ML17212A045
| ML17212A045 | |
| Person / Time | |
|---|---|
| Site: | Millstone  |
| Issue date: | 06/29/2017 |
| From: | Dominion Nuclear Connecticut |
| To: | Office of Nuclear Reactor Regulation |
| Shared Package | |
| ML17212A038 | List:
|
| References | |
| 17-208 | |
| Download: ML17212A045 (196) | |
Text
Millstone Power Station Unit 2 Safety Analysis Report Chapter 4
MPS2 UFSAR CHAPTER 4-REACTOR COOLANT SYSTEM Table of Contents Section Title Page 4.1 GENERAL SYSTEM DESCRIPTION ............................................................... 4.1-1 4.2 DESIGN BASIS .................................................................................................. 4.2-1 4.2.1 Design Parameters ...................................................................................... 4.2-1 4.2.2 Codes Adhered To ...................................................................................... 4.2-4 4.2.3 Quality Control Classification .................................................................... 4.2-6 4.2.4 Part-Loop Operation ................................................................................... 4.2-6 4.3 SYSTEM COMPONENT DESIGN .................................................................... 4.3-1 4.3.1 Reactor Vessel ............................................................................................ 4.3-1 4.3.2 Steam Generator ......................................................................................... 4.3-2 4.3.2.1 Flow Induced Vibration .............................................................................. 4.3-4 4.3.2.2 Tube Thinning............................................................................................. 4.3-5 4.3.2.3 Potential Effects of Tube Ruptures ............................................................. 4.3-5 4.3.2.4 Composition of Secondary Fluid ................................................................ 4.3-6 4.3.3 Reactor Coolant Pumps .............................................................................. 4.3-6 4.3.4 Reactor Coolant Piping ............................................................................. 4.3-13 4.3.5 Pressurizer................................................................................................. 4.3-13 4.3.6 Quench Tank............................................................................................. 4.3-16 4.3.7 Valves ....................................................................................................... 4.3-17 4.3.8 Instrumentation Application ..................................................................... 4.3-23 4.3.8.1 Temperature .............................................................................................. 4.3-23 4.3.8.1.1 Hot Leg Temperature................................................................................ 4.3-23 4.3.8.1.2 Cold Leg Temperature .............................................................................. 4.3-23 4.3.8.1.3 Surge Line Temperature ........................................................................... 4.3-24 4.3.8.1.4 Pressurizer Vapor Phase Temperature ...................................................... 4.3-24 4.3.8.1.5 Pressurizer Water Phase Temperature ...................................................... 4.3-24 4.3.8.1.6 Spray Line Temperature ........................................................................... 4.3-24 4.3.8.1.7 Relief and Safety Valve Discharge Temperature ..................................... 4.3-24 4.3.8.1.8 Quench Tank Temperatures...................................................................... 4.3-24 4.3.8.1.9 Reactor Vessel Flange Seal Leakage Temperature................................... 4.3-25 4.3.8.1.10 RCS High Point Vents Leakage Temperature .......................................... 4.3-25 4.3.8.2 Pressure ..................................................................................................... 4.3-25 4.3.8.2.1 Pressurizer Pressure .................................................................................. 4.3-25 4.3.8.2.2 Pressurizer Pressure .................................................................................. 4.3-26 4.3.8.2.3 Pressurizer Pressure .................................................................................. 4.3-26 4.3.8.2.4 Quench Tank Pressure .............................................................................. 4.3-26 4.3.8.3 Level ......................................................................................................... 4.3-26 4-i Rev. 35
MPS2 UFSAR Table of Contents (Continued)
Section Title Page 4.3.8.3.1 Pressurizer Level....................................................................................... 4.3-26 4.3.8.3.2 Pressurizer Level....................................................................................... 4.3-27 4.3.8.3.3 Quench Tank Level................................................................................... 4.3-27 4.3.8.4 Reactor Coolant Loop Flow...................................................................... 4.3-27 4.3.8.5 Reactor Coolant Pump Instrumentation.................................................... 4.3-27 4.3.8.5.1 Pump Seal Temperatures .......................................................................... 4.3-27 4.3.8.5.2 Motor Stator Temperatures ....................................................................... 4.3-28 4.3.8.5.3 Motor Thrust Bearing Temperatures ........................................................ 4.3-28 4.3.8.5.4 Pump Controlled Bleed-Off Temperature ................................................ 4.3-28 4.3.8.5.5 Antireverse Device Bearing Temperature ................................................ 4.3-28 4.3.8.5.6 Upper and Lower Guide Bearing Temperature ........................................ 4.3-28 4.3.8.5.7 Lube Oil Cooler Inlet and Outlet Temperature......................................... 4.3-28 4.3.8.5.8 Lower Bearing Oil Temperature............................................................... 4.3-29 4.3.8.5.9 Pump Seal Pressures ................................................................................. 4.3-29 4.3.8.5.10 Motor Oil Lift Pressure............................................................................. 4.3-29 4.3.8.5.11 Lube Oil Filter Pressure Differential ........................................................ 4.3-29 4.3.8.5.12 Pump Controlled Bleed-Off Flow............................................................. 4.3-29 4.3.8.5.13 Lube Oil and Antireverse Device Lube Oil Flow Switch......................... 4.3-29 4.3.8.5.14 Motor Oil Reservoir Level........................................................................ 4.3-29 4.3.8.5.15 Vibration Instrumentation......................................................................... 4.3-30 4.3.8.5.16 Reverse Rotation Switch........................................................................... 4.3-30 4.3.8.5.17 (Deleted) ................................................................................................... 4.3-30 4.3.8.5.18 RCP Underspeed Reactor Trip ................................................................. 4.3-30 4.3.9 Reactor Coolant Venting System.............................................................. 4.3-30 4.3.10 Permanent Reactor Cavity Seal ................................................................ 4.3-32 4.4 MATERIALS COMPATIBILITY ...................................................................... 4.4-1 4.4.1 Materials Exposed to Coolant..................................................................... 4.4-1 4.4.2 Insulation .................................................................................................... 4.4-1 4.4.3 Coolant Chemistry ...................................................................................... 4.4-2 4.5 SYSTEM DESIGN EVALUATION ................................................................... 4.5-1 4.5.1 Prevention of Brittle Fracture ..................................................................... 4.5-1 4.5.1.1 Initial Nil-Ductility Transition Reference Temperature. ............................ 4.5-1 4.5.1.2 Nil-Ductility Transition Reference Temperature Shift ............................... 4.5-2 4.5.1.3 Operational Limits ...................................................................................... 4.5-3 4.5.1.4 Pressurized Thermal Shock ........................................................................ 4.5-5 4.5.2 Seismic Design ........................................................................................... 4.5-5 4.5.2.1 Piping .......................................................................................................... 4.5-6 4-ii Rev. 35
MPS2 UFSAR Table of Contents (Continued)
Section Title Page 4.5.2.2 Vessels ........................................................................................................ 4.5-6 4.5.2.3 Pumps and Valves....................................................................................... 4.5-7 4.5.3 Overpressure Protection.............................................................................. 4.5-8 4.5.3.1 Overpressure Protection During Normal Operation ................................... 4.5-8 4.5.3.2 Low Temperature Overpressurization Protection....................................... 4.5-8 4.5.4 Reactor Vessel Thermal Shock................................................................... 4.5-8 4.5.5 Leak Detection ............................................................................................ 4.5-9 4.5.6 Prevention of Stainless Steel Sensitization ............................................... 4.5-10 4.5.7 References................................................................................................. 4.5-15 4.6 TESTS AND INSPECTIONS ............................................................................. 4.6-1 4.6.1 General........................................................................................................ 4.6-1 4.6.2 NIL Ductility Transition Reference Temperature ...................................... 4.6-1 4.6.3 Surveillance Program.................................................................................. 4.6-4 4.6.4 Nondestructive Tests................................................................................... 4.6-6 4.6.5 Additional Tests .......................................................................................... 4.6-8 4.6.6 In-Service Inspection ................................................................................ 4.6-11 4.A SEISMIC ANALYSIS OF REACTOR COOLANT SYSTEM ......................... 4.A-1 4.A.1 INTRODUCTION ..................................................................................... 4.A-1 4.A.2 METHOD OF ANALYSIS ....................................................................... 4.A-1 4.A.2.1 General....................................................................................................... 4.A-1 4.A.2.2 Mathematical Models ................................................................................ 4.A-2 4.A.2.2.1 Reactor Coolant System - Coupled Components ...................................... 4.A-2 4.A.2.2.2 Pressurizer.................................................................................................. 4.A-3 4.A.2.2.3 Surge Line.................................................................................................. 4.A-3 4.A.2.3 Calculations ............................................................................................... 4.A-4 4.A.2.3.1 General....................................................................................................... 4.A-4 4.A.2.3.2 Frequency Analysis.................................................................................... 4.A-5 4.A.2.3.3 Mass Point Response Analysis .................................................................. 4.A-5 4.A.2.3.4 Seismic Reaction Analysis......................................................................... 4.A-6 4.A.3 RESULTS .................................................................................................. 4.A-7 4.A.4 EFFECTS OF THERMAL SHIELD REMOVAL .................................... 4.A-7 4.A.5 EFFECTS OF REPLACEMENT STEAM GENERATORS..................... 4.A-7 4.A.6 CONCLUSION.......................................................................................... 4.A-8 4.A.7 References.................................................................................................. 4.A-8 4-iii Rev. 35
MPS2 UFSAR CHAPTER 4-REACTOR COOLANT SYSTEM List of Tables Number Title 4.1-1 Reactor Coolant System Volumes 4.2-1 Principal Design Parameters of Reactor Coolant System 4.2-2A Table of Loading Combinations and Primary Stress Limits 4.2-2B Table of Loading Combinations and Primary Stress Limits for the Replacement Reactor Vessel Head and Replacement pressurizer 4.2-3 Reactor Coolant System Code Requirements 4.2-4 Comparison with Safety Guide 26 4.3-1 Reactor Vessel Parameters 4.3-2 Steam Generator Parameters 4.3-3 Main Steam Safety Valve Parameters 4.3-4 Tech Pub Review PKG for T4.3-4Reactor Coolant Pump Parameters 4.3-5 Reactor Coolant Piping Parameters 4.3-6 Pressurizer Parameters 4.3-7 Quench Tank Parameter 4.3-8 Pressurizer Spray (RC-100E, RC-100F) Valve Parameters 4.3-9 Power-Operated Relief Valve Isolation Valve Parameters (RC-403, RC-405) 4.3-10 Pressurizer Power-Operated Relief Valve Parameters (RC-402, RC-404) 4.3-11 Pressurizer Safety Valve Parameters (RC-200, RC-201) 4.3-12 Active and Inactive Valves in the Reactor Coolant System Boundary 4.4-1 Materials Exposed to Coolant 4.4-2 Reactor Coolant Chemistry 4.5-1 Reactor Coolant System Component Nozzles, Nozzle Sizes and Nozzle Materials 4.5-2 Reactor Coolant System Heatup and Cooldown Limits 4.6-1 RTNDT Determination for Reactor Vessel Base Metal Millstone Unit Number 2 4.6-2 Charpy V-notch and Drop Weight Test Values - Pressurizer Millstone Unit Number 2
4.6-3 Charpy V-notch and Drop Weight Test Values - Steam Generator 4-iv Rev. 35
MPS2 UFSAR List of Tables (Continued)
Number Title 4.6-4 Charpy V-notch Values - Piping 4.6-5 Plate and Weld Metal Chemical Analysis 4.6-6 Beltline Mechanical Test Properties - Reactor Vessel Surveillance Materials 4.6-7 Tensile Test Properties - Reactor Vessel Surveillance Materials 4.6-8 Summary of Specimens Provided for Each Exposure Location 4.6-9 Capsule Removal Schedule 4.6-10 Inspection of Reactor Coolant System Components During Fabrication and Construction 4.6-11 Reactor Coolant System Inspection C-E Requirements 4.6-12 RTPTS Values at 54 EFPY 4.6-13 Adjusted Reference Temperatures (ART) Projections 4.A-1 Natural Frequencies and Dominant Degrees of Freedom 4.A-2 Seismic Loads on Reactor Coolant System Components for Operational Basis Earthquake 4-v Rev. 35
MPS2 UFSAR NOTE: REFER TO THE CONTROLLED PLANT DRAWING FOR THE LATEST REVISION.
CHAPTER 4 - REACTOR COOLANT SYSTEM List of Figures Figure Title 4.1-1 P&ID for Reactor Coolant System & Pump (Sheet 1) 4.1-2 Reactor Coolant System Arrangement-Elevation 4.1-3 Reactor Coolant System Arrangement-Plan 4.3-1 Reactor Vessel 4.3-2 Steam Generator 4.3-3 Reactor Coolant Pump 4.3-4 P&ID Reactor Coolant Pump 4.3-5 Reactor Coolant Pump Seal Area 4.3-6 Reactor Coolant Pump Predicted Performance 4.3-7 Pressurizer 4.3-8 Temperature Control Program 4.3-9 Pressurizer Level Setpoint Program 4.3-10 Pressurizer Level Control Program 4.3-11 Quench Tank 4.3-12 Permanent Reactor Cavity Seal Plate 4.5-1 Reactor Coolant System Pressure Temperature Limitations for 7 Full Power Years 4.5-2 Reactor Coolant System Pressure - Temp Limitations During Plant Heatup/
Cooldown After 7 Years Integrated Neutron Flux 4.5-3 Reactor Coolant System Pressure Temperature Limitations For 0 to 2 Years of Full Power 4.5-4 Reactor Coolant System Heatup Limitations for 54 EFPY 4.5-5 Reactor Coolant System Cooldown Limitations for 54 EFPY 4.6-1 Location of Surveillance Capsule Assemblies 4.6-2 Typical Surveillance Capsule Assembly 4.6-3 Typical Charpy Impact Compartment Assembly 4.6-4 Typical Tensile-Monitor Compartment Assembly 4.6-5 Base Metal - WR (Transverse) Plate C-506-1 Impact Energy vs Temperature 4-vi Rev. 35
MPS2 UFSAR List of Figures (Continued)
NOTE: REFER TO THE CONTROLLED PLANT DRAWING FOR THE LATEST REVISION.
Figure Title 4.6-6 Base Metal - WR (Transverse) Plate C-506-1 Lateral Expansion versus Temperature 4.6-7 Base Metal - RW (Longitudinal) Plate C-506-1 Impact Energy versus Temperature 4.6-8 Base Metal - RW (Longitudinal) Plate C-506-1 Lateral Expansion vs Temperature 4.6-9 WELD Metal PLATE C-506-2/C-506-3 IMPACT ENERGY vs Temperature 4.6-10 Weld Metal, Plate C-506-2/C-506-3 Lateral Expansion vs Temperature 4.6-11 HAZ Metal, Plate C-506-1 Impact Energy versus Temperature 4.6-12 HAZ Metal, Plate C-506-1 Lateral Expansion versus Temperature 4.6-13 SRM (HSST Plate 01MY - Longitudinal) Impact Energy versus Temperature 4.6-14 SRM (HSST Plate 01MY - Longitudinal) Lateral Expansion versus Temperature 4.A-1 Reactor Coolant System Seismic Analysis Model MS2 4.A-1A Reactor Coolant System - Seismic Analysis Model MS2 and RV14 4.A-2 RV14 Reactor and Internals Seismic Analysis Model 4.A-3 Pressurizer Seismic Analysis Model 4.A-4 Surge Line Seismic Analysis Model 4-vii Rev. 35
MPS2 UFSAR CHAPTER 4 - REACTOR COOLANT SYSTEM 4.1 GENERAL SYSTEM DESCRIPTION The function of the reactor coolant system is to remove heat from the reactor core and internals and transfer it to the secondary (steam generating) system. The reactor coolant system, which is entirely located within the containment building, consists of two heat transfer loops connected in parallel across the reactor pressure vessel. Each loop contains one steam generator, two reactor coolant pumps, connecting piping, and flow and temperature instrumentation. Coolant system pressure is maintained by a pressurizer connected to one of the loop hot legs.
A piping and instrumentation diagram of the reactor coolant system is shown in Figure 4.1-1. The legends for the piping and instrumentation diagram are given in Figures 9.1-1, 9.1-2 and 9.1-3.
Elevation and plan views of the reactor coolant system are shown in Figure 4.1-2 and Figure 4.1-3, respectively. During operation, the four pumps circulate water through the reactor vessel where it serves as both coolant and moderator for the core. The heated water enters the two steam generators, transferring heat to the secondary (steam) system, and then returns to the pumps to repeat the cycle.
System pressure is maintained by regulating the water temperature in the pressurizer where steam and water are held in thermal equilibrium. Steam is either formed by the pressurizer heaters or condensed by the pressurizer spray to limit the pressure variations caused by the contraction or expansion of the reactor coolant. The pressurizer is located with its base at a higher elevation than the reactor coolant loop piping. This eliminates the need for a separate pressurizer drain, and ensures that the pressurizer is drained before maintenance operations.
The Reactor Coolant System (RCS) is protected against overpressure by two ASME Section III Code approved spring-loaded safety valves. In addition, two solenoid-operated power relief valves (PORVs) are provided as described in Section 4.3.7. Both the safety valves and the PORVs are connected to the top of the pressurizer. Steam discharged from the valves is cooled and condensed by water in a quench tank. In the unlikely event that the discharge exceeds the capacity of the quench tank, the tank is relieved via a rupture disc to the containment atmosphere. The rupture disc is provided as the tank code over pressure protection device. The quench tank is located at a level lower than the pressurizer. This ensures that any power-operated relief valve or pressurizer valve leakage from the pressurizer, or any discharge for these valves, drains to the quench tank.
Overpressure protection for the secondary side of the steam generators is provided by ASME Code safety valves located in the main steam line pipes upstream of the steam line isolation valves. Power-operated steam dump and bypass valves are provided to prevent opening of the secondary safety valves following a loss-of-load incident. The secondary pressure protection is described in Sections 10.3 and 4.3.2.
To maintain reactor coolant chemistry within the limits discussed in Section 4.4.3 and to control pressurizer level, a continuous but variable bleed flow from one loop upstream of the reactor coolant pump is maintained. This bleed flow is controlled by pressurizer level.
4.1-1 Rev. 35
MPS2 UFSAR Constant coolant makeup is added by charging pumps in the chemical and volume control system.
Two charging nozzles and one letdown nozzle are provided on the reactor coolant piping for these operations.
An inlet nozzle on each of the four reactor vessel inlet pipes allows injection of borated water into the reactor vessel from the safety injection system in the event emergency core cooling is needed.
During a normal plant shutdown, these nozzles are also used to supply shutdown cooling flow from the low pressure safety injection pumps. An outlet nozzle on one reactor vessel outlet pipe is used to remove shutdown cooling flow.
Vent and drain connections in the reactor coolant piping are provided for draining the reactor coolant system to the radioactive waste processing system for maintenance operations. A connection is also provided on the quench tank for draining it to the radioactive waste processing system following a relief valve or safety valve discharge. Other reactor coolant loop penetrations include sampling connections (Section 9.6) and instrument connections. The nozzle identifications are tabulated in Figure 4.1-3. Normal draining of the RCS is through the chemical and volume control system.
Where required to reduce heat losses and protect personnel from high temperatures, components and piping in the reactor coolant system are insulated with a material compatible with the temperatures involved. All insulation material used on stainless steel has a soluble chloride content of less than 600 ppm to minimize the possibility of chloride-induced stress corrosion.
Electroslag welding was not used in the construction of any reactor coolant boundary component.
The major reactor coolant system components are designed for a 40 year service life. To assure that this objective can be attained, strict quality assurance standards as outlined in Sections 4.6.4and 4.6.5 were followed.
Protection provided the reactor coolant system against environmental factors such as fires, floods and missiles is described in other sections (see Chapters 1, 5, 9 and 11).
A tabulation of the RCS volumes is contained in Table 4.1-1.
4.1-2 Rev. 35
MPS2 UFSAR TABLE 4.1-1 REACTOR COOLANT SYSTEM VOLUMES Component Volume (ft3)
Reactor Vessel 4652 Steam Generators 3386 Reactor Coolant Pumps 449 Pressurizer 1500 Piping: Hot Leg 280 Piping: Cold Leg 752 Piping: Surge Line 32 Quench Tank 217 4.1-3 Rev. 35
MPS2 UFSAR FIGURE 4.1-1 P&ID FOR REACTOR COOLANT SYSTEM & PUMP (SHEET 1)
The figure indicated above represents an engineering controlled drawing that is Incorporated by Reference in the MPS-2 FSAR. Refer to the List of Effective Figures for the related drawing number and the controlled plant drawing for the latest revision.
4.1-4 Rev. 35
MPS2 UFSAR FIGURE 4.1-1 P&ID FOR REACTOR COOLANT SYSTEM & PUMP (SHEET 2)
The figure indicated above represents an engineering controlled drawing that is Incorporated by Reference in the MPS-2 FSAR. Refer to the List of Effective Figures for the related drawing number and the controlled plant drawing for the latest revision.
4.1-5 Rev. 35
MPS2 UFSAR FIGURE 4.1-1 P&ID FOR REACTOR COOLANT SYSTEM & PUMP (SHEETS 3)
The figure indicated above represents an engineering controlled drawing that is Incorporated by Reference in the MPS-2 FSAR. Refer to the List of Effective Figures for the related drawing number and the controlled plant drawing for the latest revision.
4.1-6 Rev. 35
MPS-2 FSAR FIGURE 4.1-2 REACTOR COOLANT SYSTEM ARRANGEMENT-ELEVATION
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- 1. THIS DRAWING IS VESSEL LEVELNESS BE AND GUIDANCE O~~y USED FOR INFORMATION SEE DING. E-18767-210-2oo USED FOR DETAILED DI~~NES~~~~~S SHALL BE JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.1-3 REACTOR COOLANT SYSTEM ARRANGEMENT-PLAN 6lU- OF "'A~L
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("."'1_) Nuclear PO'Ner Station Reactor Coolant ~.ystem Arrangement-Plan Unit No. 2 4. 1-3 JUN 10 1982 Rev. 24.2
MPS2 UFSAR 4.2 DESIGN BASIS 4.2.1 DESIGN PARAMETERS The reactor coolant system operated initially at a core power level of 2560 MWt but has since been uprated to a core power level 2700 MWt. The major systems and components which bear significantly on the acceptability of the site have been evaluated for operation at a core power level of 2700 MWt (NSSS power of 2715 MWt).
The reactor design described in Chapter 3 predicates hot leg temperature, cold leg temperature, minimum reactor coolant flow and reactor vessel pressure drop. These thermodynamic and hydrodynamic data are used in the design of the steam generator, reactor coolant pump, and reactor coolant piping as described in Section 4.3 for each of these components.
The principal design parameters for the reactor coolant system are listed in Table 4.2-1. The design parameters for each of the major components are given in Section 4.3. The reactor coolant system is designated a Class 1 system for seismic design and is designed to the criteria for load combinations and stresses which are presented in Table 4.2-2A and 4.2-2B. Seismic Analysis is discussed in Appendix 4.A.
The system design temperature and pressure are conservatively established and exceed the combined normal operating value and the change due to anticipated operating transients. They include the effects of instrument error and the response characteristics of the control system. The change due to the anticipated transients also considers the effect of reactor core thermal lag, coolant transport time, system pressure drop and the characteristics of the safety and relief valves.
The following design cyclic transients, which include conservative estimates of the operational requirements for the components discussed in Section 4.3, were used in the fatigue analyses required by the applicable codes listed in Table 4.2-3; the applicable operating condition category as designated by ASME Section III is indicated in each case.
- a. Five-hundred heatup and cooldown cycles during the systems 40 year design life at a heating and cooling rate of 100°F/hr between 70°F and 532°F.
The replacement reactor vessel head is designed for 200 steady state and transient operating cycles for plant heatup and cooldown at a rate of 100°F/hr between 70°F and 532°F.
The replacement pressurizer is analyzed for 500 heatup cycles at a rate of 100°Fhour and 500 cooldown cycles at a rate of 200°F/hour.
Category: Normal Condition.
- b. Pressurizer spray piping is limited to 160 plant heatup and cooldown cycles.
Primary manway studs of the replaced steam generators are limited to 200 heatup 4.2-1 Rev. 35
MPS2 UFSAR and cooldown cycles at a heating and cooling rate of 100°F/hr between 70°F and 532°F.
- c. Fifteen-thousand power change cycles over the range of 15 percent to 100 percent of full load with a ramp load change of five percent of full load per minute increasing and decreasing.
The replacement reactor vessel closure head is analyzed to 15,000 cycles for plant loading and unloading at 5% of full load/minute.
Category: Normal Condition.
- d. Primary manway studs for the replaced steam generators are limited to 1000 cycles with a ramp load change of 5% per minute decreasing and 30% per hour increasing (plant loading/unloading).
- e. Two-thousand cycles of ten percent of full load step power changes, increasing from an initial power level of 15 and 90 percent of full power and decreasing from an initial power level between 15 and 100 percent of full power.
Category: Normal Condition.
- f. Ten cycles of hydrostatic testing the reactor coolant system at 3110 psig and a temperature at least 60°F above the Nil Ductility Transition Temperature (NDTT) of the component having the highest NDTT.
The replacement pressurizer is analyzed to 10 cycles of hydrostatic test at 3125 psia and 70°F - 400°F, above the minimum RTNDT + 60°F.
Category: Test Condition.
- g. Two-hundred cycles of leak testing at 2485 psig and at a temperature at least 60°F greater than the NDTT of the component having the highest NDTT.
Category: Test Condition; evaluated as Upset Condition.
- h. Primary manway studs for the replaced steam generators are limited to 80 cycles of leak testing at 2485 psig.
- i. 106 cycles of normal variations of +/- 100 psi and +/- 6 F at operating temperature and pressure.
The replacement pressurizer is analyzed for 106 cycles of normal variations of
+/- 100 psi and +/- 7°F at operating temperature and pressure.
4.2-2 Rev. 35
MPS2 UFSAR Category: Normal Condition.
- j. Four-hundred reactor trips from 100 percent power.
Category: Upset Condition.
- k. Primary manway studs for the replaced steam generators are limited to 80 bolt preloading cycles from unbolted state.
The manway studs for the replaced pressurizer are analyzed for 100 bolt/unbolt cycles. The vent port studs for the replaced pressurizer are analyzed for 200 bolt/
unbolt cycles.
Category: Normal Condition
- l. Primary manway studs for the replaced steam generators are limited to 1500 cycles of 10% of full load step power changes, increasing from an initial power level of 15% to 90% of full power and decreasing from initial power level between 15%
and 100% of full power.
Category: Normal Condition
- m. Primary manway studs for the replaced steam generators are limited to 200 reactor trips from 100% power.
Category: Upset Condition In addition to the above list of normal design transients, the following abnormal transients were also considered when arriving at a satisfactory usage factor as defined in Section III of the ASME Boiler and Pressure Vessel Code; however, emergency condition transients were not used to form the basis for the code design of the components based on Paragraph N-417.10(f) of ASME III, 1968 Edition, Summer 1968 addenda.
- 1. Forty cycles of loss of turbine load from 100 percent power with a delayed, reactor trip.
Category: Upset Condition.
- 2. Forty cycles of total loss of reactor coolant flow when at 100 percent power.
Category: Upset Condition.
- 3. Five cycles of complete loss of secondary system pressure.
Category: Emergency Condition.
4.2-3 Rev. 35
MPS2 UFSAR The reactor coolant system and its associated controls are designed to accommodate plant step load changes of +/- ten percent of full power and ramp changes of +/- five percent of full power per minute without reactor trip. The system will accept, without damage, a complete loss of load.
4.2.2 CODES ADHERED TO The Codes adhered to and component classifications are listed in Table 4.2-3 and conform to 10 CFR Part 50, Section 50.55a. The construction permit date was December 11, 1970; thus in all instances, code dates identified below meet or exceed those required. The impact properties of all materials which form a part of the pressure boundary meet the requirements of the ASME Boiler and Pressure Vessel Code Section III, Paragraph N330, at a temperature of 40°F. The impact properties of the replacement reactor vessel closure head and replacement pressurizer meet the requirements of ASME Section III, NB 2300.
In general, code editions and addenda in effect on the date of the original purchase order to a manufacturer apply in the design, manufacture and testing of those components. The code editions and addenda which apply for the components in Tables 1.2-1 and 4.2-3 are specified in applicable FSAR subsections.
Full compliance with Safety Guide 26 was not possible since most of the components covered by Safety Guide 26 were purchased and fabrications begun prior to the March 23, 1972, issue date for this guide. Table 4.2-4 provided a comparison of those components which are not in compliance with Safety Guide 26.
The instrument air system for Millstone Unit 2 is not required for safe shutdown. Therefore, Safety Guide 26 does not apply to the design codes for this system.
The codes and standards used for the components of the diesel oil supply are as follows:
Tanks (Above Ground) - API 650 Tanks (Below Ground) - NFPA Number 30 Piping - ANSI B31.1.0 (MOD C)
Valves - ANSI B31.1.0 (MOD C)
In addition, seismic category 1 requirements and Quality Assurance Program as outlined in Appendix 1B (located in the original FSAR dated August 1972) were employed in the manufacture.
The ANS N18.2 system of quality group classifications has been utilized by the NSSS vendor for Millstone Unit 2. The AEC has voted affirmatively for the adoption of N18.2 as an ANSI standard. It is more definitive than Safety Guide 26, is supported by the major NSSS suppliers and by the utility industry, and compliance with its provisions provides a satisfactory alternative to the Safety Guide.
4.2-4 Rev. 35
MPS2 UFSAR The following Code Cases were utilized for materials and construction of components.
ASME CODE CASES Steam Generators 1332-4 Requirements for Steel Forgings 1359-1 Ultrasonic Examination of Forgings 1335-2 Requirements for Bolting Materials 1336 Requirements for Nickel-Chromium Iron Alloy (all product forms)
N-71-13 Component Supports N-10 UT of Pressure Vessel Welds N-20 Steam Generator Tubes N-294-4 Nonwelded Components N-474-1 Inconel 690 Material Reactor Vessel 1335-2 Requirements for Bolting Materials 1336 Requirements for Nickel-Chromium Iron Alloy (all product forms) 1359-1 Ultrasonic Examination of Forgings N-4-12 Material Requirements for CEDM motor housing N-525 Material Requirements for Instrumentation Nozzles and Head Vent Nozzle Pressurizer N-405-1 Socket Welds N-2142-2 Classification UNS N06052 Filler Material ANSI B31 CODE CASES Piping 1477-1 Use of 1970 Addenda of ANSI B31.7 70 Design Criteria for Nuclear Piping Under Abnormal Conditions 74 Weld Reinforcement for B31.0 Piping 83 Weld Reinforcement for B31.7 Piping For the most severe loading combination, which includes the Design Basis Earthquake loads, the primary stresses in the ASME Code Section III, Class 2 and 3 components and component supports are limited to levels comparable to the emergency stress limits defined in ASME Code Section III for Class 1 components.
4.2-5 Rev. 35
MPS2 UFSAR 4.2.3 QUALITY CONTROL CLASSIFICATION The major components of the reactor coolant system have been placed in the safety classes as defined by ANS N 18.2 Safety Criteria for the Design of Stationary Pressurized Water Reactor Plants.
4.2.4 PART-LOOP OPERATION The maximum temperature of the hot leg and cold leg will be less than the maximum temperatures for design power at design flow. Reactor power operation with less than 4 reactor coolant pumps operating or natural circulation is not allowed. However, decay heat will be transferred to the steam generator for both cases. Current Technical Specifications restrictions prohibit other than four reactor coolant pump power operations.
