THIMBLE PLUG ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE FIGURE 4.2-23 CONTROL ROD DRIVE MECHANISM UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 20 November 2011 FIGURE 4.2-24 CONTROL ROD DRIVE MECHANISM SCHEMATIC UNITS 1 AND 2 DIABLO CANYON SITE F S AR UPDATERevision 20 November 2011 Revision 11 November 1996 FIGURE 4.2-25 NOM AL LATCH CLEARANCE AT MINIMUM AND MAXIMUM TEMPERATURE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.2-26 CONTROL ROD DRIVE MECHANISM LATCH CLEARANCE THERMAL EFFECT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-1 FUEL LOADING ARRANGEMENT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE LBVP Enhanced UFSARLBVPUFSARChangeRequestReactor,NuclearDesign Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-3 BORON CONCENTRATION VS CYCLE BURNUP WITH BURNABLE ABSORBER RODS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-4 BURNABLE ABSORBER ROD ARRANGEMENT WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-5 TYPICAL INTEGRAL FUEL BURNABLE ABSORBER ROD ARRANGEMENT WITHIN AN ASSEMBLY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-6 BURNABLE ABSORBER LOADING PATTERN UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-7 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BEGINNING OF LIFE (BOL), UNRODDED CORE, HOT FULL POWER, NO XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-8 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BOL UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-9 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BOL GROUP D AT INSERTION LIMIT, HOT FULL POWER, EQUILIBRIUM XENON UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-10 NORMALIZED POWER DENSITY DISTRIBUTION NEAR BOL GROUP D AT INSERTION LIMIT, HOT FULL POWER, EQUILIBRIUM XENON UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-11 NORMALIZED POWER DENSITY DISTRIBUTION NEAR MIDDLE OF LIFE (MOL)
UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-12 NORMALIZED POWER DENSITY DISTRIBUTION NEAR END OF LIFE (EOL)
UNRODDED CORE, HOT FULL POWER, EQUILIBRIUM XENON UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-13 RODWISE POWER DISTRIBUTION IN A TYPICAL ASSEMBLY (G-10)
NEAR BOL, HOT FULL POWER, EQUILIBRIUM XENON, UNRODDED CORE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-14 RODWISE POWER DISTRIBUTION IN A TYPICAL ASSEMBLY (G-10)
NEAR EOL, HOT FULL POWER, EQUILIBRIUM XENON, UNRODDED CORE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-15 POSSIBLE AXIAL POWER SHAPES AT BOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-16 POSSIBLE AXIAL POWER SHAPES AT MOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-17 POSSIBLE AXIAL POWER SHAPES AT EOL DUE TO ADVERSE XENON DISTRIBUTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-21 PEAK POWER DENSITY DURING CONTROL ROD MALFUNCTION OVERPOWER TRANSIENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-22 PEAK LINEAR POWER DURING BORATION / DILUTION OVERPOWER TRANSIENTS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016 Revision 11 November 1996 FIGURE 4.3-23 MAXIMUM Fx Q T POWER vs AXIAL HEIGHT DURING NORMAL OPERATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-25 COMPARISON BETWEEN CALCULATED AND MEASURED RELATIVE FUEL ASSEMBLY POWER DISTRIBUTION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-26 COMPARISON OF CALCULATED AND MEASURED AXIAL SHAPE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-27 MEASURED VALUES OF F Q T FOR FULL POWER ROD CONFIGURATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-28 DOPPLER TEMPERATURE COEFFICIENT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-29 DOPPLER ONLY POWER COEFFICIENT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-30 DOPPLER ONLY POWER DEFECT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-31 MODERATOR TEMPERATURE COEFFICIENT AT BOL, NO RODS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-32 MODERATOR TEMPERATURE COEFFICIENT AT EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-33 MODERATOR TEMPERATURE COEFFICIENT AS A FUNCTION OF BORON CONCENTRATION AT BOL, NO RODS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-34 HOT FULL POWER MODERATOR TEMPERATURE COEFFICIENT FOR CRITICAL BORON CONCENTRATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-35 TOTAL POWER COEFFICIENT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-36 TOTAL POWER DEFECT AT BOL AND EOL UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-37 ROD CLUSTER CONTROL ASSEMBLY PATTERN UNIT 1 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-38 ROD CLUSTER CONTROL ASSEMBLY PATTERN UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-39 ACCIDENTAL SIMULTANEOUS WITHDRAWAL OF TWO CONTROL BANKS EOL, HZP BANKS B AND D MOVING IN THE SAME PLANE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-40 DESIGN - TRIP CURVE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-41 NORMALIZED ROD WORTH vs.