The adequacy of natural circulation for decay heat removal after reactor shutdown has been verified analytically and by tests on the Palisides reactor. The core T in the analysis has been shown to be lower than the normal full power T; thus, the thermal and mechanical loads on the core structure are less severe than normal design conditions.
To assess the margin available in a post-coastdown situation, a study was made assuming termination of pump coastdown 100 seconds after reactor trip, with immediate flow decay to the stable natural circulation condition. It should be recognized that pump rotation will not have stopped for substantially longer than 100 seconds. With the maximum decay heat load 100 seconds after trip, the system will sustain stable natural circulation flow adequate to give a power to flow ratio of less than 0.9.
Heat removed from the core during natural circulation may be rejected either by dumping to the main condenser or to the atmosphere; the rate of heat removal may be controlled to maintain core T within allowable limits. The analytical techniques are verified by tests completed on the Palisades reactor (AEC Docket Number 50-225).
4.2-6 Rev. 35
MPS2 UFSAR TABLE 4.2-1 PRINCIPAL DESIGN PARAMETERS OF REACTOR COOLANT SYSTEM Design Thermal Power, (NSSS) MWt 2715, Btu/hr 9.26 x 109 Design Pressure, psig 2485 Design Temperature (Except Pressurizer, 700°F), °F 650 Design Coolant Flow Rate, gpm 325,000 (1)
Cold Leg Temperature, Normal Service, °F 550 (1)
Hot Leg Temperature, Normal Service, °F 604 (1)
Normal Operating Pressure, psia 2250 (1)
System Volume, ft3 (Without Pressurizer) 9,551 Pressurizer Water Volume, ft3 942 at 65% level Pressurizer Steam Volume, ft3 590 at 65% level (1)
RCS piping and vessel design parameters. Volumetric flow rate is based on 122 x 106 lbm/hr mass flow rate and cold leg density. See FSAR Section 14 for principal RCS parameters used in Safety Analyses.
4.2-7 Rev. 35
MPS2 UFSAR TABLE 4.2-2A TABLE OF LOADING COMBINATIONS AND PRIMARY STRESS LIMITS Primary Stress Limits Loading Combinations Vessels Piping Supports Working Stress
See Note b. PB + PL 2.25Sm See Note c. PB 1.5[1-(PM/SD)2]SD PB 4SD/ cos[PM/
2SD]
- 3. Normal Operating Loadings + Pipe PM SL PM SL Deflection of supports limited to Rupture + Maximum Hypothetical maintain supported equipment within Earthquake (DBE). limits shown in columns 1 and 2 See Notes a and b. PL + PB 3SM MPS2 UFSAR PB 1.5[1-(PM/SL)2]SL See Note c. PB 4SL/ cos[PM/
2SL]
Notes:
(a) This load combination is not applied to the piping run within which a pipe break is considered to have occurred.
(b) For loading combinations 2 and 3, stress limits for vessels, with the symbol PM changed to PL, should also be used in evaluating the effects of local loads imposed on vessels and/or piping.
(c) These stress limits are used for cylindrical structures (e.g., CRDM housings) in the vessel design.
(d) See Table 4.2-2B for replacement reactor vessel closure head loading combinations and primary stress limits.
PM = Calculated Primary Membrane Stress PB = Calculated Primary Bending Stress 4.2-8 Rev. 35
MPS2 UFSAR PL = Calculated Primary Local Membrane Stress SM = Tabulated Allowable Stress Limit at Temperature from ASME Boiler and Pressure Vessel Code,Section III or ANSI B31.7.
SY = Tabulated Yield at Temperature, ASME Boiler and Pressure Vessel Code,Section III.
SD = Design Stress SD = SY (for ferritic steels)
SD = = 1.2SM (for austenitic steels)
SL = SY + 1/3 (Su - SY)
Su = Tensile Strength of Material at Temperature The following typical values are selected to illustrate the conservatism of this approach for establishing stress limits. Units are 103 lbs/
square inch Material SY (1) SU SM (1) SP SL A-106B 25.4 60.0 (2) 17.0 25.4 36.9 SA-533B 41.4 80.0 (2) 26.7 41.4 54.3 MPS2 UFSAR SA-508, CL2 41.4 80.0 (2) 26.7 41.4 54.3 304 SS 17.0 54.0 (3) 15.3 18.4 29.3 316 SS 18.5 58.2 (3) 16.7 20.0 31.7 (1) From ASME Boiler and Pressure Vessel Code,Section III, 1968 ED., at 650°F.
(2) Minimum value at room temperature which is approximately the same at 650°F for ferritic materials.
(3) Estimated 4.2-9 Rev. 35
MPS2 UFSAR TABLE 4.2-2B TABLE OF LOADING COMBINATIONS AND PRIMARY STRESS LIMITS FOR THE REPLACEMENT REACTOR VESSEL HEAD AND REPLACEMENT PRESSURIZER Loading Combinations ASME Code Subsection Design Pm Sm NB-3221.1 Service Level A (Normal) P1 1.5Sm NB-3221.2 Service Level B (Upset) P1 + Pb 1.5Sm NB-3221.3 P1 + Pb + Q 3.0Sm NB-3222.2 Pe 3.0Sm NB-3222.3 Ui 1.0 NB-3222.4 STH y' Sy NB-3222.5 Service Level D (Faulted) Pm Lesser of 2.4Sm and 0.7Su NB-3225 Appendix F P1 1.5Pm NB-3225 Appendix F P1 + Pb 1.5Pm NB-3225 Appendix F Where:
Pm = General Primary Membrane Stress Intensity P1 = Local Membrane Stress Intensity Pb = Bending Stress Intensity Q = Secondary Stress Intensity Pe = Expansion Stress Intensity Ui = Actual Service condition cycles divided by allowable cycles, based on calculated alternating stress and fatigue design curve.
STH = Thermal Stress Range Sm = Design Stress Intensity Su = Tensile Strength Sy = Yield Stress y' = Maximum allowable range of thermal stress on an elastic basis divided by Sy.
4.2-10 Rev. 35
MPS2 UFSAR The following typical values in ksi are selected for the replacement reactor vessel head materials at 650°F.
Material Sy Su Sm SA508 Grade 3 Class 1 41.5 80.0 26.7 ASME Section II, Part D SB 167 (Alloy 690) 20 80 20.0 ASME Code Case N525/Section II, Part D SB 166 (Alloy 690) 27.5 80.0 23.3 ASME Section II, Part D SA 182 F316LN 17.8 62.8 16.0 ASME Section II, Part D SA 312 TP316L 15.3 61.7 13.8 ASME Section II, Part D The following typical values in ksi are selected for the pressurizer materials at 650°F.
Material Sy Su Sm SA508 Grade 3 Class 2 53.9 90.0 30 ASME Section II, Part D SA 182 Grade F 316 18.5 67.0 16.7 ASME Section II, Part D 4.2-11 Rev. 35
MPS2 UFSAR TABLE 4.2-3 REACTOR COOLANT SYSTEM CODE REQUIREMENTS Components Codes Reactor Vessel (excluding replacement 1. ASME,Section III, Class A, 1968 Edition, Reactor Vessel Closure Head and Addenda through Summer 1969 Nozzles), Original Upper Shell of Steam Generator Replacement Reactor Vessel Closure 1. ASME Section III, 1998 Edition through 2000 Head and Nozzles, Replacement Addenda.
Pressurizer Replacement Lower Steam Generator 1. ASME,Section III, Class I, 1983 Edition, Addendum to Summer of 1984 Reactor Coolant Pumps 1. Draft ASME Code for Pumps and Valves for Nuclear Power, Class 1, November 1968, including March 1970 Addenda.
- 2. ASME Section III, paragraph N153 in Summer 1969 Addenda.
- 3. ASME Section III, Appendix IX.
Quench Tank ASME Section III, Class C, 1968 Pressurizer Safety Valves 1. ASME Section III, Class A, 1968 Edition, Addenda through Summer of 1970, Code Case 1344-1 Piping 1. ANSI B31.7, Class 1, 1969 Edition.
- 2. ASME Section III, paragraph N153 in Summer 1969 Addenda.
- 3. Code Case 70 to B31.7.
Secondary Safety Valves ASME Standard Code for Pumps and Valves for Nuclear Power, Class 2, March, 1970 Draft Note: The spare and original safety valves are used interchangeably. Refurbishment and retesting of the safety valves are performed periodically and the safety valves (spare and/or original) are then installed into the system rotationally.
4.2-12 Rev. 35
MPS2 UFSAR TABLE 4.2-4 COMPARISON WITH SAFETY GUIDE 26 Requirements Imposed In Classification Per Applicable Code Code Used In Addition to Code Requirements System Components Safety Guide 26 Per Safety Guide 26 Manufacture Used in Manufacture Reactor Building Pressure Quality Group C ASME Section III, ASME Section VIII Seismic Category I, manufactured Closed Cooling Vessels Class 3 Division I under Quality Assurance Program Water System of Appendix 1B (a), Spot radiographed Piping Quality Group C ASME Section III, ANSI B31.1.0 MOD Seismic Category I, 10% random (excluding Class 3 B radiography of butt welds for Containment piping 4 inch and larger, material Penetrations) identification, manufactured under Quality Assurance Program of Appendix 1B (a)
Pumps Quality Group C ASME Section III, Standards of the All pressure containing parts Class 3 Hydraulic Institute where hydrostatically tested at a minimum of 1.5 times the design MPS2 UFSAR pressure seismic I manufactured under Quality Assurance Program of Appendix 1B (a)
Valves Quality Group C ASME Section III, ANSI B31.1.0 MOD Seismic Category I, MT-PT (excluding Class 3 B Examination, material traceability Containment) on pressure retaining parts, manufactured under Quality Assurance Program of Appendix 1B (a) 4.2-13 Rev. 35
MPS2 UFSAR TABLE 4.2-4 COMPARISON WITH SAFETY GUIDE 26 (CONTINUED)
Requirements Imposed In Classification Per Applicable Code Code Used In Addition to Code Requirements System Components Safety Guide 26 Per Safety Guide 26 Manufacture Used in Manufacture Safety Injection Shutdown Quality Group C ASME Section III, ASME Section III, Seismic Category I System Heat Class 2 Class 3, TEMA R Exchangers Refueling Quality Group B ASME Section III, ASME Section III, Seismic Category I, manufactured Water Tank Class 2 Class 3 under Quality Assurance Program of Appendix 1B (a)
Piping Quality Group B ASME Section III ANSI B31.1.0 Seismic Category I, Material HCD(C) MOD(C) Identification per ASTM Specification Pumps Quality Group B ASME Section III, ASME Code for Seismic Category I, manufactured Class 2 Pumps and Valves under Quality Assurance Program for Nuclear Power, of Appendix 1B (a) (See Question Class II 4.4) MPS2 UFSAR Valves Quality Group B ASME Section III, ANSI B31.1.0 Seismic Category I, Material HCD(C) Only Class 2 MOD(C) Identification per ASTM Specification Piping 4 inch Quality Group B ASME Section III, ANSI B31.1.0 Seismic Category I HCD-3 and 6 Class 2 inch HCD-3 4.2-14 Rev. 35
MPS2 UFSAR TABLE 4.2-4 COMPARISON WITH SAFETY GUIDE 26 (CONTINUED)
Requirements Imposed In Classification Per Applicable Code Code Used In Addition to Code Requirements System Components Safety Guide 26 Per Safety Guide 26 Manufacture Used in Manufacture Auxiliary Feedwater Condensate Quality Group B ASME Section III, AWWA D100 NFPA Seismic Category I, manufactured System Storage Tank Class 2 Volume 6 under Quality Assurance Program of Appendix 1B (a) later modified to API 620 or equivalent based on Design Change to a pressurized tank Piping Quality Group B ASME Section III, ANSI B31.1.0 MOD Seismic Category I, 10% random (excluding Class 2 B radiography of butt welds for Containment piping 4 inch and larger, material Penetrations) identification manufactured under Quality Assurance Program of Appendix 1B Pumps Quality Group B ASME Section III, ASME Code for Seismic Category I manufactured Class 2 Pumps and Valves under Quality Assurance Program MPS2 UFSAR for Nuclear Power, of Appendix 1B (a)
Class II Valves Quality Group B ASME Section III, ASNE B31.1.0 Seismic Category I, MT-PT (excluding Class 3 MOD B Examination, material traceability Containment on pressure retaining parts, Isolation) manufactured under Quality Assurance Program of Appendix 1B (a) 4.2-15 Rev. 35
MPS2 UFSAR TABLE 4.2-4 COMPARISON WITH SAFETY GUIDE 26 (CONTINUED)
Requirements Imposed In Classification Per Applicable Code Code Used In Addition to Code Requirements System Components Safety Guide 26 Per Safety Guide 26 Manufacture Used in Manufacture Service Water Piping Quality Group C ASME Section III, ANSI B31.1.0 Seismic Category I, manufactured System Class 3 under Quality Assurance Program of Appendix 1B (a)
Pumps Quality Group C, ASME Section III ASME Section VIII Perform Test according to ASME Class 3 PTC 8.2 1965, Seismic Category I manufactured under Quality Assurance Program of Appendix 1B (a)
Valves Quality Group C ASME Section III, ANSI B31.1.0 Seismic Category I, manufactured Class 3 under Quality Assurance Program of Appendix 1B (a)
Vital Chilled Water Piping Quality Group C ASME Section III, ANSI B31.1.0 Seismic Category I, manufactured System Class 3 under Quality Assurance Program MPS2 UFSAR of Appendix 1B (a)
Valves Quality Group C ASME Section III, ANSI B31.1.0 Seismic Category I, manufactured Class 3 under Quality Assurance Program of Appendix 1B (a)
Condenser/ Quality Group C ASME Section III, ASME Section VIII, Seismic Category I, manufactured Evaporators Class 3 Division I under Quality Assurance Program of Appendix 1B (a)
(a)Appendix 1B was located in the original FSAR dated August 15, 1972.
4.2-16 Rev. 35
MPS2 UFSAR 4.3 SYSTEM COMPONENT DESIGN 4.3.1 REACTOR VESSEL The reactor vessel (Figure 4.3-1) is supported by three pads welded to the underside of the reactor vessel nozzles. The arrangement of the vessel supports, allows radial growth of the reactor vessel due to thermal expansion while maintaining it centered and restrained from movement caused by seismic disturbances. Departure from levelness of not more than 0.002 inch per foot of flange diameter is maintained during construction to facilitate proper assembly of reactor internals. The design parameters for the reactor vessel are given in Table 4.3-1.
The vessel closure flange is a forged ring with a machined ledge on the inside surface to support the reactor internals and core. No other ring forgings are used for reactor vessel shell sections. The flange is drilled and tapped to receive the closure studs and is machined to provide a mating surface for the reactor vessel closure seal. The vessel closure contains 54 studs, 7 inches in diameter, with eight threads per inch. The stud material is ASTM A-540, Grade B24, with a minimum yield strength of 130,000 psi. The tensile stress in each stud when elongated for operational conditions is approximately 40 ksi. Calculations show that 32 uniformly distributed studs can fail before the closure will separate at design pressure. However, 16 uniformly distributed broken studs or four adjacent broken studs will cause O-ring leakage.
Six radial nozzles on a common plane are located just below the vessel closure flange. Extra thickness in this vessel-nozzle course provides most of the reinforcement required for the nozzles.
Additional reinforcement is provided for the individual nozzle attachments. A boss located around each outlet nozzle on the inside diameter of the vessel wall provides a mating surface for the internal structure which guides the outlet coolant flow. This boss and the outlet sleeve on the core support barrel are machined to a common contour to reduce core bypass leakage. A fixed hemispherical head is attached to the lower end of the shell. There are no penetrations in the lower head.
The removal top closure head is hemispherical. The closure head is single piece low alloy steel forging replaced during refueling outage 16. All surfaces in contact with reactor coolant are clad with a quarter inch nominal thickness weld deposit similar to type 304 stainless steel. The nozzles in the reactor vessel head support the Control Element Drive Mechanisms (CEDMs). The CEDM, In-Core Instrumentation (ICI) and vent nozzles are constructed from Inconel alloy 690 material to minimize the susceptibility to Primary Water Stress Corrosion Cracking. Threaded housing flanges made of stainless steel are joined to the guide tubes by Gas Tungsten Arc Welding. The head flange is drilled to match the vessel flange stud bolt locations. The 54 stud bolts are fitted with spherical washers located between the closure nuts and head flange to maintain stud alignment during head flexing due to boltup. To ensure uniform loading of the closure seal, the studs are tensioned with hydraulic stud tensioners. Stud elongation is then measured to ensure proper preload on all the studs.
Flange sealing is accomplished by a double-seal arrangement utilizing two silver-plated Ni-Cr-Fe alloy, self-energized O-rings. The space between the two rings is monitored to allow detection of any inner ring leakage. The control element drive mechanism (CEDM) nozzles (Ni-Cr-Fe alloy 4.3-1 Rev. 35
MPS2 UFSAR through the head, stainless steel flange) terminate with threaded and seal-welded flanges at the upper end. There are eight instrumentation nozzles with Grayloc connectors to maintain pressure boundary. In addition to these nozzles, there is a three-quarter inch vent connection.
The core is supported from an internally machined core support ledge.
4.3.2 STEAM GENERATOR The nuclear steam supply system (NSSS) utilizes two steam generators (Figure 4.3-2) to transfer the heat generated in the reactor coolant system (RCS) to the secondary system and produce steam at the warranted steam pressure and quality. The design parameters for the steam generators are given in Table 4.3-2.
The steam generator is a vertical U-tube heat exchanger. The steam generator operates with the reactor coolant in the tube side and the secondary fluid in the shell side.
Reactor coolant enters the steam generator through the inlet nozzle, flows through three-quarter inch OD U-tubes, and leaves through two outlet nozzles. Vertical partition plates in the lower head separate the inlet and outlet plenums. The plenums are stainless steel clad, while the primary side of the tube sheet is Ni-Cr-Fe clad. The vertical U-tubes are Ni-Cr-Fe alloy. The tube-to-tube sheet joint is welded on the primary side.
Feedwater enters the steam generator through the feedwater nozzle where it is distributed via a feedwater distribution ring having top discharge J nozzles which direct the flow into the downcomer. The downcomer is an annular passage formed by the inner surface of the steam generator shell and the cylindrical shell wrapper which encloses the vertical U-tubes.
At the bottom of the downcomer, the secondary water is directed upward past the vertical U-tubes where it is boiled to produce steam in the evaporator. The heat transfer area is determined by the required heat transfer, the thermal driving force and the heat transfer coefficient. The heat transfer coefficient in the evaporator is calculated from experimental data.
Upon exiting from the vertical U-tube heat transfer surface, the steam water mixture enters centrifugal-type separators. These impart a centrifugal motion to the mixture and separate the steam from the water. The water leaves the primary separator through the bottom of the separator housing and is directed into the downcomer where it is mixed with the feedwater. Final drying of the steam from the centrifugal primary separators is accomplished by directing the steam through secondary cyclones. The moisture content of the outlet steam is no greater than 0.2 percent at design flow.
The steam generator primary side pressure loss is determined by summing the losses due to friction in the tubes, in the tube bends, entrances and exits, and the steam generator inlet and outlet plenums and nozzles.
The steam generator shell is constructed of carbon steel. Manways and handholes are provided for easy access to the steam generator internals.
4.3-2 Rev. 35
MPS2 UFSAR The power-operated steam dump valves and steam bypass valves obviate opening of the main steam safety valves following turbine and reactor trip from full power. The steam dump and bypass system is described in Section 10.
Overpressure protection for the shell side of the steam generators and the main steam line piping up to the inlet of the turbine stop valve and provided by 16 spring-loaded ASME Code safety valves which discharge to atmosphere. Eight of these safety valves are mounted on each of the main steam lines outside the containment upstream of the steam lined isolation valves. The opening pressure of the valves is set in accordance with ASME Code allowances. Parameters for the main steam safety valves are given in Table 4.3-3.
Instrumentation has been added to each safety relief valve (SRV) to provide a main control board annunciator alarm indication of valve closed/not closed, (Regulatory Guide 1.97, Rev. 2, D-18 variable).
The main control board annunciator window (C05 D17A/B) is a split window and will alarm when any of the SRV's on Steam Generator 1 or 2, respectively, are not closed.
Upon receiving this alarm, the operator would use the control room alarm typer or the control room cathode ray tube (CRT) display showing the SRV graphics, to determine which valve on Steam Generator 1 or 2 is not closed.
The steam generators are vertically mounted on bearing plates which allow lateral motion due to thermal expansion of the reactor coolant piping. Stops are provided to limit this motion in case of a coolant pipe rupture.
The top of each unit is restrained from sudden lateral movement by suitable stops and hydraulic snubbers mounted rigidly to the concrete structure.
In addition to the transients listed in Section 4.2.1, each steam generator is also designed for the following conditions such that no component is stressed beyond the allowable limit as described in ASME Code,Section III (Table 4.3-2):
- a. Four-thousand cycles of transient pressure differentials of 85 psi across the primary head divider plate due to starting and stopping the primary coolant pumps (RCP).
Category: Normal Condition.
- b. Ten cycles of hydrostatic testing of the secondary side at 1235 psig, the primary side is at atmospheric pressure.
Category: Test Condition.
4.3-3 Rev. 35
MPS2 UFSAR
- c. Two-hundred cycles of leak testing of the secondary side at 985 psig, the primary side will be pressurized to 165 psig.
Category: Test Condition.
- d. Fifteen-thousand cycles of adding 600 gpm of 70°F feedwater with the plant in hot standby condition.
Category: Normal Condition.
In addition to the normal design transients listed above, and those listed in Section 4.2.2, the following additional abnormal transient was also considered in arriving at a satisfactory usage factor as defined in Section III of the ASME Code:
Eight cycles of adding a maximum of 650 gpm of 70°F feedwater with the steam generator secondary side dry and at 620°F.
Category: Emergency Condition.
The unit is capable of withstanding these conditions for the prescribed numbers of cycles in addition to the prescribed operating conditions without exceeding the allowable cumulative usage factor as prescribed in ASME Code,Section III.
The steam generators are located at a higher elevation than the reactor vessel. The elevation difference creates natural circulation sufficient to remove core decay heat following coastdown of all RCPs.
The steam generators are equipped with a nitrogen addition system which has the capability of admitting N2 to the bottom blowdown headers to mix the chemicals in the steam generators during wet layup, and also through nozzles in the transition cones for blanketing the steam generators and steam lines above the water level. A flowmeter provides nitrogen flow control and visual verification that flow is occurring. A drain line on the steam generator upper vent line allows checking that the steam generator has not been flooded. A test gauge may be installed on this line to measure steam generator overpressure.
In addition to the transients listed in this section, and those in Section 4.2.1 the following factors were considered in the design of the steam generators.
4.3.2.1 Flow Induced Vibration The steam generator has also been designed to ensure that critical vibration frequencies will be well out of the range expected during normal operation and during abnormal conditions. The steam generator tubing, tube sleeves, and tubing supports are designed and fabricated with considerations given to both secondary side flow induced vibrations and RCP induced vibrations.
In addition, the heat transfer tubing, tube sleeves, and tube supports are designed so that they will 4.3-4 Rev. 35
MPS2 UFSAR not be structurally damaged under the loss of secondary pressure conditions that may produce a fluid velocity in the tube bundle four times design velocity.
Because the RCPs have a rotational speed of 900 rpm (less normal slip) the tube bundle design has considered the imposition of exciting frequencies of 14 to 15 cps and 70 and 75 cps. The lower frequency range is defined as a mechanical vibration resulting from the transmission of a mechanical impulse at the frequency of pump rotation. The upper frequency range is defined to be a sinusoidal pressure variation of +/-6 psi in the primary piping that contains the pump. The pressure variation results from the impeller vanes interacting with the cutwater vane at the volute outlet during each revolution of the impeller.
It has been found that all tubes and tube sections that will experience forcing functions from cross flow and parallel flow have natural frequencies sufficiently different from the frequency of the forcing function that they will not experience damaging vibrations. The mechanical excitation frequency is sufficiently different from the lowest natural frequency for out-of-plane or lateral vibration in any tube span that critical vibration will not occur.
4.3.2.2 Tube Thinning The original Combustion Engineering (CE) Steam Generators margin of tube-wall thinning that could be tolerated without exceeding the allowable faulted stress limits under postulated condition of a design basis largest pipe break in the reactor coolant pressure boundary (RCPB) during reactor operation was 0.008 inches.
0.0012 inch excess material had been intentionally been provided in the tube wall thickness to accommodate the estimated degradation of tubes during the service lifetime. CE expected negligible tube wall thinning when operating under the specified secondary chemistry requirements.
Because of the use of volatile secondary water chemistry there has been no tube wall thinning experienced on the steam generators. The new steam generator tubes are designed to be at least structurally equivalent to the original and in compliance to Regulatory Guide 1.121. Therefore, tube wall thinning or other forms of tube degradation can be structurally accommodated with the same degree of margin as the original.
4.3.2.3 Potential Effects of Tube Ruptures The steam generator tube rupture accident in a penetration of the barrier between the RCS and the main steam system. The integrity of this barrier is significant from the standpoint of radiological safety in that a leaking steam generator tube allows the transfer of reactor coolant into the main steam system. Radioactivity contained in the reactor coolant would mix with water in the shell side of the affected steam generator. This radioactivity would be transported by steam to the turbine and then to the condenser, or directly to the condenser via the main steam dump and bypass system. Noncondensible radioactive gases in the condenser are removed by the condenser air ejector system and discharged to the plant vent. Analysis of a steam generator tube rupture accident, assuming complete severance of a tube, is presented in Section 14.14.
4.3-5 Rev. 35
MPS2 UFSAR 4.3.2.4 Composition of Secondary Fluid Radioactivity concentrations in the secondary side of the steam generator is dependent upon the radioactive concentration of the RCS, the primary to secondary leak rate, and the operating history of the steam generator blowdown system.
4.3.3 REACTOR COOLANT PUMPS The reactor coolant is circulated by four single speed, vertical, single suction, centrifugal type pumps (Figure 4.3-3). The discharge nozzle is horizontal and the suction nozzle is in the bottom vertical position. The pressure containing components are designed and fabricated in accordance with the ASME Boiler and Pressure Vessel Code,Section III, Class A.
The design flow for the RCP is determined from the reactor mass flow. This mass flow is converted to volumetric flow at the full power cold inlet temperature to determine the pump design flow. The maximum pressure loss at the design flow rate for the reactor vessel, steam generator, and piping is determined by adding an allowance for uncertainty to the best estimate for each pressure drop. These maximum values are used to establish the RCP design head. The RCP is designed to produce the minimum reactor design flow at the maximum expected system pressure loss.
The minimum RCS pressure at any given temperature is limited by required net positive suction head (NPSH) for the RCP during portions of plant heatup and cooldown. To ensure that the pump NPSH requirements are met under all operating conditions, an operating curve is used which gives permissible RCS pressure as a function of reactor coolant temperature. The RCP NPSH restriction on this curve is determined by using the NPSH requirement for each pump combination and correcting it for pressure and temperature instrument errors and pressure measurement location. The NPSH required versus pump flow is supplied by the pump vendor.
Plant operation below this curve is prohibited. At low RCS temperatures and pressures, other considerations require the maximum pressure versus temperature curve to be above the NPSH curve.
The pump impeller is pinned and bolted to the shaft. A close clearance thermal barrier assembly is mounted above the water lubricated bearing to retard heat flow from the pump to the seal cavity which is located above the thermal barrier. The thermal barrier assembly also tends to isolate the hot fluid in the pump from the cooler fluid above and, in the event of a seal failure, serves as an additional barrier to reduce leakage from the pump. Each pump is equipped with replaceable casing wear rings. A water lubricated bearing is located in the fluid between the impeller and thermal barrier to provide shaft support. Additional shaft support is provided by bearings in the electric motor which is directly connected to the pump shaft by a rigid coupling.
The shaft seal assembly located above the thermal barrier consists of four, face type mechanical seals, three full-pressure seals mounted in tandem and a fourth low pressure backup vapor seal designed to withstand operating system pressure with the pump stopped. The performance of the shaft seal system is monitored by pressure and temperature sensing devices in the seal system (Figure 4.3-4). A controlled bleed off flow through the pump seals is maintained to cool the seals 4.3-6 Rev. 35
MPS2 UFSAR and to equalize the pressure drop across each seal. The controlled bleed-off flow is collected and processed by the chemical and volume control system. Any minor leakage past the vapor seal (the last mechanical seal), is drained to the containment sump via the containment trench and collected in the radioactive waste processing system. Normal vapor seal leakage is minor, (approximately 0 to.08 GPM per RCP), and is considered to be negligible leakage to the containment atmosphere.
The seals are cooled by circulating the controlled bleed off through the heat exchanger mounted integrally within the pump cover assembly. No damage would result in the event of pump operation without cooling water for up to five minutes. To reduce plant downtime and personnel exposure to radiation during seal maintenance, the seal system is contained in a cartridge which can be removed and replaced as a unit. The seal cartridge can be replaced without draining the pump casing. The seal detail is shown in Figure 4.3-5.
A motor-mounted flywheel reduces the rate of flow decay upon loss of pump power. The combined inertia of the pump motor and flywheel is 100,000 lbm-ft2. Flow coastdown characteristics are discussed in Section 14.6.
The RCPs are typical centrifugal volumetric flow machines. The pump response following a Loss-of-Coolant Accident (LOCA) is predicted using generally accepted methods as described in Appendix 1 of CENPD-26. CENPD-26 is a proprietary report entitled Combustion Engineering Analytical Techniques for Evaluating Loss of Coolant Accidents. A spectrum of breaks in the RCP discharge line have been analyzed and the results follow a predictable pattern. Assuming loss of electrical power to the pump at the start of the LOCA, it is seen that the pumps initially lose speed because the volumetric flow through the pump is not sufficient to sustain the nominal speed of rotation. The volumetric flow increases during the transient, accelerating the pump to its maximum speed. The extent of the initial loss of speed varies with the break size. The larger the break size, the less the initial deceleration and the higher the maximum speed attained. The pump attains its maximum speed following a double-ended discharge break. The calculated torque imposed on the impeller follows the same trend as the speed, with the maximum value occurring following the double-ended discharge break.
The need for a disengaging device to prevent motor overspeed following a LOCA has been evaluated. In view of the fact that the maximum anticipated pump speed is well within the safe operating limits for all rotating parts, a means to disengage the motor from the pump is not necessary.
A break in the suction piping causes the reactor coolant to flow through the pump opposite to the normal direction of flow, decelerating the rotation of the pump until it is brought to rest against the anti-reverse rotation device.
The pump/motor assembly includes motor bearing oil coolers, seal chamber, controls and instruments. Cooling water is provided from the reactor building closed cooling water (RBCCW) system. The design parameters for the RCPs are given in Table 4.3-4. The RCP instrumentation is described in Section 4.3.8.5.
The RCP and motor are supported by four support lugs welded to the volute. The pump is supported by four spring assemblies employed between the support lugs and the floor below.
4.3-7 Rev. 35
MPS2 UFSAR Movement in the horizontal plane to compensate for pipe thermal growth and contraction is permitted. Vertical movement is not restrained.
The major pump components wetted by the primary fluid are constructed of austenitic stainless steel to minimize corrosion. These materials are listed in Table 4.3-4. The mechanical seals consist of a rotating tungsten (1) carbide ring riding over a hard carbon face. The design life of this seal arrangement is at least 50,000 hours0 days <br />0 hours <br />0 weeks <br />0 months <br /> or 5.7 years. Each seal is designed to accept a pressure drop equal to full operating system pressure, but normally operates at one-third this pressure drop.
The predicted pump performance curve is shown in Figure 4.3-6. The air-cooled, self-ventilated pump motor is sized for continuous operation at the flows resulting from four-pump operation or partial pump operation with 0.76 specific gravity water. The motor service factor is sufficient to allow 500 heatup cycles during which the nominal horsepower load will decrease from 6000 to 4500 over a period of seven hours. The motors are designed to start and accelerate to rated speed under full load when 70 percent or more of rated normal voltage is applied. The motors are contained within standard drip-proof enclosures and are equipped with electrical insulation suitable for a zero to 100 percent humidity and radiation environment of 30 R/hr.
The design requirements of the RCPs include a minimum inertia for the rotating assembly of 100,000 lbm - ft2; to achieve this total, a flywheel with an inertia of 70,000 lbm - ft2 has been incorporated.
Each original RCP motor flywheel assembly consists of two solid discs bolted together, shrink fitted onto and keyed to the shaft above the rotor. The dimensions of each disc are:
Outside diameter, inches 75 Thickness, inches 6 Weight, each, lb 7,250 The selection of material, machining and manufacturing operations, quality control, and the rigorous acceptance criteria established to assure the integrity of the flywheel and to minimize operating stresses include the following:
A. The principal stress is 30 percent of the yield point of the flywheel material (based on the tensile tests per ASTM-A-20) at the design overspeed of 125% of the normal operating speed not considering keyway stress concentration factors. The minimum keyway fillet radius is one eight inch.
B. The bore in the flywheel was flame cut, with a minimum of one half inch of stock left on the radius for machining to final dimensions.
C. All flywheel discs have passed the following nondestructive testing:
(1) or silicon 4.3-8 Rev. 35
MPS2 UFSAR
- 1. Testing by steel vendor prior to machining
- a. One-hundred percent Ultrasonic Inspection per ASME Code,Section III, paragraph N-321.1
- b. One-hundred percent Magnetic Particle Examination per ASME Code,Section III, paragraph N-322.2.
- 2. Testing after finish machining
- a. One-hundred percent Ultrasonic Inspection of the flats and edges, performed in compliance with ASME Code,Section III, paragraph N-321.1
- b. Liquid penetrant inspection performed in compliance with ASME Code,Section III, paragraph N-322.3 on the bore and each side of each disc for eight inches radially from the bore.
D. The finish of the flywheel bore and the finish on each side of each disc for eight inches radially from the bore are held free of nicks, center punch marks, stencil marks, holes or other stress concentrations.
E. Welding was not performed on flywheel discs.
F. The keyway fillet radius on the bottom of the keyway is 0.125 inches minimum.
The flywheel material, which is pressure vessel quality, vacuum-improved steel plate, exceeds the requirements of ASTM-A-516, Grade 70 even though it was originally specified for ASTM-A-516 Grade 65. To improve the fracture toughness properties of the material, the flame cut discs, with the one-half inch allowance for machining, were heat treated as follows:
- 1. heated to 1650°F +/-25°F and held for minimum of 3.5 hours5.787037e-5 days <br />0.00139 hours <br />8.267196e-6 weeks <br />1.9025e-6 months <br />;
- 2. water quenched to below 400°F;
- 3. tempered at 1140°F for one-half hour per inch of thickness, air cooled.
The composition of the material as certified by the steel vendor is as follows:
ASTM-E-30 ASTM-E-30 C Mn P S Si Melt Number Slab Number (Weight %) (Weight %) (Weight %) (Weight %) (Weight %)
B3725 3&4 0.21 0.97 0.008 0.025 0.23 A8176 2 0.22 1.16 0.006 0.020 0.24 4.3-9 Rev. 35
MPS2 UFSAR The grain size of this silicone deoxidized steel is ASTM-E-112 size 7-8. The tensile properties of the flywheel material as certified by the steel vendor are as follows:
Tensile tests per ASTM-A-20 Drop weight test (DWT) - test at +40°F per ASTM-E-208.
0.2% Offset Melt Slab Tensile Elongation in Charpy V-notch at Yield Strength DWT Number Number Strength PSI 2 inch (%) 40°F (ft-lbf)
PSI B3725 3 76700 49000 30 104 109 91 OK B3725 4 75600 50700 31 103 95 97 OK A8176 2 76700 51500 29 84 73 83 OK The Charpy values measured for the flywheel material at 40°F are substantially higher than the data compiled on SA-516 grade 70 material by the Research & Product Development Department of CE. The report titled Longitudinal and transverse Charpy V-notch impact and dropweight test data for normalized and tempered SA-516 grade 70 material issued on August 26, 1971, and further identified by Laboratory Number X-24053 and R&PD Project Number 420001, was prepared for the Industrial Cooperative Program of the Material Division of the Pressure Vessel Research Committee of the Welding Research Council.
This indicates that the toughness properties of these wheels are better than typical SA-516 Grade
- 70. Therefore, the nil-ductility transition (NDT) temperature is lower than the highest value of
-10°F reported in that report.
Since the normal operating temperature of the flywheel is approximately 100°F, a substantial margin exists between the computer KI for large hypothetical cracks, and the toughness KIC. The critical crack size therefore, is greater than five inches from the bore of the wheel.
Crack growth calculations indicate that the number of starting cycles to cause a reasonably small crack to grow to critical size is orders of magnitude greater than the number of cycles expected during the life of Millstone Unit 2.
The loads that are considered for the calculation of the stresses in the flywheel are the combined primary stresses in the flywheel at normal operating speed. They include the stress due to interference fit on the shaft as well as the stress due to centrifugal force.
Normal operating speed of the flywheel is 900 rpm (less normal slip). The flywheel has a design overspeed of rated rpm plus 25 percent, which equals 1,125 rpm. The maximum tangential stresses in the flywheel at normal operating speed are 25 percent of the material yield strength.
The maximum tangential stresses in the flywheel at design overspeed are 30 percent of the material yield strength.
4.3-10 Rev. 35
MPS2 UFSAR The RCP flywheels are accessible for 100 percent in place volumetric ultrasonic examination during in-service inspection. Two (2) access panels, 180° apart, are provided on the outside of each RCP motor.
The replacement RCP motor flywheel is a one piece forging, 75 inches OD by 12 inches thick, shrink fitted onto and keyed to the motor shaft above the rotor.
The replacement RCP motors were procured as Quality Assurance items in accordance with 10 CFR 21 and 10 CFR 50 Appendix B. They are fully interchangeable with the original RCP motors.
The selection of material, machining and manufacturing operations, quality control, and the rigorous acceptance criteria established to assure the integrity of the flywheel and to minimize operating stresses include the following:
A. The principal stress does not exceed 30 percent of the yield point of the flywheel material (based on the tensile tests per ASTM-A-370) at the design overspeed of 125 percent of the normal operating speed not considering keyway stress concentration factors. The minimum keyway fillet radius is one-eighth inch.
B. If the bore in the flywheel was flame cut, a minimum of one-half inch of stock was left on the radius for machining to final dimensions.
C. All flywheel discs passed the following nondestructive testing:
Prior to machining:
- a. The flywheel material was subjected to a 100 percent volumetric ultrasonic examination using procedures and acceptance criteria as specified in Paragraphs NB2532.1 and NB2532.2 of the ASME B&PV Code,Section III.
The composition of the material as certified by the steel vendors is as follows:
Chemical Composition (weight percent)
Heat C Si Mn P S Cr Mo Ni V Number 320647 0.16 0.04 0.23 0.004 0.003 1.60 0.43 3.60 0.01 515100 0.20 0.08 0.33 0.007 0.005 1.61 0.44 3.54 0.03 The heat treatment was as follows:
- 1. Heated to 1,560°F to 1,580°F and held for a minimum of 7.5 hours5.787037e-5 days <br />0.00139 hours <br />8.267196e-6 weeks <br />1.9025e-6 months <br />.
4.3-11 Rev. 35
MPS2 UFSAR
- 2. Water quenched.
- 3. Tempered at 1,110°F to 1,185°F for 12 hours1.388889e-4 days <br />0.00333 hours <br />1.984127e-5 weeks <br />4.566e-6 months <br />, air cooled.
Tensile tests were performed on the flywheel material per ASTM A370.
The NDT temperature of the flywheel material, as obtained from DWT performed in accordance with the specification ASTM E 208 was no higher than -30°F.
The Charpy V-notch (Cv) upper-shelf energy level in the weak direction of the flywheel material was at least 50 ft-lbs. A minimum of three Cv specimens were tested from each forging in accordance with ASTM A 370.
The mechanical properties of the flywheel material as certified by the steel vendors are as follows:
Mechanical Properties Tensile 0.2% Offset Elongation Heat Charpy V-notch at 20°F Drop Weight Strength Yield Strength in 2 inches Number Energy (ft-lbf) Test at -30°F (psi) (psi) (%)
320647 110,000 93,700 21.7 130 126 92.9 No break 515100 112,000 96,000 22.4 140 130 122 No break Fracture Toughness The minimum static fracture toughness of the material at the normal operating temperature of the flywheel was equivalent to a critical stress intensity factor, KIC, of at least 150-ksi in.
Compliance was demonstrated by either of the following:
- a. Testing of the actual material to establish the KIC value at the normal operating temperature.
- b. Determining that the normal operating temperature is at least 100°F above the RTNDT.
In-service inspection includes 100 percent ultrasonic examination of the flywheel of one (1) of the four (4) RCPs during each inspection interval. The acceptance criteria is in accordance with ASME - Boiler and Pressure Vessel Code,Section III, for Class I vessels.
4.3-12 Rev. 35
MPS2 UFSAR 4.3.4 REACTOR COOLANT PIPING The RCS piping consists of two loops which connect the steam generators to the reactor vessel.
Each loop can be considered to consist of 42 inch ID hot leg piping connecting the reactor vessel outlets to the steam generator inlets and 30 inch ID piping connecting the steam generator outlets to the RCPs and the coolant pumps to the reactor vessel inlets. The two 30 inch piping segments are referred to as the pump suction leg and the cold leg respectively. A 12 inch schedule 160 surge line connects one loop hot leg to the pressurizer. Design parameters for the reactor coolant piping are given in Table 4.3-5.
The reactor coolant piping is designed and fabricated in accordance with the rules and procedures of ANSI B31.7, Class I. The anticipated transients listed in Section 4.2.1 form the basis for the required fatigue analysis to ensure an adequate usage factor.
The reactor coolant piping is fabricated from SA 516 Gr 70 carbon steel mill clad internally with roll bonded type 304L stainless steel. A minimum clad thickness of one-eighth inch is maintained.
The 12 inch surge line is fabricated from ASTM A351 Gr CF8M alloy steel.
Thermal sleeves are installed in the surge line nozzle, charging nozzles and shutdown cooling inlet nozzle to reduce thermal shock effects from auxiliary system. Clad sections of piping are fitted, where necessary, with safe ends for field welding to stainless steel components.
In response to industry experience, half nozzle replacements have been performed on selected instruments and sampling nozzles as a mitigation technique against pressurized water stress corrosion cracking (PWSCC).
The piping is shop fabricated and shop welded into subassemblies to the greatest extent practicable to minimize the amount of field welding. Fabrication of piping and subassemblies is done by shop personnel experienced in making large heavy wall welds. Welding procedures and operations meet the requirements of Section IX of the ASME Boiler and Pressure Vessel Code.
All welds are 100 percent radiographed and liquid-penetrant or magnetic-particle tested and all reactor coolant piping penetrations are attached in accordance with the requirements of ANSI B31.7. Cleanliness standards consistent with nuclear service are maintained during fabrication and erection. There are no dissimilar metal field welds.
4.3.5 PRESSURIZER The pressurizer maintains RCS operating pressure and compensates for changes in coolant volume during load changes. Table 4.3-6 gives design parameters for the pressurizer. The pressurizer is shown in Figure 4.3-7.
Pressure is maintained by controlling the temperature of the saturated liquid volume in the pressurizer. At full load nominal conditions, slightly more than one-half the pressurizer volume is occupied by saturated water, and the remainder by saturated steam. A number of the pressurizer heaters are operated continuously to offset the heat losses and the continuous minimum spray, 4.3-13 Rev. 35
MPS2 UFSAR thereby maintaining the steam and water in thermal equilibrium at the saturation temperature corresponding to the desired system pressure.
During load changes, the pressurizer limits pressure variations caused by expansion or contraction of the reactor coolant. The average reactor coolant temperature is programmed to vary as a function of load as shown in Figure 4.3-8. A reduction in load is followed by a decrease in the average reactor coolant temperature to the programmed value for the lower power level. The resulting contraction of the coolant lowers the pressurizer water level causing the reactor system pressure to decrease. The pressure reduction is partially compensated by flashing of pressurizer water into steam. All pressurizer heaters are automatically energized on low system pressure, generating steam and further limiting pressure decrease. Should the water level in the pressurizer drop sufficiently below its setpoint, the letdown control valves close to a minimum value and the available charging pumps in the chemical and volume control system (CVCS) are automatically started to add coolant to the system and restore pressurizer level.
When steam demand is increased, the average reactor coolant temperature is automatically raised in accordance with the coolant temperature program (Figure 4.3-8). The expanding coolant from the reactor coolant piping hot leg enters the bottom of the pressurizer (in-surge), compressing the steam and raising system pressure. The increase in pressure is moderated by the condensation of steam during compression and by the decrease in bulk temperature in the liquid phase. Should the pressure increase be large enough, the pressurizer spray valves open, spraying coolant from the RCP discharge (cold leg) into the pressurizer steam space. The relatively cold spray water condenses some of the steam in the steam space, limiting the system pressure increase. The programmed pressurizer water level is a power dependent function. A high level error signal produced by an in-surge causes the letdown control valves to open, releasing coolant to the CVCS and restoring the pressurizer to the prescribed level.
Small pressure and coolant volume variations are accommodated by the steam volume which absorbs flow into the pressurizer and by the water volume which allows flow out of the pressurizer. The total volume of the pressurizer is determined by consideration of the following factors:
- a. Sufficient water volume is necessary to prevent draining the pressurizer as the result of a reactor trip or a loss-of-load accident. In order to preclude the initiation of safety injection and of automatic injection of concentrated boric acid by the charging pumps, the pressurizer is designed so that the minimum pressure observed during such transients is above the setpoint of the safety injection actuation signal (SIAS);
- b. The heaters should not be uncovered by the out-surge following load decreases; ten percent step decrease, and five percent per minute ramp decrease;
- c. The steam volume should be sufficient to yield acceptable pressure response to normal system volume changes during load change transients; 4.3-14 Rev. 35
MPS2 UFSAR
- d. The water volume should be minimized to reduce the energy release and resultant containment pressure during a LOCA;
- e. The steam volume should be sufficient to accept the reactor coolant in-surge resulting from loss-of-load without the water level reaching the safety and power-operated relief valve (PORV) nozzles;
- f. During load following transients, the total coolant volume change and associated charging and letdown flows should be kept as small as practical and be compatible with the capacities of the volume control tank, charging pumps, and letdown control valves in the CVCS.
To account for these factors and to provide adequate margin at all power levels, the water level in the pressurizer is programmed as a function of average coolant temperature as shown in Figure 4.3-9. High or low water level error signals result in the control actions shown in Figure 4.3-10 and described above.
The pressurizer heaters are single unit, direct immersion heaters which protrude vertically into the pressurizer through sleeves welded in the lower head. Each heater is internally restrained from high amplitude vibrations and can be individually removed for maintenance during plant shutdown. Approximately 20 percent of the heaters are connected to proportional controllers which adjust the heat input as required to account for steady state losses and to maintain the desired steam pressure in the pressurizer. These heaters are separated into two banks (approximately 160 kW each) and are provided with diverse vital power.
The remaining heaters are connected to on-off controllers. These heaters, called backup heaters, are normally deenergized but are turned on by a low pressurizer pressure signal or high level error signal. This latter feature is provided since load increases result in an in surge of relatively cold coolant into the pressurizer, decreasing the temperature of the water volume. The action of the CVCS restoring the level results in a pressure undershoot below the desired operating pressure.
To minimize the pressure undershoot, the backup heaters are energized earlier in the transient, contributing more heat to the water before the low pressure setting is reached. An interlock will prevent operation of the backup heaters if the high level error signal occurs concurrent with a high pressurizer pressure signal. A low-low pressurizer level signal deenergizes all heaters to prevent heater burnout.
The pressurizer spray is supplied from each of the RCP discharges on one loop to the pressurizer spray nozzle. Automatic spray control valves control the amount of spray as a function of pressurizer pressure; both of the spray control valves function in response to the signal from the controller. These components are sized to use the differential pressure between the pump discharge and the pressurizer to pass the amount of spray required to prevent the pressurizer steam pressure from opening the PORVs during normal load following transients. A small continuous flow is maintained through the spray lines at all times to keep the spray lines and the surge line warm, reducing thermal shock during plant transients. This continuous flow also aids in keeping the chemistry and boric acid concentration of the pressurizer water equal to that of the coolant in 4.3-15 Rev. 35
MPS2 UFSAR the heat transfer loops. An auxiliary spray line is provided from the charging pumps to permit pressurizer spray during plant heatup, or to allow cooling if the RCPs are shut down.
In the event of an abnormal transient which causes a sustained increase in pressurizer pressure, at a rate exceeding the control capacity of the spray, a high pressure trip level will be reached. This signal trips the reactor and opens the two PORVs. The steam discharged by the relief valves is piped to the quench tank where it is condensed. In accordance with Section III of the ASME Boiler and Pressure Vessel Code, the RCS is protected from overpressure by two spring-loaded safety valves. The discharge from the safety valves is also piped to the quench tank. See Section 4.3.7 for the safety valve design parameters.
The pressurizer is supported by a cylindrical skirt welded to the lower head. Since the pressurizer surge line has sufficient flexibility, no provisions are made for horizontal movement and the skirt is bolted rigidly to the floor.
The pressurizer assembly was replaced in 2006 with a new pressurizer assembly fabricated from materials that are less susceptible to primary water stress corrosion cracking. The replacement pressurizer is fabricated and installed to the same design criteria as the original pressurizer with some improvements. The cylindrical shell sections, upper and lower heads including the large bore nozzles of the replacement pressurizer are forged components, thereby minimizing the welds and weld inspections. Safe ends made of stainless steel are provided as required on the large bore nozzles to facilitate field welds to the connecting piping. The interior surface of the pressurizer is clad with weld deposited stainless steel. The heater sleeves, instrument nozzles and the vent/pass nozzle are fabricated from stainless steel instead of the originally used Inconel Alloy 600 material. The nozzles are attached to the pressurizer by j-groove welds to the clad buildup. The total number of heaters is reduced from 120 to 60. The heat output of each heater is roughly twice that of the replaced heater, thus maintaining the same amount of total heat output.
A six and one-half inch inside diameter vent port was added on the upper head of the replacement pressurizer. This vent port is a substitute for the removal of the pressurizer manway during routine refueling outages with RCS nozzle dams installed. The vent port is sized to avoid a RCS pressurization that would exceed the design pressure of the RCS nozzle dams following a postulated loss of shutdown cooling with the reactor vessel head on and reactor coolant water levels one foot below the reactor vessel flange or lower. For non-routine outages where nozzle dams are installed and reactor coolant water levels are higher than one foot below the reactor vessel flange and the reactor vessel head is on, the pressurizer manway will need to be removed in order to avoid a RCS pressurization that would exceed the nozzle dam design pressure following a postulated loss of shutdown cooling. In addition, removal of either the vent port or the pressurizer manway provides an adequate RCS vent path for low temperature overpressure protection in Mode 5 and Mode 6 when the head is on the reactor vessel.
4.3.6 QUENCH TANK The quench tank is designed to prevent the discharge of the pressurizer relief or safety valves from being discharged to the containment. The quench tank is shown in Figure 4.3-11. The steam discharged into the quench tank from the pressurizer is discharged under water by a sparger to 4.3-16 Rev. 35
MPS2 UFSAR enhance condensation. The normal quench tank water volume of 135 cubic feet is sufficient to condense the steam released from the pressurizer safety and relief valves. The quench tank is sized to accommodate the steam released as a result of a loss-of-load accident followed immediately by an uncontrolled rod withdrawal accident with no coolant letdown or pressurizer spray.
The water temperature rise in the quench tank is limited to 281°F, assuming a maximum initial water temperature of 120°F. The gas volume in the tank is sufficient to limit the maximum tank pressure after the above steam release to 35 psia. The contents of the quench tank are cooled by recirculation through the primary drain tank and quench tank cooler. The temperature of the water in the quench tank is indicated on the main control console. A high temperature alarm is also provided. A high quench tank temperature alerts the operator to cool the tank contents.
A measurement channel provides a quench tank pressure indication on the main control console and actuates a high pressure alarm. High quench tank pressure indicates that the tank has received a discharge from the safety or relief valves, or from the HPSI test line relief valve. The operator would then take action to restore the tank to normal operating conditions.
Quench tank level indication and high and low level alarms are also provided on the main control console.
The quench tank can condense the steam discharged during a loss-of-load accident as described in Section 14.2 without exceeding the rupture disc set point, which is rated for 96 psig at 72°F and 89 psig at 350°F, assuming normal closing of the safety valves at the end of the accident. It is not designed to accept a continuous uncontrolled safety valve discharge. The rupture disc on the quench tank provides code overpressure protection of the tank. The rupture disc vents to the containment. The quench tank parameters are given in Table 4.3-7.
The tank normally contains demineralized water under a nitrogen overpressure. The sparger, spray header, nozzles and rupture disc fittings are stainless steel. The tank is designed and fabricated in accordance with the ASME Boiler and Pressure Vessel Code,Section III, Class C.
The quench tank is located at a level lower than the pressurizer. This ensures that any PORV or pressurizer safety valve leakage from the pressurizer, or any discharge from these valves, drains to the quench tank.
4.3.7 VALVES The design parameters for the pressurizer spray valves (RC-100E, RC-100F) are given in Table 4.3-8. The PORV isolation valve (RC-403, RC-405) parameters are given in Table 4.3-9.
The position of each valve on loss of actuating signal (failure position) is selected to ensure safe operation. System redundancy is considered when specifying the failure position of any given valve. Valve position indication is provided at the main control panel.
4.3-17 Rev. 35
MPS2 UFSAR Manually operated valves in the RCS have backseats to limit stem leakage when in the open position. Globe valves are installed with flow entering the valve under the seat. This arrangement will reduce stem leakage during normal operation or when closed.
The two PORVs, designated RC-402 and RC-404 on Figure 4.1-1, relieve sufficient pressure to avoid opening of the RCS safety valves. The relief valves are actuated by the high RCS pressure trip signal. Parameters for these valves are given in Table 4.3-10.
The valves are solenoid-operated power relief valves. The two half capacity valves are located in parallel pipes which are connected to the pressurizer relief valve nozzle in the inlet side and to the relief line piping to the quench tank on the outlet side. A motor-actuated isolation valve is provided upstream of each of the relief valves to permit isolating the valve for maintenance or in case of valve leakage.
The capacity of the PORVs is sufficient to pass the maximum steam surge associated with a continuous control rod withdrawal accident starting from low power. Assuming that a reactor trip is effected on a high pressure signal, the capacity of the PORVs is sufficient so that the safety valves do not open. The relief valve capacity is also large enough so that the safety valves do not open during a loss-of-load accident from full power. This assumes normal operation of the pressurizer spray system, and reactor trip on high pressure. The PORVs also function to provide low temperature overpressurization protection (LTOP) to the RCS. This is accomplished by manually selecting a reduced valve setpoint as described in Section 7.4.8.
Two safety valves, designated RC-200 and RC-201 on Figure 4.1-1 are located on the pressurizer to provide overpressure protection for the RCS. They are totally enclosed, backpressure compensated, spring-loaded safety valves meeting ASME Code requirements. Parameters for these valves are given in Table 4.3-11.
Both safety valves (RC-200, 201) are equipped with acoustic valve position monitors. These monitors will provide operators with an indication of the status of the safety valves. The PORVs have been upgraded to monitor their position from the control room by the position indication lights instead of the acoustic monitoring method previously used. The valve monitoring system conforms with NUREG-0578 C lessons learned from TMI Task Force Report.
The safety valves pass sufficient pressurizer steam to limit the RCS pressure to 110 percent of design (2,735 psig), following a complete loss of turbine generator load without simultaneous reactor trip. Reactor trip occurs on a high RCS pressure signal. To determine the maximum steam flow, the only other pressure relieving system assumed operational is the steam system safety valves. Conservative values for all system parameters, delay times, and core moderator coefficient are assumed. This analysis is given in Section 14.2, Loss-of-Load External Electrical Load and/or Turbine Trip.
The mounting of pressure relieving devices (safety valves and relief valves) within the RCPB and on the main steam lines outside of the containment is in accordance with the applicable provisions of ASME Boiler and Pressure Vessel Code Section III.
4.3-18 Rev. 35
MPS2 UFSAR The pressurizer safety and relief valves are connected to nozzles on the top of the pressurizer vessel. The loads which the nozzles experience during normal plant operation and when the valves are relieving are included in the specification for the pressurizer.
All overpressure relief valves and their connected piping (i.e., headers, header connections and discharge piping) are designed to withstand the following conditions without exceeding the applicable codes primary stress allowable: maximum loads due to valve discharge thrust, internal pressure, dead weight and earthquake applied simultaneously. When more than one relief valve is attached to a piping system, the loads due to all relief valves discharging simultaneously are applied to the system along with the above mentioned primary loads. In addition, the loads from the most critical combination of valves discharging are applied. The local stresses in the main steam line outside the containment at the connection of the relief valves were computed as specified in Welding Research Council Bulletin 107 and contained below the allowable primary stress level.
The pressurizer safety and relief valve discharge piping system was modified by deleting the loop seals upstream of the Pressurizer Safety Valves (PSVs) and Power-Operated Relief Valves (PORVs). The piping for both the PSVs and PORVs was again modified during the replacement of the pressurizer. The PORVs were also replaced with upgraded PORVs and credited as an acceptable pressurizer steam space vent path during post accident conditions. The new piping configuration was evaluated to address NUREG-0737, Action Item II.D.1 (relief valve and safety valve testing).
The thermal-hydraulic analysis was performed to calculate the transient fluid time-history forcing functions acting on the pipe segments due to each safety or relief valve discharge. These forcing functions are combined in a common entry mode to maximize the forces acting on the discharge piping. The potential case of water discharge through relief valves during low temperature modes of operation was also considered.
The structural reanalysis of the PSV and PORV discharge piping system included the normal plant loading, plant transients described in Section 4.2.1, seismic loading, and the fluid transient forcing functions. Seismic analysis of the piping system was performed by the modal analysis response spectra method. Dynamic response of the piping system to the PSV and PORV discharge loads was performed by the time-history modal superposition method.
Pipe primary and secondary stress intensities and fatigue usage factors were found to be within the Code allowable values. The pipe supports of the PSV and PORV discharge piping system were modified to accommodate the load and displacements resulting from the reanalysis.
The main steam relief valve system is designed so that the blowdown force is transmitted directly to the structure by mechanical/structural devices, and not through the piping. These relief valves are provided with discharging stacks to direct steam blowdown to atmosphere. Stacks are designed so that backpressure does not result in a valve reaction force.
Pumps and valves within the RCPB are classified as either active or inactive components. Active components are those whose operability is relied upon to perform a safety function, as well as 4.3-19 Rev. 35
MPS2 UFSAR reactor shutdown function, during the transients or events considered in the respective operating condition categories. Inactive components are those whose operability (e.g., valve opening or closure, pump operation or trip) are not relied upon to perform the system function during the transients or events considered in the respective operating condition categories. Thus, certain pumps and valves (classified as active components) within the RCPB are required not only to serve as pressure-retaining components (as in the case of passive components such as vessel and piping) but also to operate reliably to perform a safety function such as safe shutdown of the reactor and mitigation of the consequences of a pipe break accident under the loading combinations considered in RCPB as either active or inactive. The only pumps within the RCPB are the RCPs which are inactive under faulted conditions.
Active components outside of the RCPB have been designed to function as required when subjected to the loadings and the maximum pressure and temperature occurring under normal and accident conditions in the areas in which the components are located. Anticipated temperature and pressure transients which would have an effect on operability of components were specified as design requirements.
A complete list of the active pumps and valves located within the RCPB was provided previously as part of Amendment 14, and is found as Table 4.3-12.
The following is a list of active pumps and valves located outside the RCPB whose operability is relied upon to perform a safety function such as safe shutdown of the reactor or mitigation of the consequences of a postulated pipe break in the RCPB.
Pumps Post Normal LOCA Component Quantity Materials Code Test Code Position Position High Pressure 3 Draft ASME Code ASI Standard 610, Off On Safety Injection for Pumps and ASME Power Test Valves for Nuclear Code PTC- 8.2 and Power, Class II, Standards of the Nov. 1968 Hydraulic Institute Low Pressure 2 Draft ASME Code ASI Standard 610 Off On Safety Injection for Pumps and Standard of the Valves for Nuclear Hydraulic Institute, Power, Class II, and ASME Power Nov. 1968 Test Code PTC-8.2 4.3-20 Rev. 35
MPS2 UFSAR Pumps Post Normal LOCA Component Quantity Materials Code Test Code Position Position Containment 2 Draft ASME Code Standard of the Off On Spray Pumps for Pumps and Hydraulic Institute Valves for Nuclear Power, Class II, 1968 Valves Normal Post LOCA Component Quantity Materials Code Test Code Position Position High Pressure 2 Draft ASME Code Closed Open Safety Injection for Pumps and Pump Suction Valves for Nuclear (Check) Power, Nov. 1968 High Pressure 4 Draft ASME Code Closed Open Safety Injection for Pumps and Pump Discharge Valves for Nuclear (Check) Power, Nov. 1968 Low Pressure 2 Draft ASME Code Closed Open Safety Injection for Pumps and Pump Discharge Valves for Nuclear (Check) Power, Nov. 1968 Containment - Draft ASME Code - As As Required Isolation Valves for Pumps and Required Valves for Nuclear Power, Nov. 1968 Containment 2 Draft ASME Code Closed Open Spray (Motor for Pumps and Operated) Valves for Nuclear Power, Nov. 1968 Containment 2 Draft ASME Code Closed Open Sump Discharge for Pumps and (Check) Valves for Nuclear Power, Nov. 1968 4.3-21 Rev. 35
MPS2 UFSAR Valves Normal Post LOCA Component Quantity Materials Code Test Code Position Position Refueling Water 2 Draft ASME Code Closed Open during Storage Tank for Pumps and Injection Mode.
Discharge Valves for Nuclear Closed during (Check) Power, Nov. 1968 Recirculation Mode.
Shutdown 1 Draft ASME Code Open Open Cooling Heat for Pumps and Exchanger Valves for Nuclear Bypass (2-SI- Power, Nov. 1968 306) (Air Operated)
Shutdown 1 Draft ASME Code Closed Closed Cooling Heat for Pumps and Exchanger Flow Valves for Nuclear Control Power, Nov. 1968 (2-SI-657)
(Air Operated)
For inactive valves and pumps other than the RCPs, the rules of the Pump and Valve Code (March 1970 Draft) for design conditions are applied in evaluating the loadings produced by the Emergency and Faulted Conditions.