PERCENT INSERTION, ALL RODS BUT ONE UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-42 AXIAL OFFSET vs. TIME PWR CORE WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-43 XY XENON TEST THERMOCOUPLE RESPONSE QUADRANT TILT DIFFERENCE vs. TIME UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-44 CALCULATED AND MEASURED DOPPLER DEFECT AND COEFFICIENTS AT BOL, FOR A TWO-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-45 COMPARISON OF CALCULATED AND MEASURED BORON CONCENTRATION FOR A TWO-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-46 COMPARISON OF CALCULATED AND MEASURED BORON FOR A TWO LOOP PLANT WITH A 12-FT CORE HEIGHT AND 121 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.3-47 COMPARISON OF CALCULATED AND MEASURED BORON IN A 3-LOOP PLANT WITH A 12-FT CORE HEIGHT AND 157 ASSEMBLIES UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-1 PEAK FUEL AVERAGE AND SURFACE TEMPERATURES DURING FUEL ROD LIFETIME vs. LINEAR POWER DENSITY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-2 PEAK FUEL CENTERLINE TEMPERATURE DURING FUEL ROD LIFETIME vs. LINEAR POWER DENSITY UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-3 THERMAL CONDUCTIVITY OF UO 2 (DATA CORRECTED TO 95%
THEORETICAL DENSITY)
UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-4 AXIAL VARIATION OF AVERAGE CLAD TEMPERATURE FOR ROD OPERATING AT 5.43 KW/FT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-5 PROBABILITY CURVES FOR W-3 AND R GRID DNB CORRELATIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-6 TDC vs. REYNOLDS NUMBER FOR 26-INCH GRID SPACING UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-7 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 4-FT ELEVATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-8 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 8-FT ELEVATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-9 NORMALIZED RADIAL FLOW AND ENTHALPY DISTRIBUTION AT 12-FT ELEVATION CORE EXIT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-10 VOID FRACTION vs. THERMODYNAMIC QUALITY H-HSAT/H G-HSAT UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-11 PWR NATURAL CIRCULATION TEST UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-12 COMPARISON OF A REPRESENTATIVE W TWO-LOOP REACTOR INCORE THERMOCOUPLE MEASUREMENTS WITH THINC-IV PREDICTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-13 COMPARISON OF A REPRESENTATIVE W THREE-LOOP REACTOR INCORE THERMOCOUPLE MEASUREMENTS WITH THINC-IV PREDICTIONS UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-14 HANFORD SUBCHANNEL TEMPERATURE DATA COMPARISON WITH THINC-IV UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-15 HANFORD SUBCRITICAL TEMPERATURE DATA COMPARISON WITH THINC-IV UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-16 DISTRIBUTION OF INCORE INSTRUMENTATION UNIT 1 DIABLO CANYON SITE FSAR UPDATE Error! Not a valid embedded object. Revision 11 November 1996 FIGURE 4.4-17 DISTRIBUTION OF INCORE INSTRUMENTATION UNIT 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-18 IMPROVED THERMAL DESIGN PROCEDURE ILLUSTRATION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 11 November 1996 FIGURE 4.4-19 MEASURED VERSES PREDICTED CRITICAL HEAT FLUX - WRB-1 CO ETION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE HISTORICALRevision23December2016 Revision 11 November 1996 FIGURE 4.4-20 MEASURED VERSES PREDICTED CRITICAL HEAT FLUX - WRB-2 CO ETION UNITS 1 AND 2 DIABLO CANYON SITE FSAR UPDATE Revision 23 December 2016