For active components, additional requirements are imposed on the design to assure operability during the faulted operating conditions. As appropriate, these additional requirements consist of simulated tests and/or supplementary calculations which demonstrate that the active component will perform its required function during the specified conditions. Where calculations are employed, the primary stresses produced by the faulted conditions are limited to values less than the Emergency Condition limits of Subparagraph HB-3224.1 in all regions of the active component where deformations may impair the required function.
For the RCPs, as appropriate, the stress criteria for Vessels, as discussed above, are applied in evaluating the Emergency and Faulted Conditions (elastic analysis). These limits are consistent with the Design by Analysis method of Article 4, ASME Section III Code which is applied in the design calculation. For design conditions other than those explicitly addressed by Section III of the ASME Code, and where design calculations are used to evaluate stresses and deformations in pumps, the methods and criteria applied are in accordance with Article 4, ASME Section III Code. The calculations will include the effects of gross and local structural discontinuities and the loadings produced by geometrical eccentricities. Current state-of-the-art analytical methods including finite element techniques, are employed in the calculations. Experimental techniques were not employed.
4.3-22 Rev. 35
MPS2 UFSAR 4.3.8 INSTRUMENTATION APPLICATION The measurement channels necessary for operational control and protection of the RCS are described below. A brief explanation of the purpose of each measurement channel is made and a summary of resulting action is given. A detailed description of critical instrument channel actions may be found in Chapter 7.
Four independent measurement channels are provided for each parameter which initiates protective system action. Two independent signals are required to initiate protective action, thereby, preventing spurious actions resulting from the failure of one measurement channel. This arrangement results in a high degree of protective measurement channel reliability in terms of initiating action when required and avoiding unnecessary action from spurious signals. Two independent measurement channels are provided for parameters which are critical to operational control. These control channels are separate from the protective measurement channels. To avoid control conflicts, control action is derived from only one channel at any time, while the second channel serves as a backup. This allows continued operation of the facility if one channel fails and permits maintenance on the failed channel during operation. This arrangement results in increased availability.
4.3.8.1 Temperature 4.3.8.1.1 Hot Leg Temperature Each of the two hot legs contains five narrow range channels to measure coolant temperature leaving the reactor vessel. Four of these channels are used to furnish a hot leg temperature signal to the reactor protective system. The fifth hot leg temperature measurement channel provides a signal to the average temperature computer which is a part of the reactor regulating system (RRS).
The average temperature of the loop is recorded on a two-pen recorder in the main control room.
The second pen on each loops recorder records an average temperature reference signal received from the RRS.
A high temperature alarm is provided on this channel to alert the operator to a high temperature condition. The temperature from this measurement channel is indicated in the main control room in addition to being recorded. The other hot leg temperature channels are also displayed in the main control room.
4.3.8.1.2 Cold Leg Temperature Each of the four cold legs contains three temperature measurement channels. The cold leg Resistance Temperature Detectors (RTD) are located downstream of the RCPs. Two channels from each cold leg (four per heat transfer loop) are used to furnish a cold leg coolant temperature signal to the reactor protective system (RPS). All eight of these cold leg temperature measurements are indicated in the main control room. Two of the remaining four cold leg temperature measurement channels, one each from opposite loops, are narrow range temperature measurements that input to the RRS for calculation of average temperature and the Feedwater regulating system for dynamic compensation in single element control. These loops also provide 4.3-23 Rev. 35
MPS2 UFSAR control room indication of narrow range temperature. The remaining two cold leg measurement channels, one each from opposite loops, are wide range temperature measurements that provide input to the subcooled margin monitor (Inadequate Core Cooling ICC) and Low Temperature Over Pressure (LTOP) channels. These loops also provide control indication and recording of wide range temperature.
4.3.8.1.3 Surge Line Temperature This measurement channel provides an indication of surge line temperature in the main control room. A low surge line temperature condition activates an alarm in the main control room. The low-temperature alarm during normal operation is an indication that the continuous spray rate has decreased.
4.3.8.1.4 Pressurizer Vapor Phase Temperature The pressurizer vapor phase RTD is located on the upper dome of the pressurizer. This channel provides a wide range temperature indication of the temperature of the steam phase in the pressurizer.
4.3.8.1.5 Pressurizer Water Phase Temperature The pressurizer water phase RTD is located at an elevation below the top of the pressurizer heaters. This channel provides a wide range temperature indication in the main control room and is used during plant heatup and cooldown.
4.3.8.1.6 Spray Line Temperature An RTD in each spray line provides a temperature indication and a low temperature alarm in the control room for each spray line. A low temperature alarm during normal operation is an indication the continuous spray rate has decreased.
4.3.8.1.7 Relief and Safety Valve Discharge Temperature Temperatures in the pressurizer safety valve and PORV discharge lines are measured and indicated in the main control room. A high temperature in one of these lines is an indication that the associated valve may be leaking. High temperature alarms are provided to alert the operator to this condition.
4.3.8.1.8 Quench Tank Temperatures The temperature of the water in the quench tank is indicated in the main control room. A high temperature alarm is also provided. A high quench tank temperature alerts the operator to the requirement for cooling of the tank contents.
4.3-24 Rev. 35
MPS2 UFSAR 4.3.8.1.9 Reactor Vessel Flange Seal Leakage Temperature This RTD is located in the reactor vessel flange leak-off line. The channel is displayed in the main control room and actuates a high temperature alarm. A high temperature is indicative of excessive leakage past the first reactor vessel flange seal.
4.3.8.1.10 RCS High Point Vents Leakage Temperature Thermocouple installed on the downstream side of solenoid valve train of the reactor vessel head vent system is utilized to monitor leakage past the system solenoid valves. Under normal operating conditions, the thermocouple will measure the ambient temperature in the piping downstream of the solenoid valve train. The output of each thermocouple is continuously recorded by the plant computer. Note that monitoring of the leakage past the PORVs in the pressurizer steam space vent path is described in Section 4.3.8.1.7, above.
Any leakage through the system valves will cause an increased temperature in the downstream piping which will be detected by the thermocouple. At a predetermined setpoint, an alarm will be actuated, identifying a high temperature reading on the appropriate thermocouple. Once a high temperature alarm is received, further actions will be governed by the Technical Specifications for reactor coolant system leakage.
4.3.8.2 Pressure 4.3.8.2.1 Pressurizer Pressure Four independent narrow range pressure channels are provided for initiation of protective systems action. The pressure transmitters are connected to the upper portion of the pressurizer via the upper level measurement nozzles and measure pressurizer vapor pressure. All four channels are indicated in the main control room and actuate separate high, low, or low low pressure alarms in the control room.
The protection actions these pressure signals initiate are:
- 1. Reactor trip on high primary system pressure. The reactor trip signals are also used to open the PORVs;
- 2. Safety injection system actuation on low low primary system pressure;
- 3. Reactor trip on a low primary system pressure. The set point is a function of the coolant temperatures in the hot and cold legs. The variable set point has high and low limits alarmed in the control room and is not allowed to decrease below 1865 psia.
4.3-25 Rev. 35
MPS2 UFSAR 4.3.8.2.2 Pressurizer Pressure Two independent pressure channels provide narrow range pressure signals for controlling the pressurizer heaters and spray valves. The output of one of these channels is manually selected to perform the control function. During normal operation, a small group of heaters are proportionally controlled to offset heat losses. If the pressure falls below a low pressure set point, all of the heaters are energized. If the pressure increased above the high pressure set point, the spray valves are proportionally opened to increase the spray flow rate as pressure rises. An interlock will prevent operation of the backup heaters in the event of a high level error signal concurrent with a high pressure condition. These two channels are also used to provide pressurizer pressure signals to the RRS. The two channels are continuously recorded in the main control room and are provided with high and low pressure alarms.
4.3.8.2.3 Pressurizer Pressure Two low-range pressure measurement channels provide a control room indication of RCS pressure during plant startup and shutdown in the main control room. They also provide independent pressure signals to the shutdown cooling suction isolation valves (refer to Section 9.3.4.1) which prevent these valves from opening above a selected set point. If the shutdown cooling suction valves are open when the pressure exceeds a selected set point (280 psia), an annunciator receives a signal to alarm from these pressure channels. The channels also provide signals to actuate the PORVs for LTOP. These two instrument channels are independent and redundant.
4.3.8.2.4 Quench Tank Pressure This measurement channel provides a quench tank pressure indication in the main control room and actuates a high pressure alarm. High quench tank pressure indicates that the tank has received a discharge from the safety or relief valves, or from the HPSI test line relief valve. The operator will then take action to restore the tank to normal operating conditions.
4.3.8.3 Level 4.3.8.3.1 Pressurizer Level Two pressurizer level channels are used to provide two independent level signals for control of the pressurizer liquid level. These signals are used to deenergize the pressurizer heaters on low low pressurizer level to prevent heater burn out, provide input to one pen in the two-pen recorder in the control room, and actuate high and low pressurizer level alarms in the main control room. The second pen on the level recorder records the programmed pressurizer level setpoint computed by the RRS as a function of the average reactor coolant temperature. The level transmitters are compensated for the steam and water densities existing in the pressurizer during normal operation.
The liquid level in the pressurizer is programmed to vary as a function of average reactor coolant temperature. This level set point is computed by the RRS and furnished to controls associated 4.3-26 Rev. 35
MPS2 UFSAR with these measurement channels. One of the two measurement channels is manually selected to furnish an actual liquid level signal to the controls. If these two signals differ, the level control adjusts the CVCS charging or letdown flow rates to make the difference zero. Each of the level channels is indicated in the main control room and is equipped with a high and low level alarm in the control room.
4.3.8.3.2 Pressurizer Level One wide range pressurizer channel is provided for main control room indication of pressurizer level during plant startup and shutdown.
4.3.8.3.3 Quench Tank Level A quench tank level channel indicates quench tank level in the main control room. The transmitter also activates high and low level alarms in the main control room.
4.3.8.4 Reactor Coolant Loop Flow For independent differential pressure measurement channels are provided in each heat transfer loop to measure the pressure drop across the steam generators. Four pressure taps are located in each hot leg piping section just before the elbow entering the steam generator and four pressure nozzles are located in the steam generator outlet plenum. Four differential pressure transmitters are connected between the four hot leg nozzles and the steam generator nozzles, resulting in four steam generator differential pressures.
The outputs of the transmitters are sent to four analog summing devices in the low total flow trip logic. Each summing device receives two differential pressure signals with the summation of these signals representing the total core flow at all times, even during coast down transients.
The summing devices provide four independent total flow signals. The four signals are indicated separately in the main control room and activate separate low-flow alarms. In the RPS, they are compared with the low-flow reactor trip set point, selected by the operator to correspond with the number of operating RCPs. If two channels indicate flow which is less than the flow set point, the reactor is tripped.
4.3.8.5 Reactor Coolant Pump Instrumentation The RCPs and motors are equipped with the instrumentation necessary for proper operation and to warn of incipient failures. (See Figure 4.3-4.) A description of the major channels follows:
4.3.8.5.1 Pump Seal Temperatures The reactor coolant temperature in the lower seal cavity may be indicated in the main control room through its selection on a multiposition switch. The switch also permits display of all of the remaining temperature measurement channels for each pump. The pump seal temperature is alarmed to alert the operators to a high-temperature condition. A high temperature condition is an 4.3-27 Rev. 35
MPS2 UFSAR indication that the integral heat exchanger is not performing satisfactorily or is a backup indication that the component cooling water flow has decreased or supply temperature has increased.
4.3.8.5.2 Motor Stator Temperatures Each RCP motor is provided with six RTDs embedded in the stator windings. During initial pump testing the highest reading RTD was selected for this temperature measurement control.
The signal output of this RTD may be selected for indication in the main control room by a multiposition switch. Should stator temperature exceed a predetermined limit, a high temperature alarm will be sounded in the control room. High temperature is detrimental to motor winding insulation life, and may be caused by high ambient temperature, reduction in the cooling air flow to the stator or inadequate time delay between successive starts of the motor.
4.3.8.5.3 Motor Thrust Bearing Temperatures Temperatures of the motor upward thrust bearing, and downward thrust bearing may be indicated in the main control room through selection on a multiposition switch. A high temperature alarm is provided for each pump in the main control room which is annunciated if any one of the bearing temperatures in the pump exceeds a safe value.
4.3.8.5.4 Pump Controlled Bleed-Off Temperature The temperature of the controlled bleed-off flow may be displayed in the main control room through its selection on a multiposition switch. An alarm signal is provided should the controlled bleed off temperature exceed a high limit. A high temperature condition is an indication that the integral heat exchanger is not operating properly.
4.3.8.5.5 Antireverse Device Bearing Temperature This measurement channel provides a status on the operating temperature of the antireverse device bearing. Display in the main control room is available through selection on a multiposition switch. A high temperature alarm is provided to alert plant operators to an abnormal condition.
4.3.8.5.6 Upper and Lower Guide Bearing Temperature The upper and lower guide bearing temperatures may be displayed in the main control room at the option of the operators. An alarm signal is provided if the high temperature limit is exceeded.
4.3.8.5.7 Lube Oil Cooler Inlet and Outlet Temperature The inlet and outlet temperatures of the lube oil cooler are available for display in the main control room and are alarmed to alert plant operators to high temperature conditions.
4.3-28 Rev. 35
MPS2 UFSAR 4.3.8.5.8 Lower Bearing Oil Temperature The lower bearing oil temperature may be displayed in the main control room at the option of the plant operators.
4.3.8.5.9 Pump Seal Pressures The middle, upper, and controlled bleed-off pump seal cavities in each pump are provided with pressure sensors which generate a signal proportional to the pressure within the cavity. The pressure in any seal may be selected for display in the main control room through its selection on a three-position switch. A high and low pressure alarm is annunciated for the middle and upper seal measurement channels. Abnormally, high pressure in the upper and middle seal cavities indicates a failed or failing lower or middle seal. A low pressure condition in the middle seal cavity indicates a failed or failing upper seal. A recorder in the control room records seal pressures in order to recognize pump seal degradation.
4.3.8.5.10 Motor Oil Lift Pressure This pressure measurement channel provides a signal to the RCP control circuit to prevent motor start with insufficient motor thrust bearing oil pressure.
4.3.8.5.11 Lube Oil Filter Pressure Differential There are three lube oil filters and one strainer, each with differential pressure indication capability. These measurement channels provide alarms for high differential pressure across any of the filters or the strainer, indicating clogging.
4.3.8.5.12 Pump Controlled Bleed-Off Flow Flow instruments are used to measure the controlled bleed off flow from the pump upper seal cavity to the chemical and volume control system. These instruments provide a remote indication of the flow rate in the East and West electrical penetration rooms, and annunciate high and low flow alarms in the control room. There is also an input to the plant computer and a recorder in the control room which records flow.
4.3.8.5.13 Lube Oil and Antireverse Device Lube Oil Flow Switch These measurement channels provide alarm signals when a low flow condition exists in the thrust bearing lube oil loop or in the antireverse device lube oil flow.
4.3.8.5.14 Motor Oil Reservoir Level Float-type sensors or differential pressure transmitters are used to produce signals proportional to the oil levels in the upper and lower motor oil reservoirs. These signals are used to provide an indication on the main control panel of the oil level in each oil reservoir. Either oil reservoir level 4.3-29 Rev. 35
MPS2 UFSAR may be selected for display in the control room through use of a two-position switch. Each signal also annunciates a high or low level alarm in the control room.
4.3.8.5.15 Vibration Instrumentation Motor vibration is sensed by two velomitor probes attached to the upper motor frame. Excessive motor vibration will cause an alarm on the plant process computer.
Pump shaft orbit is monitored by two proximity probes mounted 90 degrees to each other in a horizontal plane. A separate key phasor probe provides a single pulse per revolution as a reference for determining angular changes in shaft orbit. Outputs from the probes are also recorded.
4.3.8.5.16 Reverse Rotation Switch Reverse rotation of an RCP is sensed by a reverse rotation switch. This switch actuates an alarm in the control room. Reverse rotation indicates failure of the mechanical anti-reverse device.
4.3.8.5.17 (Deleted) 4.3.8.5.18 RCP Underspeed Reactor Trip An RCP underspeed trip has been added which uses a speed sensor on the RCP motor. The sensor generates a frequency signal proportional to speed which is in turn converted to a voltage. This voltage signal is maintained by the RPS, with one pump signal being monitored by only one channel in the RPS. When any two pump speeds drop below 830 RPM a reactor trip will occur.
This trip is designed to protect against simultaneous loss of all pumps and the resulting loss of coolant flow, with a faster reaction or trip time, than is provided by the steam generator differential pressure signal.
4.3.9 REACTOR COOLANT VENTING SYSTEM The RCS venting system provides the capability for removing noncondensible gases collected in the system in order to allow for satisfactory long term core cooling.
The two important safety functions enhanced by this venting capability are core cooling and containment integrity. For events within the present design basis for nuclear power plants, the capability to vent noncondensible gases will provide additional assurance that the requirements of 10 CFR 50.44 will be met. For events beyond the design basis, this venting capability will substantially increase the ability to deal with large quantities of noncondensible gas.
Reactor Vessel Head Vent System The reactor coolant head vent system is equipped with two (2) solenoid-operated globe valves in series in each piping train. Each valve has remote-manual control capability from the control room with open and closed position indication. Provision of two (2) solenoid operated globe valves in series for each vent train minimizes the probability of a vent path failing to close, once 4.3-30 Rev. 35
MPS2 UFSAR opened. The power source for each valve train is an independent redundant DC emergency bus, energized from separate redundant battery systems. In addition, the valves also receive power from redundant independent AC emergency buses. All valves fail closed upon loss of power supply to the actuator. The solenoid vent valves are qualified to IEEE-344-1975.
A manual isolation valve is installed downstream of the solenoid operated vent valves. This valve is normally open and is intended to isolate leakage that may develop through the solenoid-operated valves. Also, a manual isolation valve is located just upstream of the two solenoid valves on each train of the RCS head vent piping, capable of isolating the affected train. Piping upstream of the valve is designed to reactor coolant system pressure rating, providing an at-power isolation capability.
The discharge sparger for the reactor coolant head vent system is located in the vicinity of the containment air coolers where the vented gases will be cooled, mixed with additional containment air, and discharged into the lower elevation of the containment. Uniform mixing of the containment post accident atmosphere is provided by the post-accident recirculation system. The RCS vent system piping has been analyzed in accordance with ASME,Section III, of the Boiler and Pressure Vessel Code, for the Class 1 portion of the system. The balance of the system has been analyzed pursuant to ANSI B31.1 Power Piping Code.
Pressurizer Steam Space Vent System Venting of the noncondensible gases can also be performed from the pressurizer. The pressurizer venting system consists of two flow paths with redundant isolation valves in each flow path. Each flow path has a power operated relief valve and a block valve. The block valve in each train is normally open. During the pressurizer replacement project the two (2) power operated relief valves were upgraded so they can be credited to perform the venting function post accident. The PORVs are EEQ qualified and receive power from battery backed independent vital DC buses.
The noncondensibles are vented via the PORV discharge piping into the quench tank and then to the waste gas header as necessary. If the pressure reaches in excess of the rupture disc relief pressure, the noncondensibles would be released into the containment. The PORV inlet and discharge piping has been analyzed in accordance with ASME,Section III, of the Boiler and Pressure Vessel Code, Class 1 and Class 2 and 3 requirements respectively.
The reactor vessel and pressurizer vents were designed to utilize existing penetrations within each vessel. The system can pass in excess of the gas volume equivalent to one-half the RCS volume in one (1) hour. Although the RCS vents are larger than the size corresponding to the definition of LOCA (10 CFR 50, Appendix A), consequences of ruptures of the vents are bounded by the results of current small break loss of coolant accident (SBLOCA) analyses.
Since the vent lines are sized larger than the size corresponding to the definition of LOCA, the system is equipped with two (2) solenoid-operated globe valves in series in each piping train.
Each valve has remote-manual control capability from the control room with open and closed position indication. A manual isolation valve is installed downstream of the solenoid operated vent valves on each of the reactor and pressurizer vent systems. This valve is normally open and is intended to isolate leakage that may develop through the solenoid operated valves. Also, a manual 4.3-31 Rev. 35
MPS2 UFSAR isolation valve is located just upstream of the two solenoid valves on each train of the RCS head vent piping, capable of isolating the affected train.Piping upstream of the valve is designed to reactor coolant system pressure rating, providing an at-power isolation capability.
The design of the venting system minimizes the probability of a vent path failing to close, once opened. This has been accomplished by providing two (2) solenoid operated globe valves in series for each vent train. The power source for each valve train is an independent redundant DC emergency bus, energized from separate redundant battery systems. In addition, the valves also receive power from redundant independent AC emergency buses. All valves fail closed upon loss of power supply to the actuator.
The discharge sparger for the RCS vent system is located in the vicinity of the containment air coolers where the vented gases will be cooled, mixed with additional containment air, and discharged into the lower elevation of the containment. Uniform mixing of the containment post-accident atmosphere is provided by the post-accident recirculation system.
The RCS vent system piping has been analyzed in accordance with ASME,Section III, of the Boiler and Pressure Vessel Code, for the Class 1 portion of the system. The balance of the system has been analyzed pursuant to ANSI B31.1 Power Piping Code. The solenoid vent valves are qualified to IEEE-344-1975.
4.3.10 PERMANENT REACTOR CAVITY SEAL The permanent reactor cavity seal is designed to contain refueling water in the refueling cavity for fuel shuffle during outages. The reactor cavity seal consists of seal membrane sub-assembly and support structure sub-assembly. The seal membrane sub-assembly consists of a stainless steel membrane, inner and outer legs attached to the reactor vessel seal ledge and the embedment ring by circumferential fillet welds all around the reactor vessel. The support structure assembly functions as the load bearing assembly consisting of radial members around the annulus, resting on the reactor vessel flange and the embedment ring. The reactor cavity seal is shown in Figure 4.3-12.
The reactor cavity seal has multiple openings, which provide access to the ex-core nuclear instrumentation as well as ventilation for the reactor cavity cooling air. These openings have hinged cover plates, which are closed for flooding the transfer canal during refueling. O-rings are installed to provide watertight seal to prevent leakage into the reactor cavity. Prior to reactor operation, the hinged cover plates will be laid back to allow for ventilation of cooling air from the reactor cavity.
The cavity seal is designed to withstand the pressure loads from the refueling water as well as the motions of the reactor vessel and containment building due to seismic displacements. It can also accommodate axial and radial growth from the normal and transient thermal conditions of the reactor vessel. The cavity seal is also designed and tested to withstand loads imposed by a dropped fuel assembly. The cavity seal is designed for 80 heat up/cool down cycles and 50 cycles of maximum allowed water static head.
4.3-32 Rev. 35
MPS2 UFSAR Leak before break analysis is applied as the basis for design of the reactor cavity seal and neutron shielding. Compartmental pressurization due to reactor coolant loop rupture is excluded for the design of reactor cavity seal and the neutron shielding in accordance with Reference 3.A-29.
The support structure is fabricated from 300 series stainless steel conforming to ASME Section II Part A. The seal membrane is allowed to deflect such that it can rest on the support structure during flooding. The cavity seal membrane, although not required, is designed and analyzed to the guidelines of ASME B&PV Code Section III, Appendix XIII and ASME Section II, Parts A and C, 1995 Edition, through 1996 Addenda.
4.3-33 Rev. 35
MPS2 UFSAR TABLE 4.3-1 REACTOR VESSEL PARAMETERS Design Pressure, psig 2485 Design Temperature, °F 650 Nozzles Inlet (4 each), inches 30 Outlet (2 each), ID inches 42 CEDM (69), ID, inches 2.718 Instrumentation (8), nominal, inches 4 5/8 Vent (1), nominal, inches 0.75 Dimension Inside Diameter, nominal, inches 172 Overall Height, Including CEDM Nozzles, inches 503.75 Height, Vessel Without Head, inches 408-9/16 Wall Thickness, minimum, inches 8-5/8 Upper Head Thickness, minimum inches 7-3/8 Lower Head Thickness, minimum inches 4-3/8 Cladding Thickness, Replacement Closure Head, inches nominal 0.25 Cladding Thickness, Replacement Closure Head, inches minimum after machining 1/8 Cladding Thickness, Bottom Head, minimum 3/16 Cladding Thickness, Remainder of vessel, minimum, inches 1/8 Material Shell/Bottom Head SA-533-65 Grade B, Class 1 Steel Closure Head SA 508 Grade 3 Class 1 Carbon Steel Forgings A-508-64, Class 2 Cladding Stainless Steel (1) and NiCrFe Alloy (1)Weld deposited austenitic stainless steel with a composition approximately equivalent to SA-240, type 304 in contact with coolant.
4.3-34 Rev. 35
MPS2 UFSAR CEDM Nozzles Ni-Cr-Fe Alloy welded to SA-182, F316LN Instrumentation Nozzles Ni-Cr-Fe Alloy welded to SA-182, F316LN Dry Weights Closure Head lb. 147,900 Vessel, without flow skirt, lb. 682,000 Studs, Nuts and Washers, lb. 38,900 Total lb. 878,900 Volumes Bottom of Core, ft3 1113.11 Center of Core, ft3 1680.93 Top of Core, ft3 2248.74 Full Vessel, ft3 4651.27 4.3-35 Rev. 35
MPS2 UFSAR TABLE 4.3-2 STEAM GENERATOR PARAMETERS Number 2 Type Vertical U-Tube Number of Tubes (Design/Actual ) 8523 Tube Outside Diameter, inches 0.750 Heat Transfer Rate, each, Btu/hr 4.63 x 109 Nozzles and Manways Primary Inlet Nozzle (1 each), ID, inches 42 Primary Outlet Nozzle (2 each), ID, inches 30 Steam Nozzle (1 each), ID, inches 34 Feedwater Nozzle (1 each), nominal, inches 18 Instrument Taps (12 each), nominal, inches 1 Primary Manways (2 each), ID, inches 18 Secondary Manways (2 each), ID, inches 16 Secondary Handhole (4 each), ID, inches 8 Bottom Blowdown (2 each), nominal, inches 4 Nitrogen Addition (1 each), nominal, inches 1 Wet Layup (1 each), nominal, inches 2 Primary Side Design Design Pressure, psig 2485 Design Temperature, °F 650 Design Thermal Power (NSSS), MWt 2715 Coolant Flow (Each), lb/hr 74 x 106 Normal Operating Pressure, psia 2250 Coolant Volume, each, ft3 1693 Secondary Side Design Design Pressure, psig 1000 Design Temperature, °F 550 Normal Operating Steam Pressure, psia 880, Full Load Normal Operating Steam Temperature, °F 530, Full Load Blowdown Flow, Design, Maximum, Each, lb/hr 112,000 4.3-36 Rev. 35
MPS2 UFSAR Steam Flow, Each, lb/hr 5.9 x 106 Steam Moisture Content, Maximum, percent 0.20 Feedwater Temperature, °F 435 Number of Steam Primary Separators, each Steam Generator 170 Number of Secondary Separators, each Steam Generator 170 Dimensions Overall Height, Including Support Skirt, inches 749 Upper Shell Outside Diameter, inches 239.75 Lower Shell Outside Diameter, inches 166 Weights Dry, lb. 1,070,400 Flooded, lb. 1,666,600 Operating, lb. 1,283,000 4.3-37 Rev. 35
MPS2 UFSAR TABLE 4.3-3 MAIN STEAM SAFETY VALVE PARAMETERS Main Steam Piping Design Pressure, psig 1,100 (NOTE)
Main Steam Piping Design Temperature, °F 600 Fluid Saturated Steam Valve Number Set Pressure psia Capacity lb/hr (each valve) 1, 2 1000 794,060 3, 4 1005 794,060 5, 6 1015 794,060 7, 8 1025 794,060 9, 10 1035 794,060 11, 12 1045 794,060 13, 14, 15, 16 1050 794,060 Total Capacity (16 valves) lb/hr 12,704,960 Material Body ASTM A105 Gr II Disc ASTM 565 Gr 616 or ASME SB-637 UNS N07750 Type 3 Trim ASTM A451 Gr CPF8 NOTE:ASME Section III Code requires pressure rise to be limited to no more than 10% above piping design pressure. Operability of the safety valves ensures that the main steam system pressure will be limited to within 110% of its design pressure. Design pressure for main steam safety valves - 1035 psig.
4.3-38 Rev. 35
MPS2 UFSAR TABLE 4.3-4 TECH PUB REVIEW PKG FOR T4.3-4REACTOR COOLANT PUMP PARAMETERS Synchronous Speed, rpm 900 Type Vertical, Limited Leakage, Centrifugal Shaft Seals Type N-9000 Assembly Stationary Face Ring Carbon-Morganite CNFJ Rotating Face Ring Tungsten or Silicon Carbide Design Pressure, psig 2,485 Design Temperature, °F 650 Normal Operating Pressure, psig 2,235 Maximum Operating Temperature, °F 549 Design Flow, gpm 81,200 Total Dynamic Head, ft, Minimum 243 Maximum Flow (one-pump Operation), gpm 120,000 Dry Weight, lb. 168,050 Flooded Weight, lb. 175,050 Reactor Coolant Volume, ft3 per pump 112 Shaft Material ASTM A-182 Type F-304 Casing Material ASME SA-351 Gr CF8M Casing Wear Ring Material ASTM A-351 Gr CF8 Hydrostatic Bearing Bearing Material ASTM A-351 Gr CF8 Journal Material ASTM A-351 Gr CF8 Motor Voltage, volts (source) 6,900 Voltage, volts (rated) 6,600 Frequency, Hz 60 Phase 3 Horsepower (rated)/rpm 6,500/887 Synchronous Speed, rpm 900 4.3-39 Rev. 35
MPS2 UFSAR Instrumentation Quantity (per pump)
Seal Temperature 1 Pump Casing Differential Temperature 1 Seal Pressure 3 Controlled Bleed off Flow 1 Controlled Bleed off Temperature 1 Motor Oil Level 2 Motor Bearing Temperature 5 Motor Stator Temperature
- 6 Reverse Rotation Flow 1 Vibration Monitoring System *** 5 Oil Lift Pressure 1 Lubrication Oil Temperature 3 Total Seal Assembly Leakage (Normal and Stand-by Operation)
Three Pressure Seals Operating, gpm **
Two Pressure Seals Operating, gpm **
One Pressure Seal Operating, gpm **
- NMAC, Main Coolant Pump Seal Maintenance Guidelines, Final Report-December 1993 can be used to calculate these volumes more accurately at different conditions.
- Vibration Monitoring System consists of two (2) velomitors on the motor casing, and two (2) proximity probes and one (1) key phasor on the pump shaft.
4.3-40 Rev. 35
MPS2 UFSAR TABLE 4.3-5 REACTOR COOLANT PIPING PARAMETERS Number of loops 2 Flow per loop, lb/hr 61 x 106 Pipe Size Reactor outlet, ID, inches 42 Reactor inlet, ID, inches 30 Surge line, nominal, inches 12 Design Pressure, psig 2485 Design Temperature, °F 650 Velocity, Hot leg, ft/sec 40.4 Velocity, Cold leg, ft/sec 36.3 4.3-41 Rev. 35
MPS2 UFSAR TABLE 4.3-6 PRESSURIZER PARAMETERS Design Pressure, psig 2,485 Design Pressure, °F 700 Normal Operating Pressure, psia 2250 Normal Operating Temperature, °F 653 Internal Free Volume, ft3 1500 Normal Operating Water Volume, Full Power, ft3 800 Normal Steam Volume, Full Power, ft3 700 Installed Heater Capacity, kW 1600 (Note: Total Heater Capacity may be less due to Heater unavailability)
Spray Flow, Maximum, gpm 375 Spray Flow, Continuous, gpm 1.5 Nozzles Surge Line (1) nominal, inches 12 Safety Valves (2) nominal, inches 4 Relief Valve (1) nominal, inches 4 Spray (1) nominal, inches 4 Heater Sleeve (60) ID, inches 0.905 Manual Vent (1) nominal inches Manway nominal, inches 16 Alternate Vent Port nominal, inches 6.5 Instrument Nozzles Level (4) nominal, inches 1 Temperature (2) nominal, inches 1 Pressure (2) nominal, inches 1 Materials Vessel SA-508 Grade 3, Class 2 Cladding - Cylinder Shell, Upper and Lower Head Type 308 Stainless Steel (1) 4.3-42 Rev. 35
MPS2 UFSAR Dimensions Overall Length, inches (bottom of support skirt to tip of relief nozzle) 434.06 Outside Diameter, inches 106.56 Inside Diameter, inches (with cladding) 96.16 Cladding Thickness, inches (minimum) 1/8 Dry Weight, Including Heaters, lb. 202,731 Flooded Weight, Including Heaters, lb. 297,433 (1)Weld deposited austenitic stainless steel in contact with coolant.
4.3-43 Rev. 35
MPS2 UFSAR TABLE 4.3-7 QUENCH TANK PARAMETER Design Pressure, psig 100 INT/15 EXT Design Temperature, °F 350 Normal Operating Pressure, psig 3 Normal Operating Temperature, °F 120 Internal Volume, ft3 217 Normal Water Volume, ft3 135 Normal Gas Volume, ft3 82 Blanket Gas Nitrogen Nozzles Pressurizer discharge (1), inch, nominal 10 Demineralized water (1), inch, nominal 2 Rupture Disc (1), inch, nominal 18 Drain (1), inch, nominal 3 Temp. Instrument (1), inch, nominal 1 Level Instrument (1), inch, nominal 1 Pressure and Level Instrument (1) inch, nominal 1 Vent (1), inch., nominal 1.5 Vessel Material ASTM-A-240 TP 304 Dimensions Overall Length, inches 145.5 Outside Diameter, inches 60 Dry Weight, lb. 4600 Flooded Weight, lb. 18,120 4.3-44 Rev. 35
MPS2 UFSAR TABLE 4.3-8 PRESSURIZER SPRAY (RC-100E, RC-100F) VALVE PARAMETERS Service - Pressurizer Spray Control Design Temperature, °F 650 Design Pressure, psig 2485 Flow, gpm 440 Pressure Drop, psi 8.5 - 40 Failure Position Failed Closed Manufacturer Fisher Controls Co.
Design Code Pump and Valve Code, Nov. 1968 Draft, Class I Seismic Class I Materials Body 316 SST ASTM A351-CF8M TABLE 4.3-9 POWER-OPERATED RELIEF VALVE ISOLATION VALVE PARAMETERS (RC-403, RC-405)
Service - Pressurizer Power-Operated Relief Valve Isolation Design Temperature, °F 675 Design Pressure, psig 2,485 Actuator Electric Motor Failure Position As Is ANSI Class 2,500 lb Manufacturer Velan Valve Company Design Code Pump and Valve Code Nov. 1968 Draft, Class I Seismic Class I Materials Body ASTM A182 Grade F316 4.3-45 Rev. 35
MPS2 UFSAR TABLE 4.3-10 PRESSURIZER POWER-OPERATED RELIEF VALVE PARAMETERS (RC-402, RC-404)
Design Pressure, psig 2485 Design Temperature, °F 675 Fluid Saturated Steam 0.1% (wt) Boric Acid Number 2 Capacity, lb/hr (minimum) each 153,000 Type Solenoid Operated Set Pressure, psig 2,385 and 400 psig (low temperature overpressurization)
Failure Position Closed Design Code ASME Section III, 1977 Edition through Winter 1979 Addenda Materials Body 316L SS, SA182 4.3-46 Rev. 35
MPS2 UFSAR TABLE 4.3-11 PRESSURIZER SAFETY VALVE PARAMETERS (RC-200, RC-201)
Design Pressure 2,485 Design Temperature, °F 675 Fluid Saturated Steam, 0.1% (wt) Boric Acid Set Pressure RC-200, psig 2,485 RC-201, psig 2,485 Capacity, lb/hr, at set pressure RC-200 294,000 RC-201 294,000 Type Spring loaded-balances bellows, enclosed bonnet Accumulation, % 3 Back pressure Compensation Yes Blowdown, % 12 Design Code ASME Section III, Class A, 1968 Edition, Addenda through Summer of 1970, Code Case 1344-1 Materials Body 316 SST, ASTM A 182 4.3-47 Rev. 35
MPS2 UFSAR TABLE 4.3-12 ACTIVE AND INACTIVE VALVES IN THE REACTOR COOLANT SYSTEM BOUNDARY Classification Valve Type/ Active - A Post LOCA Line Number Inactive - I Normal Position Position Shutdown Cooling Motor / 2 A Closed Closed Charging a Air / 2 A Open / Closed Open / Closed Check / 2 A Open / Closed Open / Closed Letdown Air / 2 A Open Closed Manual / 1 I Open Open Auxiliary Spray Air / 1 I Closed Closed Check / 1 I Closed Closed Pressurizer Spraya Air / 2 I Open / Closed Closed Manual / 6 I Open Open Pressurizer Relief Motor / 2 I Open Open Solenoid / 2 I Closed Closed Pressurizer Safety 2 I Closed Closed Safety Injection Tank Motor / 4 I Open Open Check / 4 A Closed Open Leakage Control (SIS) Air / 4 I Closed Closed Safety Injection Check / 8 A Closed Open LPSI Header Check / 4 A Closed Open Motor / 4 A Closed Open HPSI Header Check / 8 A Closed Open Motor / 8 A Throttled Open Open Drain: Reactor Manual / 13 I Closed Closed Coolant Loop Air / 1 I Open Open Charging Manual / 4 I Closed Closed Pressurizer Spray Manual / 4 I Closed Closed Letdown Manual / 4 I Closed Closed 4.3-48 Rev. 35
MPS2 UFSAR TABLE 4.3-12 ACTIVE AND INACTIVE VALVES IN THE REACTOR COOLANT SYSTEM BOUNDARY Classification Valve Type/ Active - A Post LOCA Line Number Inactive - I Normal Position Position Safety Injection Manual / 14 I Closed Closed Auxiliary Spray Manual / 4 I Closed Closed Shutdown Cooling Manual / 2 I Closed Closed Vent / Test: Reactor Manual / 2 I Closed Closed Vessel Vent / Test: Manual / 2 I Closed Closed Pressurizer Vent / Test: Manual / 3 I Closed Closed Pressurizer Spray Vent / Test: Letdown Manual / 3 I Closed Closed Vent / Test: Charging Manual / 4 I Closed Closed Vent / Test: Safety Manual / 10 I Closed Closed Injection Vent / Test: Auxiliary Manual / 2 I Closed Closed Spray Sampling Manual / 3 I Open Open Shutdown Cooling 1 I Closed Closed Relief
- a. Valves may be open or shut during normal operation or postincident.
4.3-49 Rev. 35
MPS-2 FSAR FIGURE 4.3-1 REACTOR VESSEL CEOM NOZZLES (e" REQ'O)
UFTING LUG (I RE~'D.)
1N.~VLA\"! ON WPfl'ORT RINS ~~TED INTO VfEW OUTl.ET NJZZlE INLET NOlZl £ (4 REQ'.O) r A
A SURVEILLANCE SAMPlE. TU8E (Go ftF.:Q'O)
VESSEL VESSEl.
172." lO, MIN. - - - - SUPPOR,,.
(aREQ'D)
CORE STABILIZING lLG (' REQ'C)
CORE SlOP lUG CORE. S10P JP===-=_ _-I(9 REQ"O) )' LU~ (~ R,Eq'O)
OUTlET NOZZlE (Z RictO) lif;CTION A-A
. 4j- ~IN FLO\<<{ BAFFLE
~~+/-:z~::;7-~:..a'(trW'f) CLAO JUN 10 1982
MPS-2 FSAR FIGURE 4.3-2 STEAM GENERATOR Integral Steam Restrictor Improved Steam Separation Equipment Feedwater Nozzle and Pipe Thermal Sleeve Low Cobalt Tubing (0.015%)
and Cladding (0.1 %)
High Capacity Slowdown (7% ) Wide Range Water Level Indicator Enlarged Handholes and Secondary Shell Drain Manways Tubesheet Marking Polished Cladding MAY 1994
MPS-2 FSAR FIGURE 4.3-3 REACTOR COOLANT PUMP r-------
I
~~-
~~-......-~1
- I R15~
Vapor Driver Seal Mount Drain Controlled Bleed-Off
.U Closure Stud Pump Case JULY 1998
MPS2 UFSAR FIGURE 4.3-4 P&ID REACTOR COOLANT PUMP The figures indicated above represents an engineering controlled drawing that is Incorporated by Reference in the MPS-2 FSAR. Refer to the List of Effective Figures for the related drawing number and the controlled plant drawing for the latest revision.
4.3-53 Rev. 35
MPS-2 FSAR FIGURE 4.3-5 REACTOR COOLANT PUMP SEAL AREA Seat Stationary Fac Seal Rotating Face Pressu re Connection Cooling Water Upper Seal Outlet TEMPERATURE v1 U
Cooling (
SENSING ELEMENT H Water 1nlet Connection
\1 Outer TUbe, 1JO.-~r~ n--~ Controlled
-Bleed-Off Cooljng Water Pressu re Connection
...,~~o Middle and Vapo rYlSeai
~~~~~controlled Bleed-Off
~~ Labyrinth Passages INNER GASKET LEAK-OFF Inner Juoo,-
Inner TUbe, . Recircuiatlng Controlled Lower Seal Bleed-Off Fluid JULY 1998
MPS-2 FSAR FIGURE 4.3-6 REACTOR COOLANT PUMP PREDICTED PERFORMANCE NPSH in Feet of Water 400 300 Efficiency Total Percent Head 200 90 in Feet
% Pump Eft. 100 ~
0 70 60 50 t1) 30 B. H. P. at SP. GR. = 1. 0 20 10 B. H. P. at SP. GR. =0.76 t- 2000 0
~ 20 40 60 80 100 120 ': 140
.... Thou sand Gallons per Minute
~
m JUN 10 1982
MPS-2 FSAR FIGURE 4.3-7 PRESSURIZER LEVEL NOZZLE r-LEVEL NOZZLE SPRA Y NOZZLE 270' f 30'
-r 90'
/ / I
/RELlEF NC?,~ZLE ( leo'
/ /1 0 ~><
SAFETY NOZZLE'"
1800
~ TEMP NOZZLE BQTTOM VIEW 180 0 I
i o i 0 395.75" i o o i RS 60 ELECTRiC HEATE o I o o i : 00 o 0 i 0 0 o.
°0 i.
o0 o 0 _
TEMP NOZZLE 0
o
- 0 *
- _ 0 _ ._.* _.~. _
).- - 270' *. _._ _ ........!.... _. 0 0 90 I .° o.
0
.0.
o rL---~-_~
0 0 0 o 0 - ! 0 0 o
00...0-_-"-
0 I'":
_.. ,.. ZLE o i LEVEL NOZ I
IN; S6" SURGE NOZZLE
~_~~.O~
( ~ 00
. ." 0 0"
SUPPOR'r SKIRT
-- ~
MPS-2 FSAR FIGURE 4.3-8 TEMPERATURE CONTROL PROGRAM 600 590 Thot*
592.8 580 570 Tavg*
568.9 560 550 Reactor Coolant Temperatures (degree F)
Tcold 540 545.0 532 530 0 10 20 30 40 50 60 70 80 90 100 Reactor Power (100 Percent = 2700 MWt)
- Temperatures are based on a best estimate RCS flow rate of approximately 389,900 gpm Rev. 24.2
MPS-2 FSAR 70 FIGURE 4.3-9 PRESSURIZER LEVEL SETPOINT PROGRAM 65 60 55 50 Pressurizer Level (%)
45 40 35 530 535 540 545 550 555 560 565 570 575 RCS Average Temperature (degrees F)
Rev. 24.2
MPS-2 FSAR FIGURE 4.3-10 PRESSURIZER LEVEL CONTROL PROGRAM Nominal letdown is 40 GPM to maintain level with continuous charging pump operation (1) First charging pump chosen as backup 40 (2) Second charging pump chosen as backup (if available)
" (3) High level error alarm (4) Low level error alarm and backup signal to start all charging pumps, stop backup charging pumps (5) All pressurizer heaters and backup signal to stop backup charging pumps (1) (2) 30 -(2) Oft (I)
On On Off 1-0 I-C LLJ o
0-Q)
Q)
<l>
20 V) ...J
.c.
.r=.Q)
Q,)-
.-en
<.J> :I:
c..5 (4) f 10 La oLa
-10 Oft On Lr..J (5) (5)
Q.)
Q.)
....J 1 2 3 4" 5 Ou1put SignaJ From Proportiona I Controller
MPS-2 FSAR FIGURE 4.3-11 QUENCH TANK ressu ri~~;RESSURE AND LEVEL TAP l Une Inlet 1-112 Vent 11
. Rupture Disc Relief """r----------l 145-112" \ iI
~
2(1 Demin.
Water Inlet 3" Drai n I" Temp Probe j 1" LEVEL TAP MAY 1998
MPS-2 FSAR FIGURE 4.3-12 PERMANENT REACTOR CAVITY SEAL PLATE Cavity Seal Membrane r Radial Restraint
/ _ Reactor Vessel
,I Support Plate Assembly -, ..: Head
\
Concrete .J
'- Cavity Liner Embedment Ring ..J
\. Reactor Vessel Seal Ledge Section A-A Seal Membrane
~ Hatch
\\
\
\
0 \
180 A
MPS2 UFSAR 4.4 MATERIALS COMPATIBILITY 4.4.1 MATERIALS EXPOSED TO COOLANT The materials exposed to the reactor coolant have shown satisfactory performance in operating reactor plants. A listing of materials is given in Table 4.4-1.
4.4.2 INSULATION Piping and equipment are insulated with granular-type, reflective-type and NUKON fiberglas-type material compatible with the temperature and functions involved. All insulation material used on stainless steel has a low (< 600 ppm) soluble chloride content to minimize the possibility of chloride induced stress corrosion. Removable metal reflective-type thermal insulation is provided on weld areas of the reactor coolant system subject to inservice inspection. The replacement pressurizer is entirely covered with reflective metallic insulation, taking into consideration the containment sump clogging concerns as detailed in NRC Regulatory Guide 1.82. The chemical makeup of the insulation conforms to NRC Regulatory Guide 1.36.
Nonremovable metal reflective-type thermal insulation is provided on the reactor cavity wall. The primary channel heads of the two steam generators are covered with the NUKON fiberglas-type material.
Removable blanket insulation is provided on the CEDM, instrumentation nozzle areas of the replacement reactor vessel head. Interconnected rigid panel insulation covers the lower portion of the head and the head flange for easy removal.
The thickness of insulation is such that the exterior surface temperature is not higher than approximately 50°F above the maximum containment ambient (120°F). All insulation support attachments are attached prior to final stress relief.
The possibility of leakage of reactor coolant onto the reactor vessel head or other part of the reactor coolant pressure boundary causing corrosion of the pressure boundary has been investigated by Combustion Engineering (CE).
Detailed laboratory examinations have shown that:
- a. Reactor coolant (containing boric acid) alone, at temperatures greater than about 250°F, does not result in significant corrosion of low alloy steels. Therefore, under normal operating conditions, corrosion of the pressure boundary is not a concern.
Below this temperature, boric acid solutions can result in significant corrosion.
This corrosion is controlled with an aggressive preventative maintenance program and procedures to evaluate all unidentified reactor coolant leakage.
- b. Boric acid solutions dripped through the calcium silicate insulation to be used on this plant do not initiate attack.
4.4-1 Rev. 35
MPS2 UFSAR The results of these tests have therefore shown that reactor coolant system leakage onto surfaces of the reactor coolant pressure boundary will not affect the integrity of the pressure boundary when calcium silicate insulation, NUKON fiberglas-type insulation or metal reflective-type insulation is used.
4.4.3 COOLANT CHEMISTRY Control and variation of the reactor coolant chemistry is a function of the chemical and volume control system. Sampling lines are provided from the reactor coolant piping to provide a means for taking periodic sample of the coolant for chemical analysis. Table 4.4-2 contains the Reactor Coolant Chemistry parameters and limits listing. The water chemistry is maintained as follows:
At temperatures below 250°F, no upper limit on dissolved O2 is specified.
- 1. Hydrazine should only be added during subcritical heatup at 1.5 times the measured oxygen concentration.
- 2. Consistent with concentration of additives.
All wetted surfaces in the reactor coolant system are compatible with the above water chemistry.
4.4-2 Rev. 35
MPS2 UFSAR TABLE 4.4-1 MATERIALS EXPOSED TO COOLANT Reactor Replacement Closure Head Cladding Weld Deposit Type 309 SS (layer 1)
Type 308 SS (subsequent layers)
Vessel Cladding Weld Deposited Type 308 SS
- Vessel Internals 304 SS and Ni-Cr-Fe Alloy Fuel Cladding Zircaloy-4 Control Element Drive Mechanisms Ni-Cr-Fe Piping Base Metal SA 516 Gr 70 Carbon Steel **
Piping Cladding Austenitic Stainless Steel Type 304 L Steam Generator Bottom Head Cladding Weld Deposited Type 308 SS
- Tube Sheet Cladding Weld Deposited Ni-Cr-Fe Alloy Tubes Ni-Cr-Fe Alloy Pumps Casing Austenitic Stainless Steel, Type 316 Internals Austenitic Stainless Steel, Type 316 and Type 304 Pressurizer Cladding
- Cylinder Shell, Upper and Lower Head Weld Deposited Type 308 and 309 SS
- Weld Deposited Austenitic Stainless Steel in contact with coolant.
- Piping Base Material is exposed on instrument nozzles that have been subjected to a half nozzle replacement.
4.4-3 Rev. 35
MPS2 UFSAR TABLE 4.4-2 REACTOR COOLANT CHEMISTRY PARAMETER REACTOR COOLANT LIMITS Suspended Solids, ppm maximum 0.35 prior to reactor startup pH at 25°F Determined by the concentration of boric acid and lithium present. Consistent with the Primary Chemistry Control Program. (a)
Chloride, ppm Cl-, maximum 0.15 Fluoride, ppm F-, maximum 0.10 Hydrogen as H2, cc (STP)/Kg H2O 25-50 Dissolved O2, ppm maximum 0.1 (b) (c) (d)
Lithium as Li7, ppm Consistent with the Primary Chemistry Control Program (a)
Boron, ppm 0-2620 (e)
Conductivity, S/cm at 25°C Relative to Lithium and Boron concentration (a) During power operation lithium is coordinated with boron to maintain a pH(t) of 7.0, but 7.4, consistent with the Primary Chemistry Control Program. Lithium is added to the RCS during plant startup, but prior to reactor criticality, and is in specification per the Primary Chemistry Control Program within 72 hours8.333333e-4 days <br />0.02 hours <br />1.190476e-4 weeks <br />2.7396e-5 months <br /> after criticality. Lithium may be removed from the reactor coolant immediately before, or during, shutdown periods to aid in the cleanup of corrosion products. By evaluation, a maximum lithium concentration of 4.5 ppm is permissible with a target lithium concentration of 4.3 ppm for 100% power operations.
(b) The temperature at which the Oxygen limit applies is > 250°F.
(c) The at power operation residual Oxygen concentration control value is 0.005 ppm.
(d) During plant startup, Hydrazine may be used to control dissolved Oxygen concentration at 0.1 ppm.
(e) RCS boron concentration is maintained as necessary to ensure core reactivity or shutdown margin requirements are met. Although the RCS and related auxiliary systems containing reactor coolant are designed for a maximum concentration of 2620 ppm boron, it should be noted the design basis for the TSP baskets in the containment sump assumes the RCS, SITs, and RWST are at a maximum boron concentration of 2400 ppm.
4.4-4 Rev. 35
MPS2 UFSAR 4.5 SYSTEM DESIGN EVALUATION 4.5.1 PREVENTION OF BRITTLE FRACTURE To protect against non-ductile failure, the requirements of 10 CFR 50 Appendix G have been implemented and the requirements of 10 CFR 50.61 have been satisfied.
10 CFR 50 Appendix G provides fracture toughness requirements which ensure sufficient margins of safety against non-ductile failure during normal operation, including anticipated operational occurrences and inservice hydrostatic tests. The requirements of this Appendix are implemented by Figure 4.5-4 which provides maximum heatup and cooldown rates for the reactor coolant system and maximum reactor coolant system pressure (as indicated by pressurizer pressure) as a function of reactor vessel inlet temperature. Additional discussions addressing the development of these limits are provided in Sections 4.5.1.2 and 4.5.1.3.
10 CFR 50.61 provides additional fracture toughness requirements to protect against non-ductile failure of the reactor vessel during pressurized thermal shock (PTS) events. Compliance with these requirements is demonstrated by ensuring that the end-of-life reference temperature (RTPTS) for the reactor vessel beltline materials stays below the established limits using the prescribed methods. Additional discussion addressing 10 CFR 50.61 is provided in Section 4.5.1.4.
4.5.1.1 Initial Nil-Ductility Transition Reference Temperature.
The original design requirements for carbon and low alloy materials which form the pressure boundary of the reactor coolant system (RCS) have impact properties which meet the requirements of paragraph N-330 of the Summer 1969 ASME Boiler and Pressure Vessel Code,Section III, at 40°F or less.
To address changes in regulations and demonstrate compliance with 10 CFR 50 Appendix G and 10 CFR 50.61 requirements, the original design requirements of N-330 were supplemented and the materials initial Nil-Ductility Transition Reference Temperature (RTNDT) were subsequently established.
The impact properties for the replacement reactor vessel closure head meet the requirements of Article NB 2331 of the ASME B&PV Code,Section III, 1998 Edition through 2000 Addenda.
Reference temperature RTNDT of - 40°F was established in accordance with SA 508 Supplementary Requirement (S10) and NB 2300.
The replacement reactor vessel closure head and the replacement pressurizer were evaluated for protection against non-ductile failure in accordance with the methodology presented in ASME Section III, Appendix G for Class 1 components. The maximum stress intensity factors for the transients meet the fracture toughness requirements of ASME Section III Appendix G for a postulated defect of 1/10th thickness of the reactor vessel head and 1/4th thickness of the pressurizer.
4.5-1 Rev. 35
MPS2 UFSAR In the case of the replacement steam generators, the materials were required to satisfy the requirements of ASME,Section III, 1983 Edition through the Summer 1984 Addenda, Article NB-2331, and establish a maximum RTNDT at a temperature of 0°F.
4.5.1.2 Nil-Ductility Transition Reference Temperature Shift The flux of fast neutrons at the reactor vessel wall is governed by the reactor core load design, arrangement of the reactor internals and average power levels, among other factors. The integration of this flux over time, called fluence, is monitored by dosimetry materials included in the surveillance capsules located near the vessel inner wall. In the time since original plant startup the thermal shield has been removed and the core load design has changed. In addition, small crack-arresting holes have been drilled in the core barrel, affecting the flux for one vessel plate.
Based on results from surveillance capsule dosimetry retrieved through cycle 14, the known configuration history, neutron flux modeling calculations described below, and further assuming future reactor operation with the low leakage design at 2700 Mwt and 90 percent plant capacity factor, the maximum fluence at the end of the period of extended operation of 60 years will be approximately 3.83 x 1019 n/cm2 (E > 1Mev). These fluence estimates are fully described in Reference 4.5-2. The following summary describes the key methods of the referenced analysis.
Discussion of Fluence Calculations The prediction of neutron fluence at various locations was based on an analysis of neutron transport for given configurations and source developed to model the reactor. To further refine the model accuracy, the results of the fluence analysis were correlated with measurements of actual fluence based on dosimetry retrieved from surveillance capsules. Estimations of future fluence are then based on a combination of the currently measured fluence and the extrapolation of calculated cycle 14 flux though the end of licensed plant life. Thus, it is assumed there will be no significant change to reactor configuration or core load design.
The three dimensional discrete ordinates transport computer code DORT was used in the surveillance capsule W-83 analysis to model neutron transport within the reactor. The code results describe the space and energy dependent neutron flux present in the reactor.
The reactor was modeled as a 1/8th segment of the core, the reactor internals, core barrel, thermal shield (through cycle 5), explicit representations of the surveillance capsules at 6° and 14°, the pressure vessel cladding and vessel wall, the insulation external to the pressure vessel, the primary biological cladding and shield wall.
Note that a variation of this model, in which material composition of the surveillance capsules was redefined as water, was utilized to determine the maximum neutron exposure at the pressure vessel wall in octants of the core that do not contain surveillance capsules.
The actual activation or fission measured for the retrieved capsule dosimetry was compared to the calculated activation. The ratio of measured to calculated activation, M/C, was determined to fall well within the criteria specified in Regulatory Guide 1.190.
4.5-2 Rev. 35
MPS2 UFSAR Shift Prediction The shift prediction methodology for the determination of the adjusted reference temperature (ART) is done in accordance with Revision 2 to Regulatory Guide 1.99 (dated May 1988). The ART, for each material in the beltline is given by the following expression:
ART = Initial RTNDT + RTNDT + Margin The shift in RTNDT is based on fluence predictions, described above, for the time period corresponding to 54 EFPY. Table 4.6-13 provides the results of the calculation.
4.5.1.3 Operational Limits All components in the RCS are designed to withstand the effects of cyclic loads due to RCS temperature and pressure changes. These cyclic loads are introduced by normal unit load transients, reactor trips and startup and shutdown operation.
During unit startup and shutdown, the rates of temperature and pressure changes are limited. The design number of cycles for heatup and cooldown is based upon a rate of 100°F/hr and for cyclic operation.
The maximum allowable RCS pressure at any temperature is based upon the stress limitations for brittle fracture considerations. These limitations are derived by using the rules contained in Section III of the ASME Code including Appendix G, Protection Against Nonductile Failure and the rules contained in 10 CFR 50, Appendix G, Fracture Toughness Requirements.
FSAR Figures 4.5-4 and 4.5-5 provide the RCS pressure-temperature limitations during plant heatup and cooldown. Figures 4.5-4 and 4.5-5 are valid for the period up to and including fifty four years of full power integrated neutron flux, as determined using the rationale of Section 4.5.1.2, and was developed using the rules of Appendix G, Protection Against Nonductile Failure of the ASME Boiler and Pressure Vessel Code,Section XI, 2002 Addenda.
Using these rules the belt line material of the reactor vessel is established as the controlling component section throughout plant life. This established an upper boundary on RCS pressure as a function of RCS temperature and allowable heatup and cooldown rates to ensure prevention of nonductile failure.
The limitations for normal heatup and cooldown rates and the applicable temperature ranges are summarized in Table 4.5-2.
The RCS pressure-temperature limits provided by Figures 4.5-4 and 4.5-5 have been corrected to indicated pressurizer pressure versus indicated cold leg temperature.
Indicated cold leg temperature is the best available indication of the reactor vessel downcomer temperature and will normally be monitored as RCS cold leg temperature when reactor coolant pumps are operating or natural circulation is occurring. In the instances where the shutdown cooling (SDC) system is operating without RCPs, the SDC system return temperature will be 4.5-3 Rev. 35
MPS2 UFSAR used. Appropriate corrections which account for dynamic flow losses, static elevation differences and instrumentation uncertainties have been applied.
Also shown is an allowable region for shutdown cooling system operation. This region is established based upon the design pressure-temperature ratings of components of the shutdown cooling system and the normal operation of this system as described in Chapter 6 (Section 6.3) and Chapter 9 (Section 9.3).
The reactor vessel beltline material consists of six plates. The NDT temperatures (TNDT) of each plate was established by drop weight test (DWT). Charpy tests were then performed to determine at what temperature the plates exhibited 50 ft-lbs absorbed energy and 35 mils lateral expansion.
(Data points were based on average of three specimens.)
Similar testing was not performed on all remaining material in the RCS. However, sufficient impact testing was performed to meet appropriate design code requirements and a conservative RTNDT of 50°F has been established for longitudinal direction.
As a result of fast neutron irradiation in the region of the core, there will be an increase in the RTNDT with operation. The techniques used to predict the integrated fast neutron (E 1 Mev) fluxes of the reactor vessel are described in Section 4.5.1.2 of the FSAR.
Since the neutron spectra and flux measured at the samples and reactor vessel inside radius should be nearly identical, the measured reference transition temperature shift for a sample can be applied to the adjacent section of the reactor vessel for later stages in plant life equivalent to the difference in calculated flux magnitude. The maximum exposure of the reactor vessel will be obtained from the measured sample exposure by application of the calculated azimuthal neutron flux variation.
The actual shift in RTNDT will be established periodically during plant operation by testing of reactor vessel material samples which are irradiated cumulatively by securing them near the inside wall of the reactor vessel as described in Section 4.6.3 and shown in Figure 4.6-1 of the FSAR. To compensate for any increase in the RTNDT caused by irradiation, limits on the pressure-temperature relationship are periodically changed to stay within the stress limits during heatup and cooldown.
In addition to the requirements provided by ASME Section XI, Appendix G and 10 CFR 50, Appendix G, the following items were also considered in the development of the RCS pressure-temperature limits provided by Figures 4.5-4 and 4.5-5.
Lowest Service Temperature - As indicated previously, an RTNDT for all material with the exception of the reactor vessel beltline was established at 50°F. ASME III, Art. NB-2332(b) requires a lowest service temperature of RTNDT + 100°F for piping, pumps and valves. Below this temperature a pressure of 20 percent of the system hydrostatic test pressure cannot be exceeded.
4.5-4 Rev. 35
MPS2 UFSAR
- a. Maximum Pressure for Shutdown Cooling - This pressure is established by considering the design pressure of the shutdown cooling system, shutoff head of the Low Pressure Safety Injection (LPSI) pumps, elevation head from the pressurizer to the LPSI pumps, margin to SDC safety valve setpoints and the design temperature of the shutdown cooling system.
4.5.1.4 Pressurized Thermal Shock In accordance with 10 CFR 50.61, reactor pressure vessel belt line materials have been reviewed to establish a reference temperature for pressurized thermal shock (RTPTS). This review evaluated core loading patterns and the actual or best estimate of copper and nickel in the vessel material. In addition, the reactor vessel material composition and properties were compared to those of surveillance capsule materials from which actual tests and measurements were taken. A summary of this review is as follows:
- a. Copper/Nickel Content Best estimate copper/nickel content values for the Reactor Vessel Beltline Plates and welds are given in Table 4.6-12.
- Plates; Full chemistry results available for beltline plates.
- Welds; Where chemistry results were unavailable, nickel content was conservatively estimated using data available for the type of wire used.
- b. Core Configuration The neutron fluence values given in Table 4.6-12 have been used and have been calculated as described in Section 4.5.1.2. These end-of-life fluence values represent the most recent surveillance capsule (capsule W-83) evaluation.
Calculated RTPTS values have been obtained using the above assumptions. Table 4.6-12 provides the results of the calculations. This table will be updated whenever changes in core loadings, surveillance measurements, or other information indicate a significant change in the RTPTS projected values, as required by 10 CFR 50.61(b)(1). The values that were calculated do not exceed the RTPTS screening criteria of 270°F for plates, forgings, and axial weld materials, and 300°F for circumferential weld materials at 54 effective full power years.
4.5.2 SEISMIC DESIGN The nuclear steam supply system (NSSS) is designed to withstand the loads imposed by the maximum hypothetical accident and the maximum seismic disturbance without loss of functions required for reactor shutdown and emergency core cooling. The method of combining stresses produced by these simultaneous conditions is described in Section 4.2.1.
4.5-5 Rev. 35
MPS2 UFSAR A seismic analysis of the RCS is given in Appendix 4.A.
The RCS components are considered Class 1 for seismic design. Loadings which result from earthquake conditions are categorized and, in combinations with other specified loadings, are evaluated in accordance with the rules of ASME Boiler and Pressure Vessel Code,Section III.
- a. Operating Basis Earthquake (OBE) - The OBE condition is categorized as an upset condition. In evaluations using normal and upset conditions, loadings resulting from the OBE shall be considered to occur during normal operation at full power.
200 cycles of the OBE have been specified in the system design. The procedure used to account for the number of earthquake cycles during one seismic event includes consideration of the number of significant motion peaks expected to occur during the event. The number of significant motion peaks during one seismic event would be expected to be equivalent in severity to no more than 40 full load cycles about a mean value of zero and with an amplitude equal to the maximum response produced during the entire event. Based upon this consideration and the assumption that seismic events equivalent to 5 OBEs will occur during the life of the plant, Category I systems, components and equipment are designed for a total of 200 full load cycles.
- b. Design Basis Earthquake (DBE) - Two faulted conditions, which include loadings resulting from the DBE, are defined.
- Loadings resulting from the combined effects of the DBE and normal operation at full power.
- Loading resulting from the combined effects of the DBE, normal operation at full power and pipe rupture conditions.
4.5.2.1 Piping The primary stress limits applied in evaluating the emergency and faulted conditions for the RCS piping are specified as follows:
The RCS piping is designed in accordance with the requirements for Class I piping of ANSI B31.7, Code for Nuclear Power Piping. The primary stress limits of ANSI B31.7, Case 70, Design Criteria for Nuclear Power Piping Under Abnormal Conditions, are applied in evaluating the emergency and faulted conditions, except in the case of Faulted Condition (1) noted above in Section 4.5.2.b. In this case, the primary stress limits for emergency conditions (Case 70) are applied.
4.5.2.2 Vessels The primary stress limits applied in evaluating the emergency and faulted conditions for vessels in the RCS are specified as follows:
4.5-6 Rev. 35
MPS2 UFSAR The reactor vessel, steam generators and pressurizer were designed in accordance with the rules for Class A vessels of the ASME Boiler and Pressure Vessel Code Section III. The replacement steam generator subassemblies are designed in accordance with the rules of Class I vessels, ASME Section III. The primary stress limits of Section III, Paragraph N-417-10, Stress Limitations for Emergency Conditions, are applied in evaluating the emergency conditions and in evaluating Faulted Condition (1) noted above in Section 4.5.2.b.
With respect to Faulted Condition (2) in Section 4.5.2.b, the primary stress limits of Section III, N-417-11, Stress Limitations for Faulted Conditions, modified as follows, are applied.
- a. In lieu of the value suggested in N-417.11b, the yield strength value to be used in applying the limit analysis procedure will be equal to tabulated yield strength plus one-third of the difference between the tensile strength and the tabulated yield strength, with values taken at temperature.
- b. In the piping run within which a pipe break is considered to have occurred, the stress criteria for this condition need not be applied to the relevant nozzles or to the nozzle-vessel region within the limits of reinforcement given in N-454(a), except in the case of nozzles integral with component support assemblies. In the case of nozzles integral with component support assemblies, the criteria is applicable in all regions which sustain support reactions.
The replacement reactor vessel closure head is designed in accordance with ASME Section III, Class 1 vessels, 1998 Edition through 2000, Addenda. The primary stress limits of Section III, NB 3225 Appendix F, F-1331.1 (a, b and c) are applied in evaluating the faulted conditions (Table 4.2-2B). The load combination for the faulted condition (Service Level D) is defined in Section 4.5.2.b. DBE and LOCA loads are combined using the Square Root Sum of Squares (SRSS) method for evaluating the faulted condition. The emergency conditions (Service Level C) are bounded by the design conditions and therefore, the replacement reactor vessel head is evaluated using the primary stress limits of NB 3221.
The pressurizer was replaced to the design requirements of ASME Boiler and Pressure Vessel Code Section III, Subsection NB, 1998 Edition through 2000 Addenda. The primary stress limits for the emergency and faulted conditions are applied in accordance with subsection NB 3000 of the design code.
4.5.2.3 Pumps and Valves The primary stress limits applied in evaluating the emergency and faulted conditions for the pumps and valves in the RCS are specified as follows:
The RCS pumps and valves are designed in accordance with the rules of ASME Code for Pumps and Valves for Nuclear Power - March 1970, Draft. Supplementary to these rules, the primary stress limits used for Vessel, as discussed under Item b. above, are applied in evaluating the emergency and faulted conditions for the reactor coolant pumps (RCP). In the case of valves, the 4.5-7 Rev. 35
MPS2 UFSAR rules of the Pump and Valve Code are considered adequate to assure that, as regards primary stresses in the pressure boundary, the piping, not the valves, will be the limiting element.
Therefore, no supplementary criteria which limit the primary stresses during abnormal conditions are necessary.
4.5.3 OVERPRESSURE PROTECTION 4.5.3.1 Overpressure Protection During Normal Operation The RCS is structurally designed for operation at 2485 psig and 650°F (pressurizer 700°F).
Operation of the system 2235 psig nominal and 600°F will result in material stresses 90 percent of design values. Detailed structural analyses have been performed by the component vendors and reviewed independently by Combustion Engineering (CE) for all portions of the system. Welding materials used have physical properties superior to the materials which they join. Inspection procedures and tests specified and independently reviewed by CE were carried out to assure that pressure-containing components have the maximum integrity obtainable with present code-approved inspection techniques.
The RCS is protected against overpressure by two ASME Code approved safety valves which limit system pressure to a maximum of 110 percent of design. In addition, two solenoid-operated relief valves are provided as described in Section 4.3.7.
4.5.3.2 Low Temperature Overpressurization Protection The RCS low temperature overpressurization protection (LTOP) system, along with administrative procedures, provides protection against exceeding the ASME Section III, Appendix G (Protection Against Brittle Fracture) requirements during cold plant conditions; i.e.,
temperature < 275°F. The LTOP system consists of two redundant relief trains each with one power operated relief valve (PORV) with a setpoint of 400 psig and associated relief piping as described in Section 7.4.8.
4.5.4 REACTOR VESSEL THERMAL SHOCK An analysis of the thermal stresses produced in the reactor vessel wall due to the operation of the safety injection system has been performed. The analysis has been reported in a CE report Thermal Shock Analysis on Reactor Vessels due to Emergency Core Cooling System (ECCS)
Operation, A-68-9-1, and was submitted for the record on Docket Number. 50-309, Maine Yankee Atomic Power Station. The results show that there will be no failure of the reactor vessel due to brittle fracture.
Work has also been performed to refine the surface heat transfer coefficient. The temperature quench data obtained during the heat treatment of several heavy section steel plates was reviewed.
With this background, CE planned and conducted additional quench tests to develop experimental heat transfer coefficients.
4.5-8 Rev. 35
MPS2 UFSAR These tests were performed on a plate approximately 2 foot by 2 foot by one-half foot thick and instrumented with 11 thermocouples. The plate was heated to 550°F and lowered quickly into an agitated (turbulent) water bath at 80°F, nearly duplicating the temperature conditions which would be present in the reactor during ECCS operation. The temperature of all thermocouples was recorded throughout the cooldown of the plate.
Subsequently, the data was compared to a heat transfer computer model of the plate to obtain an effective heat transfer coefficient. A detailed report covering this work, entitled Experimental Determination of Limiting Heat Transfer Coefficients during Quenching of Thick Steel Plates in Water (A-68-10-2, December 13, 1968), was submitted to the AEC (now NRC) and made part of the public record. The report concludes that an effective heat transfer coefficient of 300 Btu/hr-ft2-F provides a realistic upper limit for thick steel plates quenched in highly agitated room temperature water.
The stress near the tip of axial and circumferential vessel cracks of various depth has been determined by the finite element method. This work was reported by a CE report, Finite Element Analysis of Structural Integrity of a Reactor Pressure Vessel during Emergency Core Cooling, A-70-19-2, January 1970, and is part of the public record.
These reports substantiate the analytical conclusion that a vessel failure will not occur due to ECCS operation. An acute crack, even if formed, will not propagate.
4.5.5 LEAK DETECTION Methods are provided to alert the operator of the presence of leakage from the RCS in a timely manner to allow detection and isolation of the leak to ensure the leakage does not exceed acceptable limits. Detection of leaks from the RCS can be accomplished by one or a combination of the below listed means.
Leak Detection Within the Containment Leaks within the containment may be indicated by:
- a. Increased pressure and temperature in the containment;
- b. Monitoring the normal containment sump level;
- c. An increase in airborne activity as measured by the containment air radiation monitor system. The sensitivity and response time of the particulate and gaseous detectors are dependent on many factors. Although the airborne activity detectors may very well give an early warning of an RCS leak, any correlation of these radiation monitor readings and the RCS leakage rate will be weak. These monitors are best used for trending purposes and a trigger to check other indications for leakage source; 4.5-9 Rev. 35
MPS2 UFSAR
- d. Monitoring the reactor building closed cooling water (RBCCW) temperature to and from the containment air recirculation (CARS) and cooling units.
Reactor Coolant System Leakage from the RCS is indicated by the level in the pressurizer or in the primary drain tank and/
or high RCS makeup flow from the chemical and volume control system.
Relief and Safety Valves Located on the Reactor Coolant System Piping from the relief and safety valves located on the pressurizer is provided with temperature sensors with readout in the main control room. Any temperature increase will indicate relief or safety valve leakage. In addition, an increase in pressurizer quench tank level, pressure, or temperature will also indicate leakage.
Reactor Vessel Head Closure The space between the double O-ring seal is monitored to detect an increase in pressure, which indicates a leak past the inner O-ring. A leak indicator in containment indicates pressure. Upon high temperature a control room alarm is sounded.
Leakage Through Steam Generator Tubes or Tube Sheet An increase in radioactivity indicated by radiation monitors for the gases from the condenser air ejectors or steam generator blowdown system monitors will indicate leakage through steam generator tubes to the secondary side. The N-16 radiation monitors will indicate primary to secondary leakage when the reactor is at power.
4.5.6 PREVENTION OF STAINLESS STEEL SENSITIZATION Sensitization of stainless steel occurs when unstabilized Type 300 Series stainless material is held in the temperature range of 900-1400°F for sufficient time to form a continuous network of chromium carbide precipitates. Sensitization occurs after approximately 100 hours0.00116 days <br />0.0278 hours <br />1.653439e-4 weeks <br />3.805e-5 months <br /> at 900°F, as compared to one hour at 1400°F. Stabilized Type 300 Series stainless material avoids continuity of chromium carbide precipitates in the grain boundaries by careful control of metal chemistry.
There are no furnace sensitized stainless steels in the reactor coolant pressure boundary (RCPB).
Sensitization is precluded from the NSSS through materials selection and control to all welding and heat treating procedures.
Major portions of the RCPB in CEs nuclear plants are shown in preceding tables in this section to be formed by carbon steels and a high nickel base alloy. None of these materials is susceptible to furnace sensitization (a continuous network of iron-chromium grain boundary carbides) in the sense of unstabilized Type 300 Series stainless steels. All internal carbon steel surfaces are weld-deposit or roll-bond clad with Inconel or stainless steel, to preclude excessive corrosion.
4.5-10 Rev. 35
MPS2 UFSAR Internal surfaces of the reactor vessel, pressurizer and steam generator primary side are overlaid with Type 308, 309 or 308L weld deposited metal. Weld metal composition is carefully controlled to overcome interface dilution and promote an austenoferritic duplex structure. Therefore, during the stress relief heat treatment (1150 +/-25°F) required by the ASME Code for the pressure vessel, a continuous network of chromium carbide precipitates is not formed in the Type 308 or 308L weld overlay even though this material has been subjected to a furnace heat treatment. The delta ferrite acts as a carbon sink and prevents continuity of carbide precipitates.
Extensive testing has confirmed that, properly formulated (a duplex structure), Type 308 weld deposited metal does not form a continuous carbide network within grain boundaries even following a typical vessel post weld heat treatment (viz, 1150°F for 20 hours2.314815e-4 days <br />0.00556 hours <br />3.306878e-5 weeks <br />7.61e-6 months <br />). Hence, the material is immune to intergrannular corrosion.
The replacement reactor vessel head is overlaid inside with stainless steel weld material. The first layer is type 309 stainless steel and all subsequent layers including the final layer that is in contact with the reactor coolant is type 308L stainless steel.
Susceptibility to underclad / reheat cracking was minimized by controlling the welding heat input and chemical composition of the RV Head forging to maintain the Delta G function less than 0.1 in accordance with the correlations developed by the vendor (Mitsubishi Heavy Industries). In addition, in order to comply with the intent of Reg Guide 1.43, examinations were performed on three representative penetration holes in the RV Head J groove preparations prior to depositing the buttering to specifically check for underclad / reheat cracking on the susceptible area up to 12 inch below the fusion line between the base material and cladding.
The bimetallic weld on the CEDM and instrumentation nozzles for the replacement head joins the stainless steel threaded connector or flange to the alloy 690 penetration tube. Additionally, the materials for welding to Alloy 690 have lower susceptibility to PWSCC than the original alloy 82182 welds.
The J-groove weld design for the guide tubes is modified to control the amount of overwelding to a minimum and thus minimize residual weld stresses. The weld surface finish was also improved to facilitate surface examinations.
All other Type 300 Series stainless steel used either is not subjected to a furnace sensitization heat treatment or, as is the case of cladding on the primary piping, is of Type 304L (low carbon, 0.03% max.) composition and is not susceptible to the formation of continuous chromium carbide grain boundary networks.
The replacement pressurizer is overlaid inside with stainless steel weld material. Susceptibility to underclad/reheat cracking was precluded by performance testing of the cladding weld procedure specifications in accordance with NRC Regulatory Guide 1.43.
The RCS pump casing is CF8M (Cast 316), which again is a duplex material. The casting is solution annealed after welding; hence, this component will not have a sensitized structure.
4.5-11 Rev. 35
MPS2 UFSAR Nitrogen-enhanced stainless steel was not used in the fabrication of any RCPB component.
Because carbon steel piping is used in the RCS, no safe ends are required on the reactor vessel, or steam generator primary nozzles. Where small diameter solid stainless pipes are employed (or in the instance of welding the coolant pump casing to carbon steel), an Inconel-182 weld deposit is built up on the nozzle prior to vessel post-weld heat treatment. Thereafter, an annealed stainless steel safe end is shop welded to the Inconel-182 buildup using alloy 82/182 weld metal.
In joining small diameter annealed solid stainless steel piping, as is used in the pressurizer surge line, charging pump lines and safety injection systems, some carbide precipitation will occur as a result of welding. However, the precipitation that occurs in the weld heat affected zone does not sensitize the material in the context of forming continuous grain boundary carbide precipitates.
Samples from typical such welds pass the industry accepted standard for intergrannular corrosion susceptibility (i.e., Strauss Test - ASTM-A393). Metallographic examination of such welds reveal that only discontinuous grain boundary precipitates are present.
The following four welding processes are used to weld stainless steel in CEs NSSSs. Welding processes are performed in accordance with written procedures, as provided in the Quality Assurance Program. Nitrogen is not used as a purge gas in the welding process in lieu of argon or helium gas.
- Shielded Metal Arc (SMA)
- Gas Tungsten Arc (GTA)
- Gas Metal Arc (GMA)
- Submerged Arc (SA)
- a. Shielded metal arc (SMA) is a process wherein coalescence is produced by heating with an electric arc drawn between a flux covered metal electrode and the work.
- b. In the gas tungsten arc (GTA), coalescence is produced by heating with an electric arc drawn between a tungsten electrode and the work. Filler metal, if required, is added by feeding a bare metal rod or wire into the weld pool. Shielding of the weld is obtained from an inert gas mixture.
- c. With gas metal arc (GMA), coalescence is effected by heating with an arc drawn between a continuous feed wire electrode and the work. Shielding of the weld is obtained from an externally supplied inert mixture.
- d. Submerged arc (SA) produces coalescence by heating with an arc or arcs drawn between a bare metal (filler) electrode or electrodes and the work. The arc and weld are shielded by a blanket of granular fusible flux.
4.5-12 Rev. 35
MPS2 UFSAR Table 4.5-1 lists the nozzles on the steam generator, reactor vessel, pressurizer and piping. The table also indicates the size of the nozzle, base material of the nozzle and, where applicable, the material of the nozzle safe end.
The procedures used in welding nozzles within CE manufacturing facilities are generally as follows: (1) For nozzles with stainless steel safe ends, the safe ends are not attached until after final stress relief, and (2) the stainless steel safe end is welded to Inconel buttering on the alloy steel and the weld made using Inconel weld wire. With this procedure furnace sensitizing of stainless steel is precluded.
During manufacture of the core structures, various parts of the core structure are tested for sensitization using the Strauss Test (ASTM A393). Test specimens consist of: (1) mockups of various welded joints, and (2) monitoring specimens included in any heat treatment of various components. None of the specimens tested in conjunction with fabrication of reactor vessel internals for previous CE plants have failed the Strauss Test. The replacement reactor vessel head and replacement pressurizer weld materials and welding are controlled in accordance with Regulatory Guide 1.44, May 1973, Control of the use of Sensitized Steel, to preclude sensitization of austenitic stainless steels.
The typical weld heat input with the above processes as used by CE to joint Type 300 Series stainless steel varies from 6000 joules per inch GTA to 96,000 joules per inch SA. To avoid weld heat affected zone sensitization, CE limits the interpass temperature on multipass welds in stainless steels to 350°F maximum. The replacement pressurizer uses only low carbon stainless steel materials. The CE interpass temperature limits do not apply to the replacement pressurizer.
AREVA limited the interpass temperature for low carbon stainless steel materials to 250°C (482°F), which is sufficient to prevent sensitization. The combination of normal heat input using the above welding procedures and control of interpass temperature assures minimum carbide precipitation in the weld heat affected zone. Samples from large welds have been examined in the laboratory and none has failed the Strauss Test.
In field welding operations, Bechtel uses welding procedures that limit heat input to the weld areas, and thus preclude the possibility of sensitization of austenitic stainless steels. Most of the welding employed is of the manual SMA process; a minor amount of GMA welding is also used.
Neither one of these processes would be classified as an excessively high heat input welding procedure.
Further precautions employed to preclude field sensitization of austenitic stainless steels consist of:
- a. Preheat and interpass temperatures are limited to 350°F maximum.
- b. Controlled welding sequence is used to minimize heat input.
- c. The practice of block welding is prohibited.
4.5-13 Rev. 35
MPS2 UFSAR
- d. Postweld heat treatment is prohibited on equipment and/or parts that are completely or partially fabricated of austenitic stainless steel. During the fabrication of the replacement pressurizer post weld heat treatment was performed on the safety/relief nozzles and spray nozzle safe ends. Nozzle welds were post heat-treated using a Post Weld Heat Treatment (PWHT) procedure specially qualified for the heat of material used for the safe ends in accordance with Regulatory Guide 1.44 to preclude sensitization.
- e. Application of heat to correct weld distortions resulting in dimensional deviations in equipment and/or parts fabricated of austenitic stainless steel is prohibited.
In preparing for, and engineering, the field welding requirements, close liaison is maintained between Bechtel and CE. Detailed welding parameters prepared by CE are submitted to CE for review and mutual concurrence and approval before they are adopted for use. Bechtel quality assurance procedures for field welding are discussed in Appendix 1B. Appendix 1B was located in the original FSAR dated August 15, 1972.
The delta ferrite content of all austenitic stainless steel weld metals used to fabricate CEs RCS components is controlled to 5-18% in the as-deposited condition. Delta ferrite content is confirmed from chemical analysis and the Schaeffler or McKay Diagrams. In addition, a calibrated ferrite measuring instrument (Seven Gauge or similar) is used. The ferrite requirement is met for each heat and/or lot of filler metal used in fabrication. The ferrite content in the weld materials and welding for the replacement reactor vessel head and replacement pressurizer are in accordance with Reg Guide 1.31, Control of Ferrite in Stainless Steel weld metal.
Where field welding of austenitic stainless steels is required in the RCS only the inert GTA and manual SMA processes are used. The welding procedures were qualified in accordance with Section IX of the ASME Boiler & Pressure Vessel Code. Tensile test specimens were taken to exhibit the tensile strength of the welded joints and bend tests were taken to indicate the ductility of the weld joints. Filler material compositions are in accordance with the ASME SFA/AWS filler material specification and are selected on the basis of the austenitic stainless steels to be welded.
In addition to these requirements the filler materials must be capable of depositing 8 to 25%
ferrite. This is verified for each heat or lot of filler material by plotting the heat analysis for bare wire or the analysis of an all weld metal deposit for covered electrodes on the Schaeffler, DeLong or equivalent diagram to determine its ferrite content and the acceptability of the filler materials.
The austenitic stainless steel materials including cladding are analyzed for delta ferrite in accordance with NB-2433. The FN shall be 5FN to 15FN. The FN for undiluted ER309L deposit shall be in the range of 5FN - 22FN. By control of the welding processes, the filler materials and the welding parameters (by specifying a maximum interpass temperature of 350°F), the welds should contain sufficient delta-ferrite in the austenitic matrix to avoid hot cracking in the austenitic stainless steel welds.
4.5-14 Rev. 35
MPS2 UFSAR 4.
5.7 REFERENCES
4.5-1 W. G. Counsil (NU) letter to J. R. Miller (NRC), Millstone Nuclear Power Station, Unit No. 2, Proposed Revisions to Technical Specifications, Pressure-Temperature Curves (January 4, 1984), Attachment 2 - CE Report TR-N-MCM-008, Evaluation of Irradiated Capsule W-97 (April, 1982).
4.5-2 S. E. Scace (DNC) to U.S. NRC, Millstone Nuclear Power Station, Unit No.2, Submittal of Third Reactor Vessel Surveillance Capsule Report, (February 2003),
Enclosure - WCAP-16012 Revision 0, Analysis of Capsule W-83 from the Dominion Nuclear Connecticut Millstone Unit 2 Reactor Vessel Radiation Surveillance Program, (February 2003).
4.5-15 Rev. 35
MPS2 UFSAR TABLE 4.5-1 REACTOR COOLANT SYSTEM COMPONENT NOZZLES, NOZZLE SIZES AND NOZZLE MATERIALS Steam Generator Component (Number) Size Material Primary Inlet (1) 42 inch ID Carbon steel safe ends clad with stainless steel Primary Outlet (2) 30inch ID Carbon steel safe ends clad with stainless steel Pressure Taps (4) 1inch Schedule 160 Inconel B-166 Steam Outlet (1) 36 inch ID Carbon steel Feedwater (1) 18 inch Schedule 80 Carbon steel Bottom Blowdown (2) 4 inch ID Carbon steel Liquid Level (12) 1 inch Schedule 80/ Carbon steel/Inconel B-166 Schedule 160 Nitrogen Addition (1) 1 inch Schedule 80 Carbon steel Wet Layup (1) 2 inch Schedule 160 Carbon steel Reactor Vessel and Head Component (Number) Size Material Primary Outlet (2) 42 inch ID Carbon steel clad with stainless steel Primary Inlet (4) 30 inch ID Carbon steel clad with stainless steel CEDM/HJTC (69) 2.718 inch ID Ni-Cr-Fe and stainless steel Instrumentation (8) 4.625 inch ID Ni-Cr-Fe and stainless steel Vent (1) 0.75 inch Schedule 80 Inconel SB-167 Pipe Component (Number) Size Material Surge Nozzle (1) 12 inch Schedule 160 A-105 Gr II with A-351 Gr CF8M safe end 4.5-16 Rev. 35
MPS2 UFSAR Pipe Component (Number) Size Material Pressure (8) 0.75 inch Schedule Inconel B-166 with A-182 Type 160 316 safe end RTD (25) 1 inch nominal Inconel B-166 Shutdown Cooling (1) 12 inch Schedule 140 A-105 Gr II with A-351 Gr CF8M safe end Spray (2) 3 inch Schedule 160 A-105 Gr II with A-182 Type 316 SS safe end Safety Injection (4) 12 inch Schedule 140 A-182 F1 with A-351 Gr CF8M safe end Charging Inlet (2) 2 inch Schedule 160 A-105 Gr II with A-182 Type 316 SS safe end Sampling (2) 0.75 inch Schedule Inconel B-166 with A-182 Type 160 316 SS safe end Drain/Letdown (5) 2 inch Schedule 160 A-105 Gr II with A-182 Type 316 SS safe end Pump (8) 30 inch ID A-516 Gr 70 clad with A-240, Type 304L SS with A-351, CF8M safe end 4.5-17 Rev. 35
MPS2 UFSAR TABLE 4.5-2 REACTOR COOLANT SYSTEM HEATUP AND COOLDOWN LIMITS Cooldown Heatup a Indicated Cold Leg Indicated Cold Leg Temperature Limit Temperature Limit 220°F 50°F/hour 200°F 60°F/hour
> 220°F 100°F/hour 200°F < T 275°F 80°F/hour
> 275°F 100°F/hour a.These limitations apply to hydrostatic and leak test conditions.
4.5-18 Rev. 35
MPS-2 FSAR FIGURE 4.5-1 REACTOR COOLANT SYSTEM PRESSURE TEMPERATURE LIMITATIONS FOR 7 FULL POWER YEARS
.- .- .. _--~
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- '1 I_f-'
. =~
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MPS-2 FSAR FIGURE 4.5-3 REACTOR COOLANT SYSTEM PRESSURE TEMPERATURE LIMITATIONS FOR 0 TO 2 YEARS OF FULL POWER MINIMUM PRESSURE TEMPERATURE FOR:
- CRITICAL OPERATION OF CORE 3200 ** NON-CRITICAL OPERATION OF CORE SYSTEM HYDRO LOWEST SERVICE HEATUP **
2800 TEMPERATURE COOLDOWN **
HEATUP
- COOLDOWN
- 2400 INDICATED PRESSURIZER PRESSURE, PSIA 2000 1600 1200 NOTES:
0 100 200 300 400 500 INDICATED REACTOR COOLANT TEMPERATURE JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.5-4 REACTOR COOLANT SYSTEM HEATUP LIMITATIONS FOR 54 EFPY 2500 I I I I I I I I I I I I I I I I I I I I I 1 I I I I I I I I I I 1 f- - -I-- --1----"1-- ---1--- --T--f-- I -- ---1-- f--- ---
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MPS-2 FSAR FIGURE 4.5-5 REACTOR COOLANT SYSTEM COOLDOWN LIMITATIONS FOR 54 EFPY 2500 I I I I I I 1 I
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MPS2 UFSAR 4.6 TESTS AND INSPECTIONS 4.6.1 GENERAL Shop inspection and tests of all major components are performed at the vendors plants prior to shipment. An inspection at the site is performed to assure that no damage has occurred in transit.
Testing of the reactor coolant system (RCS) are performed at the site upon completion of the plant construction. These tests will include hydrostatic tests of all fluid systems. A complete visual inspection of all welds and joints are performed prior to the installation of the insulation. All field welds are radiographically and dye penetrant inspected in accordance with the requirements of Section III of the American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code.
In addition to the code-required examinations on the replacement reactor vessel head, base line examinations were performed prior to the component being place in service. These baseline examinations include a full volumetric examination of the CEDM nozzle base material, a minimum of 2 inches from the high point of the J-groove weld down to the threaded portion.
Additionally eddy current examination was performed on the wetted surface of at least 28 peripheral CEDM nozzles in the bimetallic weld area.
A hot flow test of the reactor coolant loop up to zero power operating pressure and temperature without the core installed will be made. The system will be checked for vibration and cleanliness.
Auxiliary systems will be checked for performance (see Chapter 13).
4.6.2 NIL DUCTILITY TRANSITION REFERENCE TEMPERATURE The carbon and low alloy steels which form the reactor coolant pressure boundary are required to satisfy the requirements of 10 CFR 50, Appendix G which utilizes the nil ductility transition reference temperature (RTNDT) as the basis for establishing operational limitations for the reactor coolant system.
The original materials associated with the reactor coolant pressure boundary were ordered and tested to the requirements of ASME Code,Section III, Paragraph N-330. The impact properties of these materials were required to meet the acceptance criteria noted in Paragraph N-330 at +40°F.
These tests determined the nil ductility transition temperature (NDTT) for these materials. As the original design requirements were insufficient to directly establish the initial RTNDT of the pressure boundary materials and comply with the requirements of 10 CFR 50, Appendix G, the RTNDT was either estimated using the procedures of MTEB 5-2, performance of supplemental testing of surplus material in accordance with NB-2331 of Section III to the ASME Code or developed from generic impact testing.
In the case of the reactor vessel, the beltline materials will experience a shift (an increase) in nil ductility transition reference temperature due to neutron irradiation. This increase is calculated in accordance with regulatory positions and is described in Section 4.5.1.3.
4.6-1 Rev. 35
MPS2 UFSAR To assure that the change in the fracture toughness properties behave in the expected fashion, a reactor vessel material surveillance program is conducted. A description of the surveillance program is provided in Section 4.6.3.
The design material toughness test requirements were as follows:
Reactor Vessel Carbon and low alloy steel materials which form a part of the pressure boundary shall meet the requirements of the ASME Code,Section III, Paragraph N-330 at a temperature of +40°F. It shall be an objective that the materials meet this requirement at -10°F. Charpy tests shall be performed and the results used to plot a transition curve of impact values vs. temperature extending from fully brittle to fully ductile behavior. The actual NDT temperature of inlet and outlet nozzles, vessel and head flanges, and shell and lower head materials shall be determined by drop weight tests per ASTM E-208.
Replacement Reactor Vessel Closure Head The impact properties of carbon and low alloy steel materials including weld filler metals for the replacement head shall meet the requirements of ASME Section III, Subsection NB 2331, 1998 Edition through 2000 Addenda. Charpy V-notch transition curves were established in accordance with SA 508 supplementary requirements (S3) for temperatures showing, upper shelf energy, lower shelf energy and transition. The actual TNDT shall be determined by drop weight test in accordance with ASTM E208. Reference temperature, RTNDT shall be determined in accordance with NB 2331.
Steam Generator and Pressurizer It shall be an objective that impact properties of all ferritic steel materials which form a part of the pressure boundary shall meet the requirements of the ASME code Section III, at a temperature of
+10°F; alternate higher temperature levels up to 40°F may be used only if the material fails at
+10°F. Such higher temperature levels, if applicable, shall be determined and documented. This objective is applicable to the pressurizer and the original steam generators, of which the original steam drums are still in use. For the steam generator replacement subassemblies, the maximum allowable RTNDT as defined in paragraph NB-2311(a) of ASME Section III Code is 0°F. For the replacement pressurizer ferritic steel materials, the RTNDT shall be performed at a temperature of 10 degrees F or less. The actual TNDT is determined by drop weight test in accordance with NB 2331 to ASTM-208-91.
Reactor Coolant Piping Materials used to fabricate the pipe fittings shall be specified, examined and tested to satisfy as a minimum the requirements of Chapter I-III of the American Nuclear Society (ANS) Code for Pressure Piping B31.7, Class 1.
4.6-2 Rev. 35
MPS2 UFSAR Impact properties of carbon steel materials, including welds, shall have a minimum V-notch value of 20 ft-lb (average of three specimens) or 15 ft-lb (any individual specimen) at 40°F. It shall be a design objective that the materials meet this requirement at 10°F. Weld procedure qualifications and weld metal certifications records may serve to demonstrate impact properties of welds.
The initial toughness test data for these components are provided in Tables 4.6-1, 4.6-2, 4.6-3 and 4.6-4. Table 4.6-1 also provides RTNDT values.
Toughness test data are summed as follows:
- a. The maximum NDT temperature for the reactor vessel as obtained from drop weight tests is +10°F. Drop weight tests were conducted only for material used in the reactor vessel.
- b. The maximum temperature corresponding to the 50 ft-lb value of the Cv fracture energy for the reactor vessel is +65°F.
Refer to the tables presented above the Charpy V-notch data at 10°F for the steam generators, pressurizer, and reactor coolant piping.
- c. The minimum upper-shelf Cv energy value for the strong direction of the material used in the reactor vessel is 103 ft-lb.
The upper shelf-Cv energy was not determined for the material used in fabricating the steam generator, pressurizers, or reactor coolant piping. The data was not obtained for the weak direction in the material used to fabricate the reactor vessels, thus branch technical position MTEB5.2 is used to establish transverse (WR) properties.
Due to regulatory changes during the construction of the facility, it was necessary to establish the RTNDT of the reactor coolant pressure boundary materials to comply with the requirements of 10 CFR 50 Appendix G. In most instances, this has been accomplished by utilizing the guidance of MTEB 5.2 to estimate the RTNDT of the material based upon the available data. An initial RTNDT of 50°F has been established for the reactor coolant pressure boundary materials (excluding the reactor vessel beltline) based on MTEB 5-2. However, in the case of the reactor vessel beltline materials, the RTNDT was not determined through a combination of methods including utilizing the guidance of MTEB 5-2, testing surplus materials to the requirements of NB-2300, and utilizing generic data. The initial RTNDT values for the beltline materials are provided in Table 4.6-12. In addition, the primary side of the steam generator has been replaced and the materials RTNDT values have been determined from testing in accordance with NB-2300.
4.6-3 Rev. 35
MPS2 UFSAR 4.6.3 SURVEILLANCE PROGRAM The surveillance program is implemented to monitor the radiation-induced changes in the mechanical and impact properties of the pressure vessel materials in accordance with the requirements of 10 CFR 50, Appendix H. Changes in the impact properties of the material are evaluated by the comparison of pre-irradiation and post-irradiation Charpy impact test specimens.
Changes in mechanical properties are evaluated by the comparison of pre-irradiation and post-irradiation data from tensile test specimens.
Three metallurgically different materials representative of the pressure vessel are investigated.
These are base metal, weld metal, and weld HAZ material. In addition to the materials from the reactor vessel, materials from a standard heat of A533B, made available through the Heavy Section Steel Technology (HSST) Program, are also used. This reference material is fully processed and heat treated and is used for Charpy impact specimens so that a comparison may be made between the irradiations in various operating power reactors and in experimental reactors. A complete record of the chemical analysis, fabrication history and mechanical properties of all surveillance test materials is maintained.
The exposure locations and a summary of the specimens at each location is presented in Table 4.6-8. The pre-irradiation NDT temperature of each plate in the intermediate and lower vessel shell courses is determined from the drop weight tests and correlated with Charpy impact tests.
Base metal test specimens are fabricated from sections of the shell plate in either the intermediate or the lower shell course which exhibits the highest unirradiated NDT temperature. All base material test specimens are cut from the same shell plate. This material is heat treated to a condition of the base metal in the completed reactor vessel.
Weld metal and HAZ material are produced by welding together two plate sections from the intermediate or lower shell course of the reactor vessel. All HAZ test materials are also fabricated from the plate which exhibits the highest unirradiated NDT temperature.
The material used for weld metal and HAZ test specimens was adjacent to the test material used for ASME Code,Section III tests and was at least one plate thickness from any water-quenched edge. The procedures used for making the shell girth welds in the reactor vessel was followed in the preparation of the weld metal and HAZ test materials. The procedures for inspection of the reactor vessel welds was followed for inspection of the welds in the test materials. The welded plate was heat treated to a condition which is representative of the final heat treated condition of the completed reactor vessel.
Additional information from the baseline surveillance program includes the chemical composition of the surveillance plate and weldment (made from two separate heats of weld wire),
which are given in Table 4.6-5. The baseline mechanical properties of the base metal (WR and RW), weld metal, heat affected zone (HAZ), and standard reference material (SRM), are shown in Tables 4.6-6 and 4.6-7. The Charpy V-notch impact energy and lateral expansion data as a function of test temperature are shown in Figures 4.6-5 through 4.6-14.
4.6-4 Rev. 35
MPS2 UFSAR The test specimens are contained in six irradiation capsule assemblies. The axial position of the capsules bisected by the midplate of the core. The circumferential locations include the peak flux regions. The reactor vessel surveillance program was designed in accordance with ASTM E185 (no edition specified). The program complies with ASTM E185-73 and 10 CFR 50, Appendix H.
The location of the surveillance capsule assemblies is shown in Figure 4.6-1. A typical surveillance capsule assembly is shown in Figure 4.6-2. A typical Charpy impact compartment assembly is shown in Figure 4.6-3. A typical tensile monitor compartment assembly is shown in Figure 4.6-4.
Fission threshold detectors (U-238) were inserted into each surveillance capsule to measure the fact neutron flux. Threshold detectors of Ni, Ti, Fe, S, and Cu with known Co content have been selected for this application to monitor the fast neutron exposure. Cobalt is included to monitor the thermal neutron exposure.
The selection of threshold detectors is based on the recommendations of ASTM E-261. Method for Measuring Neutron Flux by Radioactive Techniques. Activation of the specimen material will also be analyzed to determine the amount of exposure.
The maximum temperature of the encapsulated specimens will be monitored by including in the surveillance capsules small pieces of low-melting-point eutectic alloys or pure metals individually sealed in quartz tubes.
The temperature monitors will provide an indication of the highest temperature to which the surveillance specimens were exposed but not the time-temperature history or the variance between the time-temperature history of different specimens. These factors, however, will affect the accuracy of the estimated vessel material NDT temperature to only a small extent.
Test specimens removed from the surveillance capsules are tested in accordance with ASTM Standard Test Methods for Tension and Impact Testing. The data obtained from testing the irradiated specimens will be compared with the unirradiated data and an assessment of the neutron embrittlement of the pressure vessel material will then be made. This assessment of the NDT temperature shift is based on the temperature shift in the average Charpy curves, the average curves being considered representative of the material.
The periodic analysis of the surveillance samples permit the monitoring of the neutron radiation effects upon the vessel materials. If, with due allowance for uncertainties in NDT temperature determination, the measured NDT temperature shift turns out to be greater than predicted, then appropriate limitations would be imposed on permissible operating pressure-temperature combinations and transients to ensure that the existing reactor vessel stresses are low enough to preclude brittle fracture failure.
The original six surveillance capsules were inserted into their designated holders during the final reactor assembly operation. Each capsule remains in the reactor for the tentative schedule listed in Table 4.6-9. Table 4.6-9 shows the target fluence for each of the capsules.
4.6-5 Rev. 35
MPS2 UFSAR The fluence values in Table 4.6-9 are accurate within +30 percent.
4.6.4 NONDESTRUCTIVE TESTS Prior to and during fabrication of the reactor vessel, nondestructive tests based upon Section III of the ASME Boiler and Pressure Vessel Code were performed on all welds, forgings and plates as follows:
All full penetration pressure retaining welds were 100 percent radiographed to the standards of paragraph N-624 of Section III of the ASME Boiler and Pressure Vessel Code. Other pressure retaining welds such as those used for the attachment of mechanism housings, vents and instrument housings or the replacement reactor vessel head and J groove welds were inspected to additional inspection criteria listed in Table 4.6-11.
All forgings were inspected by ultrasonic testing, using longitudinal beam techniques. In addition, ring forgings were tested using shear wave techniques. Rejection under longitudinal beam inspection, with calibration so that the first back reflection is at least 75 percent of screen height, was based on interpretation of indications causing complete loss-of-back reflection. Rejection under shear wave inspection was based on indications, exceeding the amplitude of the indication from a calibration notch whose depth is three percent of the forging thickness not exceeding 28 inch with a length of 1 inch.
All forgings were also subjected to magnetic-particle examination or liquid-penetrant testing depending upon the material. Rejection was based on Section III of the ASME Code, paragraph N626.3 for magnetic-particle and paragraph N627.3 for dye penetrant testing.
Plates were ultrasonically tested using longitudinal ultrasonic testing techniques. Rejection under longitudinal beam testing performed in accordance with ASME Code, with calibration so that the first back reflection is at least 50 percent of screen height, was based on defects causing complete loss of back reflection. Any defect which showed a total loss of back reflection which could not be contained within a circle whose diameter is the greater of three inches or one-half the plate thickness was unacceptable. Two or more defects smaller than described above which caused a complete loss-of-back reflection were unacceptable unless separated by a minimum distance equal to the greatest diameter of the larger defect unless the defects were contained within the area described above.
Nondestructive testing of the vessel was performed during several stages of fabrication with strict quality control in critical areas such as frequent calibration of test instruments, metallurgical inspection of all weld rod and wire, and strict adherence to the nondestructive testing requirements of Section III of the ASME Boiler and Pressure Vessel Code.
The detection of flaws in irregular geometries was facilitated because most nondestructive testing of the materials was completed while the material was in its simplest form. Nondestructive inspection during fabrication was scheduled so that full penetration welds were capable of being radiographed to the extent required by Section III of the ASME Boiler and Pressure Vessel Code.
4.6-6 Rev. 35
MPS2 UFSAR The new replacement reactor vessel closure head is a single piece forging. The head was replaced during refueling outage 16. Prior to and during fabrication of the replacement reactor vessel head, nondestructive tests based upon Section III of the ASME Boiler and Pressure Vessel Code 1998 Edition through 2000 Addenda were performed on the forging and welds.
Ultrasonic and magnetic particle examinations were performed on the head forging in accordance with ASME Section III, NB 2000 and NB 5000 respectively. Head cladding was ultrasonically examined for both bond and defects using a calibration block typical of the cladding and base material. Any indications that produce amplitude equal to or greater than the amplitude received from the three-eighths inch flat bottom hole, regardless of length, were unacceptable (see Table 4.6-11 for additional owners inspection requirements).
Pressure retaining welds were 100% radiographed and liquid penetrant examined in accordance with NB 5000. Canopy seal welds were liquid penetrant examined. J-groove welds were liquid penetrant examined at half thickness and again at final surface. No indications were allowed for the final PT of the J welds on the CEDM and instrument and vent nozzles and attachments of mechanism housings. Hydrostatic tests at the shop were conducted to 3107 psig. Visual examinations, magnetic particle and liquid penetrant tests were performed to reveal any surface discontinuities.
In addition to the pre-service examinations required by Section XI of the ASME Boiler and Pressure Vessel Code, augmented ultrasonic and eddy current examination were performed on the inconel nozzle bore material to meet the examination requirements of NRC Bulletin 2001-01, Circumferential Cracking of Reactor Pressure Vessel Head Penetration Nozzles, August 3, 2001 and NRC Bulletin 2002-01, Reactor Pressure Vessel Head Degradation and Reactor Coolant Pressure Boundary Integrity March 18, 2002.
Each of the vessel studs received one ultrasonic test and one magnetic-particle inspection during the manufacturing process.
The ultrasonic test was a radial longitudinal beam inspection, and a discontinuity which causes an indication with a height which exceeded 20 percent of the height of the adjusted first back reflection was cause for rejection. Any discontinuity which prevents the production of a first back reflection of 50 percent of the screen height was also cause for rejection.
The magnetic-particle inspection was performed on the finished studs. Linear axially aligned defects whose lengths are greater than one inch long and linear nonaxial defects were unacceptable.
The vessel studs are elongated by the stud tensioners during each installation of the vessel head.
The amount of elongation for the desired preload was specified by the vendor to fall within a predetermined acceptance range. Maintenance procedures for vessel head installation are in full compliance with the vendor specified range.
The replacement pressurizer assembly consists of upper and lower heads and two shells attached by circumferential seam welds. The shells and the heads are forged components. The large bore 4.6-7 Rev. 35
MPS2 UFSAR nozzles (safety, relief, spray and surge) are integral with the upper and lower head eliminating the nozzle to shell welds. The attachment weld between the lower head prolongation and the support skirt is greater than one t limit of the ASME Boiler and Pressure Vessel Code Section XI, Subsection IWB jurisdictional boundary. Therefore ASME Section XI, Subsection IWF jurisdiction applies to the attachment weld.
Non destructive examinations were performed on forgings and welds in accordance with ASME Section III, Boiler and Pressure Vessel Code 1998 Edition through 2000 Addenda. Ultrasonic and magnetic particle examinations were performed on the forged components in accordance with ASME Section III, NB 2000 and 5000. The heater sleeves, vent and instrument nozzles are J-groove weld attachments to the reinforced weld buildup of the replacement pressurizer. The partial penetration welds were examined by liquid penetrant tests in accordance with NB-5245.
The electrical heater sheaths were completely liquid penetrant inspected in accordance with NB-5000. In addition to the code requirements, additional inspection criteria listed in Table 4.6-11 for the pressurizer were required for acceptability.
Hydrostatic test of the replacement pressurizer was conducted at 3125 psia.
Prior to and during fabrication of the components of the RCS, nondestructive testing based upon the requirements of Section III of the ASME Boiler and Pressure Vessel Code is used to determine the acceptance criteria for various size flaws. The requirements for the Class A vessels are the same as the reactor vessel. Vessels designated as Class C were fabricated to the standards of Subsection C, Article 21 of Section III of the ASME Code.
Table 4.6-10 summarizes the components inspection program during fabrication and construction.
In addition to the inspections conducted during fabrication and construction of the pressurizer shown in Table 4.6-10, pre-service inspections were performed on several components of the replacement pressurizer. UT inspections were performed on the circumferential welds of the pressurizer shell and heads. Magnetic particle inspection of the skirt to vessel was performed. UT and PT inspections were performed on the safety, relief, spray and surge nozzles.
Periodic tests and examinations of the RCS are conducted after startup on a regular basis.
For preoperational and in-service structure surveillance of the RCS, refer to the Technical Specifications; tests for RCS integrity after the system is closed following normal opening, modification or repair are specified in Technical Specifications.
4.6.5 ADDITIONAL TESTS During design and fabrication of the reactor vessel, additional operations beyond the requirements of the ASME Boiler and Pressure Vessel Code,Section III were performed by the vendor.
Table 4.6-11 summarizes the additional tests by components.
During the design of the reactor vessel, detailed calculations were performed to assure that the final product would have adequate design margins. A detailed fatigue analysis of the vessel for all 4.6-8 Rev. 35
MPS2 UFSAR design conditions has been performed. In those areas which are not amenable to calculation, stress concentrations have been obtained through the use of photo-elastic models. In addition, Combustion Engineering (CE) has performed test programs for the determination and verification of analytical solutions to thermal stress problems. Also fracture mechanics and brittle fracture evaluations have been performed.
The thermal and structural analyses of CEDM and ICI head adapters of the replacement reactor vessel closure head were performed using finite element models. Structural responses from loads including branch line pipe break, faulted conditions (combination of line break and seismic),
normal operating mechanical and acoustic excitation were evaluated. ASME Appendix G evaluations were performed assuming meridional and circumferential flaws at critical locations of the reactor vessel closure head. Detailed fatigue analysis using finite element models of bimetallic welds at the interface between alloy 690 and stainless steel for the ICI nozzles were performed.
All material used in the reactor vessel was carefully selected and precaution were taken by the vessel fabricator to ensure that all material specifications were adhered to. To assure compliance, the quality control staff of CE reviewed the mill test reports and the fabricators testing procedures.
All welding methods, materials, techniques, and inspections comply with Sections III and IX of the ASME Boiler and Pressure Vessel Code. Before fabrication was begun, detailed qualified welding procedures, including methods of joint preparation, together with certified procedure qualification test reports, were prepared. Also, prior to fabrication, certified performance qualification tests were obtained for each welder and welding operator. Quality control was exercised for all welders and welds by subjection to a complete and thorough testing program in order to ensure maximum quality of welded joints.
During the manufacture of the reactor vessel, in addition to the areas covered by the ASME Boiler and Pressure Vessel Code,Section III, quality control by the vendor included:
- a. preparation of detailed purchase specifications which included cooling rates for test samples;
- b. requiring vacuum degassing for all ferritic plates and forgings;
- c. specification of fabrication instructions for plates and forgings to provide control of material prior to receipt and during fabrication;
- d. use of written instructions and manufacturing procedures which enable continual review based on past and current manufacturing experiences;
- e. performance of chemical analysis of welding electrodes, welding wire, and materials for automatic welding, thereby providing continuous control over welding materials; 4.6-9 Rev. 35
MPS2 UFSAR
- f. the determination of NDT temperature through use of drop weight testing methods as well as Charpy impact tests;
- g. and test programs on fabrication of plates up to 15 inches thick to provide information about material properties as thickness increases.
RW wave ultrasonic testing was performed on 100 percent of all plate material.
Cladding for the reactor vessel is a continuous integral surface of corrosion-resistant material, 516 inch nominal thickness. The detailed procedure used, i.e., type of weld rod, welding position, speed of welding, nondestructive testing requirements, etc., was in compliance with the ASME Boiler and Pressure Vessel Code. The cladding is ultrasonically inspected for lack of bond at intervals not to exceed 12 inches WR to the direction of welding. Unbonded areas equal to or in excess of calibration require additional scanning of the surrounding material until the boundary of the discontinuity is established. An area of unbounded clad in excess of acceptance standards is repaired.
Upon completion of all postweld heat treatments, the reactor vessel was hydrostatically tested, after which all weld surfaces, including those of welds used to repair material, were magnetic-particle inspected in accordance with Section III, paragraph N-618 of the ASME Boiler and Pressure Vessel Code.
Surveillance of the quality control program was also carried out during the manufacture of the vessel by the Windsor Quality Control Section of CE and by Northeast Nuclear Energy Company (NNECO) with an independent consultant. This work included independent review of radiographs, magnetic-particle tests, ultrasonic tests, and dye penetrant tests conducted during the manufacture of the vessel. A review of material certifications and vendor manufacturing and testing procedures was also conducted. Manufacturers records such as heat-treat logs, personnel qualification files and deviation files were also included in this review.
The nominal cladding thickness of the replacement reactor vessel closure head following machining (i.e., grinding) is quarter inch.
The cladding was ultrasonically examined such that each pass of the scanner overlap a minimum 10 percent of the transducer dimension perpendicular to the direction of the scan. Magnetic particle and liquid penetrant tests were conducted following hydrostatic test of the reactor vessel head to find any surface discontinuities. The magnetic particle and liquid penetrant tests were conducted in accordance with ASME Section III subsection NB 5000.
The replacement head was fabricated and inspected by Mitsubishi Heavy Industries at their facility. Representatives from Dominion Nuclear, CT (DNC) were present to witness the weld inspections and hydrostatic tests at various hold points. DNC also reviewed material certifications, test results conducted during fabrication.
The replacement pressurizer has a minimum stainless steel cladding of 1/5 inch. The cladding was ultrasonically examined such that each pass of the scanner overlap a minimum 10 percent of the 4.6-10 Rev. 35
MPS2 UFSAR transducer dimension perpendicular to the direction of the scan. Magnetic particle and liquid penetrant tests were conducted on 100% of the accessible surface to detect surface discontinuities were conducted in accordance with ASME Section III subsection NB 5000. In addition to the weld inspections, DNC personnel witnessed the hydrostatic test at various hold points at the fabricators shop for the replacement pressurizer.
4.6.6 IN-SERVICE INSPECTION A preoperational inspection was performed in compliance with Section XI of the ASME Boiler and Pressure Vessel Code, In-Service Inspection of Nuclear Reactor Coolant Systems, 1971, where possible. CE and Southwest Research Institute were retained to assist in the development of the in-service inspection program. Access was provided, where possible, to permit inspection of the areas listed in the code. In-service inspections are performed in accordance with Section XI.
A large portion of the insulation for the reactor vessel has been placed on the reactor cavity wall to permit inspection of the vessel outer surface. Essentially all vessel internals can be removed so that a complete visual internal inspection is possible and a volumetric internal inspection of the vessel is also possible. Pads have been welded to the outer surface of the reactor vessel to facilitate prompt location of welds for inspection purposes.
Access openings are provided on the permanent reactor cavity seal and the neutron shielding around the reactor vessel to facilitate inspection and maintenance of the neutron detector wells during refueling.
Biological shielding around the primary piping in the area of the reactor pressure vessel has been designed to afford access to the circumferential and RW welds, as well as the transition piece-to-nozzle welds.
All primary piping, as well as major components, excluding the reactor pressure vessel, have been provided with easily removable insulation in the areas of all welds and adjacent base metal requiring examination as defined by Section XI. Removable blanket insulation is provided on the CEDM, vent and instrumentation nozzles areas of the replacement reactor vessel closure head.
Plant arrangement and piping has been designed to assure that adequate access exists for either direct personnel access or for remote handling equipment to perform the examinations required by Section XI. Service connections, e.g., air, water, electricity, have been located adjacent or in close proximity to each inspection area. Consideration has been given to the type of examination and equipment requirements.
Access holes have been provided in the support skirt of each steam generator to provide a means of examining the tube sheet support stay cylinder weld.
4.6-11 Rev. 35
MPS2 UFSAR TABLE 4.6-1 RTNDT DETERMINATION FOR REACTOR VESSEL BASE METAL MILLSTONE UNIT NUMBER 2 Piece Number (Reference UPPER SHELF Drawing DROP CV ENERGY FOR E-233- CODE WEIGHT T50 T35 TCV RTNDT LONGITUDINAL 426-1) Number HEAT Number VESSEL LOCATION NDTT (°F) (°F) (°F) (°F) DIRECTION 203-02 C-500 4P2989 Vessel Flange +10F 5 50 70 10 149 5P3286-4310V1 204-02 C-511 C-5823-3A Bottom Head Dome -70 61 68 88 28 115 204-03A C-510-1 C-5823-3B Bottom Head Peel -60 -20 -2 18 -42 150 204-03C C-510-2 C-5892-3A -10 -22 -20 0 -60 135 204-03B C-510-3 C-5892-3B -40 20 20 40 -20 140 204-03D C-510-1 C-5823-3B -60 20 -2 18 -42 150 204-03E C-510-2 C-5892-3A -10 -22 -20 0 -60 135 204-03F C-510-3 C-5892-3B -40 20 20 40 -20 140 MPS2 UFSAR 205-02C C-503-1 9-7395-1-1 Inlet Nozzles -20 45 10 65 5 111 205-02B C-503-2 9-7401-1-2 +10 30 12 50 10 120 205-02A C-503-3 9-7454-1-3 -20 12 12 32 -28 108 205-02D C-503-4 9-7458-1-4 -60 30 20 50 -10 123 205-03A C-508-3 AV2999-9G-1283 Inlet Nozzle -20F 30 2 50 -10 146 Extension 205-03B C-508-1 AV2999-9G-1281 - 30 2 50 -10 205-03C C-508-2 AV2999-9G-1282 30 2 50 -10 205-03D C-508-4 AV2999-9G-1262 30 2 50 -10 205-06A C-502-1 9-7356-001 Outlet Nozzles -110 -20 -30 0 -60 132 205-06B C-502-2 9-7375-002 -130 16 -10 36 -24 103 4.6-12 Rev. 35
MPS2 UFSAR TABLE 4.6-1 RTNDT DETERMINATION FOR REACTOR VESSEL BASE METAL MILLSTONE UNIT NUMBER 2 Piece Number (Reference UPPER SHELF Drawing DROP CV ENERGY FOR E-233- CODE WEIGHT T50 T35 TCV RTNDT LONGITUDINAL 426-1) Number HEAT Number VESSEL LOCATION NDTT (°F) (°F) (°F) (°F) DIRECTION 205-07A C-509-1 AV3816-9G-1239 Outlet Nozzle Exten. -20 25 15 45 -15 141 205-07B C-509-2 AV3816-9G-1391 25 15 45 -15 215-01C C-504-1 C-5804-2 Upper Shell +10 62 53 82 22 118 215-01A C-504-2 C-5809-2 +10 62 48 82 22 131 215-01B C-504-3 C-5809-1 -10 55 52 75 15 125 215-02A C-505-1 C-5843-1 Intermediate Shell -20 - - - 8.1 118 215-02B C-505-2 C-5843-2 -10 - - - 17.5 123 215-02C C-505-3 C-5843-3 -10 - - - 5 115 215-03A C-506-1 C-5667-1 1/4T Lower Shell +10 - - - 7 112 MPS2 UFSAR 215-03C C-506-2 C-5667-2 1/4T Lower Shell -40F - - - -33.7 135 215-03B C-506-3 A-5518-1 1/4T -30 - - - -19.2 136 A1 03W62-1-1 Replacement Closure - 40 - 44 - 70 - - 40 148 Head B1 03W62-1-1 Replacement Closure - 40 - 18 - 22 - - 40 139 Head T50 (°F) corresponds to the temperature at which 50 ft-lb energy is absorbed.
T35 (°F) corresponds to the temperature at which 35 mils lateral expansion is exhibited.
TCV (°F) reflects the greater of T50 and T35 and incorporates guidance from MTEB 5-2 where necessary based upon available data.
4.6-13 Rev. 35
MPS2 UFSAR TABLE 4.6-2 CHARPY V-NOTCH AND DROP WEIGHT TEST VALUES - PRESSURIZER MILLSTONE UNIT NUMBER 2 Charpy Heat Drop Wt/ V-notch Test Charpy V-notch Lateral Expansion Description of Part Number RTNDT °F Temp °F Test Orientation Impact Energy (ft-lbs) (mils)
Upper Head T4987 -8 +52 0° 147-147-147 90-87-87 180° 160-172-157 87-94-90 Upper Shell T5086 +1 +61 0° 142-162-155 90-98-94 180° 144-128-125 90-87-90 Lower Shell T5085 -8 +52 0° 137-140-125 94-90-87 180° 127-111-113 87-79-79 Lower Head T4986 -17 +43 0° 177-169-153 94-90-87 180° 169-169-138 87-90-87 Support Skirt 4-1575 - +10 Base Ring 179-165-177 87-83-87 Skirt A 134-131-134 79-78-78 Skirt B 131-171-131 76-89-76 MPS2 UFSAR Manway / Vent 11746 - +59 Vent 116-119-115 79-83-83 Covers Manway 119-159-127 85-94-89 Lifting Lug 11764 - +59 Lug 1 130-167-133 91-94-93 Lug 2 136-144-174 93-94-94 Manway Stud N9952 - +10 - 37.6-37.6-36.9 29.3-28.9-28.1 Manway Nut 81025 - +10 - 50.1-48-7-49.4 41.0-39.5-42.2 Ventport Stud N9879 - +10 - 36.9-36.1-36.1 27.0-26.6-26.2 Ventport Nut 81025 - +10 - 50.1-48.7-49.4 41.0-39-5-42.2 4.6-14 Rev. 35
MPS2 UFSAR TABLE 4.6-3 CHARPY V-NOTCH AND DROP WEIGHT TEST VALUES - STEAM GENERATOR Steam LOCATION/ Generator RT NDT (°F) CHARPY V-NOTCH IMPACT TEST CVN TEST PART Number HEAT MATERIAL Unit Number (1) RESULTS (2) TEMP °F NOTES 5056021 W70029-1 Tubesheet / SA508 2 -70 126.9, 118.8, 104.4 146.5, 125.0, 94.0 -10 °F Class 3 5056021 W70022-1 1 -60 130.9, 146.5, 152.1 144.6, 134.9, 130.9 0° 5056020-2 88D108-1-1 Primary Head / 2 124.6, 147.5, 142.3 136.4, 142.3, 132.7 40 3 SA508, Class 3 (La) (La) 88C115 195.4, 190.3, 147.5 40 (La)
-30 114.3, 95.8, 112 104, 120, 119 (Me) 30 (ME) 0 173, 181, 151 (ME) 60 5056020-1 88D101-1-1 1 129, 111, 136 (La) 122, 125, 123 (La) 40 3 MPS2 UFSAR 88C110 157, 131, 123 (La) 40
-30 90, 98, 98 (ME) 30
-40 98.8, 90, 107 (ME) 20 0 142, 134, 164 (ME) 60 5056024-1 727957 Stay Cylinder / 1 98.1, 95.8, 97.3 112, 98.1, 102 +40 SA508, Class 3 120.2, 113, 116 126, 90.7, 101.7 +40
-35 99.5, 112, 110 95.8, 72.2, 116 +25
-35 129, 135.7, 127.6 123.9, 128.3, 131 +25 4.6-15 Rev. 35
MPS2 UFSAR TABLE 4.6-3 CHARPY V-NOTCH AND DROP WEIGHT TEST VALUES - STEAM GENERATOR (CONTINUED)
Steam LOCATION/ Generator RT NDT (°F) CHARPY V-NOTCH IMPACT TEST CVN TEST PART Number HEAT MATERIAL Unit Number (1) RESULTS (2) TEMP °F NOTES 5056024-2 727957 2 -27 106.9, 118, 112.8 104.7, 109.1, 113.6 +33
-35 104.7, 104.7, 109.1 +25
-27 115, 118, 120.9 +33 106, 110, 120 99.5, 104.7, 118 +40 122.4, 107.6, 112.8 126, 102, 109 +40 5056025-1 724015 Safe End-Inlet / 1 -8°F 130.5, 127.6, 118 +40 4 SA508, Class 1 (TANG)
-8°F 99.6, 80.4, 110.6 +52 5056025-2 724015 2 -8°F 103.2, 118, 109.1 +40 (TANG) MPS2 UFSAR
-8°F 103.3, 89.9, 97.36 +52 5056026-1, 2, 724015 Safe End-Outlet / 1&2 -8°F 115.8, 105.5, 109.1 99.5, 95.88, 88.5 +40 4 3, 4 SA508, Class 1 (TANG)
+52 5069670-2 87633-2 Manway 1 -22°F 109, 121, 124 (Top) +37.4 5069670- SA533, Grade B, -49 108, 108, 91 +10 Class 1 (Bottom) 5069670-5 87659-2 Manway SA 533, 1+2 -49 107.7, 97.5, 115 +10 Grade B, Class 1 (Top) 4.6-16 Rev. 35
MPS2 UFSAR TABLE 4.6-3 CHARPY V-NOTCH AND DROP WEIGHT TEST VALUES - STEAM GENERATOR (CONTINUED)
Steam LOCATION/ Generator RT NDT (°F) CHARPY V-NOTCH IMPACT TEST CVN TEST PART Number HEAT MATERIAL Unit Number (1) RESULTS (2) TEMP °F NOTES 5069679-1 87659-2 -40 137, 125.5, 119 +20 (Bottom) 5069670-3 87660-2 2 -40 143, 103, 107 (Top) +10
-31 106, 165, 140 +30 (Bottom) 5062982-1, 2 37314 Vessel Support 1+2 -40 181, 178, 140 (Top) +20 A533, Grade B, Class 1 (66961) -31 184, 200, 187 +30 (Bottom) 5062980-1, 2, 37410 1+2 -22 177, 190, 151 (Top) +40 MPS2 UFSAR 3, 4, 5, 6 (66922) -22 178, 160, 182 +40 (Bottom) 5056024-1 727957 Inlet Nozzle / 1 124, 113, 115 123, 129, 125 +40 SA508, Class 3
-45 71.5, 67.8, 81.8 73, 84.8, 70 -15 5056024-2 727957 2 134, 152, 136 178, 205, 179 +40
-62 58, 89, 87 88, 84, 60 -3 5056023-1 727957 Outlet Nozzle / 1 110, 111, 118 +40 SA508, Class 3 4.6-17 Rev. 35
MPS2 UFSAR TABLE 4.6-3 CHARPY V-NOTCH AND DROP WEIGHT TEST VALUES - STEAM GENERATOR (CONTINUED)
Steam LOCATION/ Generator RT NDT (°F) CHARPY V-NOTCH IMPACT TEST CVN TEST PART Number HEAT MATERIAL Unit Number (1) RESULTS (2) TEMP °F NOTES
-36 59, 74.5, 73 +42 5056023-2 727957 2 116, 125, 116 +40
-18 93, 112, 82.6 +42 5056023-3 727957 1 118, 119, 135 +40
-45 75, 67, 86 +15 5056023-4 727957 2 112, 122, 118 +40
-35 81.1, 85.56, 76.7 +25 Notes:
(1) RTNDT determined from drop WEIGHT and Charpy V-notch test results.
MPS2 UFSAR (2) Charpy-v-notch impact test results are listed in sets of three as tested. Specimen location and orientations were varied and removed for testing in accordance with ASME Section III requirements. Specimen location and orientation have been listed where possible.
(3) Specimen location identified as La and Me were orientated in longitudinal and meridional direction, respectively.
(4) Specimen location identified as TANG were oriented in tangential direction.
4.6-18 Rev. 35
MPS2 UFSAR TABLE 4.6-4 CHARPY V-NOTCH VALUES - PIPING Assembly PIECE CHARPY V-NOTCH VALUES Temperature Number Number CODE Number DESCRIPTION MATERIAL - FT-LB °F 503-01 502-20-1 C-4601-1 Pipe Segment SA-516 50 53 49 +10 Grade 70 Hot Leg 502-20-2 C-4601-2 Pipe Segment Grade 70 37 34 38 +10 502-02-1 C-4605-1 Ell Segment Grade 70 55 41 61 +10 502-02-2 C-4605-1 Ell Segment Grade 70 55 41 61 +10 506-02 C-4613-1 Nozzle A 105 43 +10 Forging Grade 2 512-03 C-4611 Nozzle Grade 2 43 36 32 +10 Forging 503-02 502-02-3 C-4605 Ell Segment SA 516 55 41 61 +10 Grade 70 MPS2 UFSAR Hot Leg 502-02-4 C-4605 Ell Segment Grade 70 55 41 61 +10 502-20-3 C-4601-3 Pipe Segment Grade 70 41 47 43 +10 502-20-4 C-4601-4 Pipe Segment Grade 70 45 47 51 +10 506-08 C-4612-1 Nozzle A 105 Grade 2 24 30 28 +10 Forging 504-01 502-12-1 C-4604-1 Pipe Segment SA 516 Grade 58 61 63 +10 70 4.6-19 Rev. 35
MPS2 UFSAR TABLE 4.6-4 CHARPY V-NOTCH VALUES - PIPING Assembly PIECE CHARPY V-NOTCH VALUES Temperature Number Number CODE Number DESCRIPTION MATERIAL - FT-LB °F Cold Leg 502-12-2 C-4604-2 Pipe Segment Grade 70 36 36 36 +10 Pump 502-08-1 C-4608 Ell Segment Grade 70 34 30 39 +10 Discharge 502-08-2 C-4608 Ell Segment Grade 70 34 30 39 +10 507-02-1 C-4615-1 Nozzle SA 105 Grade 43 36 32 +10 Forging 2 508-02-1 C-4610-1 Nozzle SA 182 Grade 98 95 104 +10 Forging F1 504-03 502-10-9 C-4609-2 Ell Segment SA 516 Grade 64 41 66 +10 70 Cold Leg 502 C-4609-2 Ell Segment Grade 70 64 41 66 +10 Pump 10 Discharge 502-18-1 C-4602-1 Pipe Segment Grade 70 58 67 62 +10 MPS2 UFSAR 502-18-2 C-4602-2 Pipe Segment Grade 70 58 67 62 +10 508-02-2 C-4610-2 Nozzle SA 182 Grade 95 94 110 +10 Forging F1 504-04 502-12-3 C-4604-3 Pipe Segment SA 516 Grade 59 66 60 +10 70 4.6-20 Rev. 35
MPS2 UFSAR TABLE 4.6-4 CHARPY V-NOTCH VALUES - PIPING Assembly PIECE CHARPY V-NOTCH VALUES Temperature Number Number CODE Number DESCRIPTION MATERIAL - FT-LB °F Cold Leg 502-12-4 C-4604-4 Pipe Segment Grade 70 59 66 60 +10 Pump 502-08-3 C-4608 Ell Segment Grade 70 34 30 39 +10 Discharge 502-08-4 C-4608 Ell Segment Grade 70 34 30 39 +10 507-02-2 C-4615-2 Nozzle SA 105 Grade 43 36 32 +10 Forging 2 508-02-3 C-4610-3 Nozzle SA 182 Grade 106 120 114 +10 Forging F1 507-07-2 C-4616-2R Nozzle SA 105 Grade 43 36 32 +10 Forging 2 504-05 502 C-4609-2 Ell Segment SA 516 Grade 64 41 66 +10 11 70 Cold Leg 502- C-4609-2 Ell Segment Grade 70 64 41 66 +10 MPS2 UFSAR Pump 10-12 Discharge 502-18-3 C-4602-3 Pipe Segment Grade 70 58 61 57 +10 502-18-4 C-4602-4 Pipe Segment Grade 70 58 61 57 +10 508-02-4 C-4610-4 Nozzle SA 182 Grade 109 76 92 +10 Forging F1 507-07-1 C-4616-1 Nozzle SA 105 Grade 43 36 32 +10 Forging 2 503-05-1 502-04-1 C-4606-1 Ell Segment SA 516 Grade 58 51 50 +10 70 Cold Leg 502-04-2 C-4606-1 Ell Segment Grade 70 58 51 50 +10 Pump Suction 4.6-21 Rev. 35
MPS2 UFSAR TABLE 4.6-4 CHARPY V-NOTCH VALUES - PIPING Assembly PIECE CHARPY V-NOTCH VALUES Temperature Number Number CODE Number DESCRIPTION MATERIAL - FT-LB °F 503-05-2 502-04-3 C-4606-1 Ell Segment SA 516 Grade 58 51 50 +10 70 Cold Leg 502-04-4 C-4606-1 Ell Segment Grade 70 58 51 50 +10 Pump Suction 503-05-3 502-04-5 C-4606-2 Ell Segment SA 516 Grade 44 49 53 +10 70 Cold Leg 502-04-6 C-4606-2 Ell Segment Grade 70 44 49 53 +10 Pump Suction 503-03-1 502-06-1 C-4607 Ell Segment SA 516 Grade 47 55 52 +10 70 503-05-4 502-04-7 C-4606-2 Ell Segment SA 516 Grade 44 49 53 +10 70 MPS2 UFSAR Cold Leg 502-04-8 C-4606-2 Ell Segment Grade 70 44 49 53 +10 Pump Suction Cold Leg 502-06-2 C-4607 Ell Segment Grade 70 47 55 52 +10 Pump Suction 502-16-1 C-4603-1 Pipe Segment SA 516 63 70 64 +10 502-16-2 C-4603-2 Pipe Segment Grade 70 63 70 64 +10 503-03-2 502-06-3 C-4607 Ell Segment SA 516 Grade 47 55 52 +10 70 Cold Leg 502-06-4 C-4607 Ell Segment Grade 70 47 55 52 +10 Pump Suction 502-16-1 C-4603-1 Pipe Segment Grade 70 63 70 64 +10 502-16-2 C-4603-2 Pipe Segment Grade 70 63 70 64 +10 4.6-22 Rev. 35
MPS2 UFSAR TABLE 4.6-4 CHARPY V-NOTCH VALUES - PIPING Assembly PIECE CHARPY V-NOTCH VALUES Temperature Number Number CODE Number DESCRIPTION MATERIAL - FT-LB °F 503-03-3 502-06-5 C-4607 Ell Segment SA 516 Grade 47 55 52 +10 70 Cold Leg 502-06-6 C-4607 Ell Segment Grade 70 47 55 52 +10 Pump Suction 502-16-1 C-4603-1 Pipe Segment Grade 70 63 70 64 +10 502-16-2 C-4603-2 Pipe Segment Grade 70 63 70 64 +10 503-03-4 502-06-7 C-4607 Ell Segment SA 516 Grade 47 55 52 +10 70 Cold Leg 502-06-8 C-4607 Ell Segment Grade 70 47 55 52 +10 Pump Suction 502-16-1 C-4603-1 Pipe Segment Grade 70 63 70 64 +10 502-16-2 C-4603-2 Pipe Segment Grade 70 63 70 64 503-07-1 502-14-1 C-4604-5 Pipe Segment SA 516 Grade 23 21 20 +10 MPS2 UFSAR 70 Cold Leg 502-14-2 C-4604-6 Pipe Segment Grade 70 52 57 54 +10 Pump Suction 502-10-1 C-4609-1 Pipe Segment Grade 70 50 43 35 +10 502-10-2 C-4609-1 Pipe Segment Grade 70 50 43 35 +10 507-10-4 C-4614-4R Nozzle SA 105 Grade 38 42 43 +10 Forging 2 4.6-23 Rev. 35
MPS2 UFSAR TABLE 4.6-4 CHARPY V-NOTCH VALUES - PIPING Assembly PIECE CHARPY V-NOTCH VALUES Temperature Number Number CODE Number DESCRIPTION MATERIAL - FT-LB °F 503-07-2 502-14-1 C-4604-5 Pipe Segment SA 516 Grade 23 21 20 +10 70 Cold Leg 502-14-2 C-4604-6 Pipe Segment Grade 70 52 57 54 +10 Pump Suction 502-10-3 C-4609-1 Ell Segment Grade 70 50 43 35 +10 502-10-4 C-4609-1 Ell Segment Grade 70 50 43 35 +10 507-10-1 C-4614-3R Nozzle SA 105 Grade 38 42 43 +10 Forging 2 505-10-1 502-14-3 C-4604-7 Pipe Segment SA 516 Grade 52 57 54 +10 70 Cold Leg 502-14-4 C-4604-8 Pipe Segment Grade 70 58 61 63 +10 Pump Suction 502-10-5 C-4609-1 Ell Segment Grade 70 50 43 35 +10 MPS2 UFSAR 502-10-6 C-4609-1 Ell Segment Grade 70 50 43 35 +10 507-10-2 C-4614-2 Nozzle SA 105 Grade 43 36 32 +10 Forging 2 505-10-2 502-14-3 C-4604-7 Pipe Segment SA 516 Grade 52 57 54 +10 70 Cold Leg 502-14-4 C-4604-8 Pipe Segment Grade 70 58 61 63 +10 Pump Suction 502-10-7 C-4609-2 Ell Segment Grade 70 64 41 66 +10 502-10-8 C-4609-2 Ell Segment Grade 70 64 41 66 +10 507-10-3 C-4614-1 Nozzle SA 105 Grade 43 36 32 +10 Forging 2 4.6-24 Rev. 35
MPS2 UFSAR TABLE 4.6-5 PLATE AND WELD METAL CHEMICAL ANALYSIS Weight Percent Plate 1/4 T-ID Weld 1/4 T-OD Weld Element C-506-1 C-506-2/C-506-3 C-506-2/C-506-3 Si 0.12 0.17 0.15 S 0.014 0.013 0.013 P 0.006 0.015 0.016 Mn 1.26 1.13 1.13 C 0.21 0.12 0.12 Cr 0.10 0.04 0.05 Ni 0.61 0.06 0.06 Mo 0.62 0.54 0.53 V 0.004 0.006 0.007 Cb < 0.01 < 0.01 < 0.01 B 0.0006 0.0003 0.0003 Co 0.011 0.009 0.009 Cu 0.14 0.30 0.21 Al 0.020 < 0.001 < 0.01 W < 0.01 0.01 < 0.01 Ti < 0.01 < 0.01 < 0.01 As 0.011 0.011 0.012 Sn 0.009 0.004 0.003 Zr 0.002 0.002 0.002 N2 0.009 0.008 0.009 4.6-25 Rev. 35
MPS2 UFSAR TABLE 4.6-6 BELTLINE MECHANICAL TEST PROPERTIES - REACTOR VESSEL SURVEILLANCE MATERIALS NDTT 30 ft-lb 50 ft-lb 35 Mils Lat. RTNDT Upper Shelf RT Yield a
Material Code Number Orientation (°F) Fix (°F) Fix (°F) Exp. Fix (°F) (°F) (ft-lb) (ksi)
Base Metal C-506-1 Transverse -10 22 66 54 6 106.5 67 Plate (WR)
Base Metal C-506-1 Longitudinal -10 36 84 65 24 b 124.5 67 Plate (RW)
Weld Metal C-506-2 / C- Transverse -60 -26 5 2 -55 129.5 76 506-3 (WR)
HAZ Metal C-506-1 Transverse -30 -44 35 34 -25 123.0 68 (WR)
- a. With respect to the plates major rolling direction for base metal; with respect to the welding direction for weld and HAZ.
- b. Not valid per 10 CFR 50, Appendix G. MPS2 UFSAR 4.6-26 Rev. 35
MPS2 UFSAR TABLE 4.6-7 TENSILE TEST PROPERTIES - REACTOR VESSEL SURVEILLANCE MATERIALS Plate Code Test Temp Yield Strength Tensile Strength Elongation R.A.
a Material Number Orientation (F) (ksi) (ksi) TE(%)/UE(%) (%)
Base Metal C-506-1 Transverse (WR) 67 88 27/11 68 Plate 250 64 81 25/10 67 550 58 84 23/09 62 Base Metal C-506-1 Longitudinal 71 67 86 29/12 71 (RW) 250 61 79 26/10 70 550 56 83 26/10 69 Weld Metal C-506-2/C-506-3 Longitudinal 71 76 86 28/11 74 (RW) 250 74 81 26/09 71 550 67 85 25/10 65 HAZ Metal C-506-1 Transverse (WR) 71 68 88 24/09 70 MPS2 UFSAR 250 60 80 25/08 72 550 62 83 21/07 68
- a. With respect to the plates major rolling direction for base metal; with respect to the welding direction for weld and HAZ.
4.6-27 Rev. 35
MPS2 UFSAR TABLE 4.6-8
SUMMARY
OF SPECIMENS PROVIDED FOR EACH EXPOSURE LOCATION Base Base Capsule Metal Metal Base Weld Weld HAZ Location on Impact Impact Metal Metal Metal Impac HAZ Reference Total Specimens Vessel Wall L (a) T (b) Tensile Impact Tensile t Tensile Impact (c) Impact Tensile 83° 12 12 3 12 3 12 3 - 48 9 97° 12 12 3 12 3 12 3 - 48 9 104° 12 - 3 12 3 12 3 12 48 9 263° 12 - 3 12 3 12 3 12 48 9 277° 12 12 3 12 3 12 3 - 48 9 284° 12 12 3 12 3 12 3 - 48 9 72 48 18 72 18 72 18 24 288 54 (a) L = Longitudinal MPS2 UFSAR (b) T = Transverse (c) Reference material correlation monitors 4.6-28 Rev. 35
MPS2 UFSAR TABLE 4.6-9 CAPSULE REMOVAL SCHEDULE REMOVAL LEAD TIME FLUENCE CAPSULE LOCATION FACTOR a (EFPY) b (n/cm2, >1.0MeV) (a)
W-97 97° 1.40 3.0 3.24 x 1018 c W-104 104° 0.95 10.0 9.49 x 1018 (c)
W-97 d 97° 10.0 --
W-83 83° 1.31 15.3 1.74 x 1019 (c)
W-277 277° 1.31 EOL e See Note (d)
W-263 263° 1.31 Standby --
W-284 284° 0.97 Standby --
- a. Updated in Capsule W-83 dosimetry analysis
- b. Effective Full Power Years (EFPY) from plant startup
- c. Plant specific evaluation
- d. Flux Monitor
- e. EOL is defined as the end-of-license period corresponding to the original 40 year license.
Capsule W-277 is projected to receive 1.31 times the reactor vessel peak EOL surface fluence of 2.4 x 1019 n/cm2 (E > 1.0 MeV). Capsule W-277 will receive the vessel peak EOL surface fluence at 23.2 EFPY. It will be removed before it receives twice the peak vessel surface fluence of 4.80 x 1019 n/cm2 (E > 1.0 MeV).
4.6-29 Rev. 35
MPS2 UFSAR TABLE 4.6-10 INSPECTION OF REACTOR COOLANT SYSTEM COMPONENTS DURING FABRICATION AND CONSTRUCTION
- 1. Reactor Vessel Forgings Flange UT, MT Studs UT, MT Cladding UT, PT Nozzles UT, MT Plates UT, MT Cladding UT, PT Welds Main Seams RT, MT CRD Head Nozzle Connection UT, PT, ET Instrumentation and Vent Nozzles UT, PT Main Nozzles to Shell RT, MT Cladding UT, PT Nozzle Safe Ends RT, MT Vessel Support Buildup UT, MT All Welds - After Hydrostatic Test MT, PT 1
- 2. Steam Generator Tube Sheet Forging UT, MT Cladding UT, PT Primary Head Forging UT, MT Cladding UT, PT Secondary Shell and Head Plates UT, MT
- 1. Liquid penetrant tests of J-welds only.
4.6-30 Rev. 35
MPS2 UFSAR Tubes UT, ET Nozzles (Forgings) UT, MT Studs MT Welds Shell, Longitudinal RT, MT Shell, Circumferential RT, MT Cladding UT, PT Nozzles to Shell RT, MT Tube-to-Tube Sheet PT Instrument Connections MT Temporary Attachments After Removal MT All Welds - After Hydrostatic Test MT Nozzle Safe Ends RT, (MT or PT)
Level Nozzles MT
- 3. Replacement Pressurizer Heads, Forging RT, MT Cladding UT, PT, MT Shell, Forging RT, MT Cladding UT, PT, MT Heaters, Sheath UT, PT Nozzles (Integral to Heads) UT, MT Studs (Manway, Ventport) UT, PT Welds Shell to Shell and Shell to Heads Circumferential RT, MT, PT, UT Cladding UT, PT, MT Nozzle Safe Ends RT, PT Instrument Connections PT Support Skirt RT, PT, UT 4.6-31 Rev. 35
MPS2 UFSAR Temporary Attachments After Removal MT Heads to Shell and Shell to Shell Welds PT Heater Assembly RT, PT
- 4. Pumps Castings RT, PT Forgings UT, PT Welds Circumferential RT, PT Instrument Connections PT All Welds After Hydrostatic Test PT
- 5. Piping Fittings RT, PT Pipe RT, PT Nozzles RT, PT Welds UT, PT Circumferential RT, PT, MT Nozzles to Run Pipe RT, PT Instrument Connections PT Cladding UT, PT Legend:
RT -Radiographic PT - Dye Penetrant ET - Eddy Current UT - Ultrasonic MT - Magnetic Particle 4.6-32 Rev. 35
MPS2 UFSAR TABLE 4.6-11 REACTOR COOLANT SYSTEM INSPECTION C-E REQUIREMENTS Reactor Vessel
<test> C-E Requirements Code Requirements Ultrasonic Testing (UT) 1. UT of Weld Clad for bond. 1. None Replacement Reactor Vessel Head (a)
<test> C-E Requirements Code Requirements Ultrasonic Testing (UT)) 1. Indications that produce an ASME Section V, Article 23, SA amplitude greater than the 578 amplitude received from the one-eighth inch flat bottom hole and less than the amplitude from the three-eighth inch flat bottom hole are to be characterized as to size, length, and depth below the surface.
Indications exceeding the following are unacceptable.
Depth from Clad Surface Length of Indication Up to 0.02 inches 0.375 inches 0.02 inches - 0.06 inches 1.0 inches 0.06 inches - 0.1 inches 3.0 inches Over 0.10 inches 6.0 inches 4.6-33 Rev. 35
MPS2 UFSAR Replacement Reactor Vessel Head (continued)
<test> C-E Requirements Code Requirements Liquid Penetrant test (PT) 1. The final PT of J-weld and ASME Section III, NB 5245 the half-inch area adjacent to the weld for CEDM adapters, instrument tube connections shall allow no indications of defects.
<test> C-E Requirements Code Requirements Ultrasonic Test (UT) 1. UT for Defects in Tube Sheet Clad UT 1. None of Weld Clad for bond.
<test> C-E Requirements Code Requirements Ultrasonic Testing 1. Indications that produce an amplitude ASME Section V, Article (UT) greater than the amplitude received from 23, SA 578 the one-eighth inch flat bottom hole and less than the amplitude from the three-eighth inch flat bottom hole are to be characterized as to their length, and depth below the surface. Indications exceeding the following are unacceptable.
Depth from Clad Surface Length of Indication Up to 0.03 inches 0.375 inches 0.03 inch - 0.06 inch 1.0 inches 0.06 inch - 0.125 inch 3.0 inches Over 0.125 inch 6.0 inches (a) This is a Dominion requirement and not a CE requirement. The reactor vessel head and replacement pressurizer were replaced in accordance with Dominion Purchase Specifications.
4.6-34 Rev. 35
MPS2 UFSAR TABLE 4.6-12 RTPTS VALUES AT 54 EFPY Neutron Initial Fluence Chemical Chemical Chemist Margin Component Content: Content: Ni ry RTNDT Term (1019n/ RTPTS Vessel Location Identification Cu (%) (%) Factor (°F) (°F) cm2) (°F)
Intermediate C-505-1 0.13 0.61 91.3 8.1 34 3.83 165.1 Shell C-505-2 0.13 0.62 91.5 17.5 34 3.83 174.7 Course Plates C-505-3 0.13 0.62 91.5 5 34 3.83 162.2 Lower C-506-1 0.15 0.60 110.0 7 34 3.78 188.8 Shell C-506-2 0.15 0.61 110.0 -33.7 34 3.78 163.5 Course Plates C-506-3 0.14 0.66 101.5 -19.2 34 3.78 183.6 Intermediate Shell Axial 2-203 A (Heat A8746) 0.15 0.13 77.7 -56 66 2.83 114.6 Welds 2-203 B/C (Heat 0.15 0.13 77.7 -56 66 3.53 114.6 MPS2 UFSAR A8746)
Lower Shell Axial Welds 3-203 A (Heat A8746) 0.15 0.13 77.7 -56 66 3.83 114.6 3-203 B/C (Heat 0.15 0.13 77.7 -56 66 2.50 114.6 A8746)
Intermediate-to- Lower 9-203 (Heat 10137) 0.22 0.04 100.0 -56.3 56 3.78 134.1 Shell Girth Weld 9-203 (Heat 90136) 0.27 0.07 124.3 -56.3 56 3.78 166.7 4.6-35 Rev. 35
MPS2 UFSAR TABLE 4.6-13 ADJUSTED REFERENCE TEMPERATURES (ART) PROJECTIONS Neutron Fluence (a), 1019 n/cm2 (E>1 ART Projections (b) 54 MeV) 54 EFPY EFPY Component Vessel Location Identification 1/4T 3/4T 1/4T 3/4T Intermediate C-505-1 2.283 0.811 153.8 128.0 Shell C-505-2 2.283 0.811 163.4 137.6 Course Plates C-505-3 2.283 0.811 150.9 125.1 Lower C-506-1 2.253 0.809 175.2 144.1 Shell C-506-2 2.253 0.809 134.5 103.4 Course Plates C-506-3 2.253 0.809 138.6 110.0 Intermediate Shell Axial Welds 2-203 A (Heat A8746) 2.283 3.811 104.6 82.6 2-203 B (Heat A8746) 1.508 0.536 96.0 73.7 2-203 C (Heat A8746) 1.508 0.536 96.0 73.7 MPS2 UFSAR Lower Shell Axial Welds 3-203 A (Heat A8746) 2.283 0.811 104.6 82.6 3-203 B (Heat A8746) 1.490 0.529 95.8 73.4 3-203 C (Heat A8746) 1.490 0.529 95.8 73.4 Intermediate to Lower Shell Girth 9-203 (Heat 10137) 2.253 0.800 121.7 93.5 Weld 9-203 (Heat 90136) 2.253 0.800 151.3 116.2 (a) Maximum neutron fluence for vessel location.
(b) Adjusted reference temperature projections based on best-estimate copper and nickel content, chemistry factor, initial RTNDT and margin given in Table 4.6-12.
4.6-36 Rev. 35
MPS-2 FSAR FIGURE 4.6-1 LOCATION OF SURVEILLANCE CAPSULE ASSEMBLIES 1800
,r-------..V, Outlet Nozzle I
,f I ,
';'---,-""\ Inlet
\ Nozzle
- )
,I
~ *'~.I...---263° Core Vessel Midplane Capsule I
mO Assembly
,~
I \
I
,.1 \, 284°
\ ,]
\\ ./
I
\
\,,"---' '.-t--J Core
'---.j~tt-- Support Reactor Barrel Vessel I Enlarged Plan View rP Elevation View JUN 29 1984 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-2 TYPICAL SURVEILLANCE CAPSULE ASSEMBLY
...-.--- Lock Assembly Tensile - Monitor } Wedge Coupling Assembly Compartment Charpy Impact Compartments Tensile - Monitor Compartment Charpy Impact Compartments Tensile - Monitor Compartment JUN 1 0 1982 JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-3 TYPICAL CHARPY IMPACT COMPARTMENT ASSEMBLY Wedge Coupling - End Cap Charpy Impact Specimens Spacers -----~
Rectangular Tubing Wedge Coupling - End Cap JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-4 TYPICAL TENSILE-MONITOR COMPARTMENT ASSEMBLY Flux Spectrum Monitor Cadmium Shielded Flux Monitor Housing ---~~
Stainless Steel Tubing Stainless Steel Tubing Cadmium Shield Treshold Detector Threshold Detector Flux Spectrum Monitor Temperature Monitor ----------1 .....--Quartz Tubing
~ lJJ Weight Temperature Monitor Low Melting Alloy Housing Tensile Specimen Split Spacer Tensile Specimen Housing - _....~
Rectangular Tubing Wedge Coupling - End Cap JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-5 BASE METAL - WR (TRANSVERSE) PLATE C-506-1 IMPACT ENERGY VS TEMPERATURE 120 (1) 10 100 o
~
>-... 80
'"Z a:
141
......,u GO f
. ~ 40 8
20 04--_~-_"'-"_---'---"""",,--_..I..-_---I~_-A._---'
~O .-40 0 40 80 UO 160 200 240 TE.ST1:£MPERATlJRE, of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-6 BASE METAL - WR (TRANSVERSE) PLATE C-506-1 LATERAL EXPANSION VERSUS TEMPERATURE 100,..----r----,.---.,....---.,.......---,----"T---,-----,.
(I)
~ 80
~
Z 0
en 60 z
4:
0-X W
..J c(
40 0:
OJ l-e{
-J 20 O__ ----'-----I.---L-__ -L-_ _--L_ _---lL..-_ _....I.- _
- 80 -40 o 40 50 120 100 200 240 TEST1EMPERATURE. of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-7 BASE METAL - RW (LONGITUDINAL) PLATE C-506-1 IMPACT ENERGY VERSUS TEMPERATURE 140 r---~--r------'r-----.----,.----.----r--_
120 C/) 100 co
...J .
..=-
u.
>-' 80 C) 0:
w Z
w 60 to-U
~
0..
~ 0 40 20 o
- 80 -40 o 40 so 120 160 200 240 TEST TEMPERATURE. of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-8 BASE METAL - RW (LOGITUDINAL) PLATE C-506-1 LATERAL EXPANSION VS TEMPERATURE 100 r----r----,r-----r----r---r----"""T"""----r--~
(J)
..J 80
~
Z 0
60
'"zc:r.
0..
0 X
W
..J 40 0
~
a:
w I-
~
..J 20 O""C-_ _- - l - J..-_ _...J-._ _ ~ """"__ ___'__ _______ __ l
- 80 o 40 80 120 160 200 240 TES-r TEMPERATURE., of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-9 WELD METAL PLATE C-506-2/C-506-3 IMPACT ENERGY VS TEMPERATURE
~o 1~O 120
.en 100 m
..J 0
~
(!)
80 a:
w zUJ
...u 60 c(
c.
-~
40 0
o'-----'---"-----a...--""'----"------.l.----'----I
-120 ..SO -40 0 40 80 l~O 160 200 TESi TEMPERATURE, OF JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-10 WELD METAL, PLATE C-506-2/C-506-3 LATERAL EXPANSION VS TEMPERATURE 100 ---....__---,------r----,---r----y---....,...----,
80 (I)
..J
~
Z..
-z 0
en 60 c(
a..
X
.W
..J 40 4:
cc 0 w
t-
-S 20 o
- 120 ..80 *40 a 40 80 120 160 200 TEST TEMPERATURE. of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-11 HAZ METAL, PLATE C-506-1 IMPACT ENERGY VERSUS TEMPERATURE 140 120 0
100 0
CI)
/lI)
-J
~
U.
>=
C-'
80 a::
w
- 2 UJ . 60 0 u
~
~
~
40 0° 20 0L-_"'--_--.lL-_---L_ _--...._ _--'-_ _ ~ _ _....L__ _J....J
- 150 ~120 *80 -40 a 40 80 120 160 TEST TEMPERA1"URE, of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-12 HAZ METAL, PLATE C-506-1 LATERAL EXPANSION VERSUS TEMPERATURE 100 r----,...--~r__--_r_--__r---_r_--_r_--__,.---~
(I) 80
-J 2
2 0 60
(/)
2
<t:.
0-X w
..J 40
<t:
c:
UJ t-0°
<t 20
-J
_ _.......-_.--l_-_---J oL.-_-L_-.........;~---'---_---I.._--.---
- 150 *120 *80 -40 0 40 80 120 160 TEST TEMPERATURE. of JUN 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4.6-13 SRM (HSST PLATE 01MY - LONGITUDINAL) IMPACT ENERGY VERSUS TEMPERATURE 140 120 -
(I) 100 co
...I
..=.
u..
~ 80 C) tt:
w Z
w 60 I-o 4:
0-
~
40 -
20 o
- 80 o 40 80 120 160 200 240 TEST TEMPERATURE. of JUN 10 1982 Rev. 24.2
Rev. 24.2 JUN 10 1982
MPS2 UFSAR 4.A SEISMIC ANALYSIS OF REACTOR COOLANT SYSTEM 4.A.1 INTRODUCTION The purpose of this appendix is to describe the methods employed and present the results obtained by dynamic seismic analyses of the reactor coolant system components. These analyses were performed to confirm the adequacy of the seismic loadings specified for the design of the components and the supports of the reactor coolant system which includes the reactor vessel, the steam generators, the reactor coolant pumps, the pressurizer, and the interconnecting reactor coolant piping.
Dynamic seismic analysis of the reactor vessel internals was performed separately and is discussed in Appendix 3.A.
4.A.2 METHOD OF ANALYSIS 4.A.2.1 General The seismic analysis of the reactor coolant system (RCS) components was performed using either normal mode or direct integration theory in conjunction with time history and response spectrum techniques, as appropriate.
Time history techniques were employed in the analysis of the reactor vessel, the two steam generators, the four reactor coolant pumps and the interconnecting reactor coolant piping. In the analysis of these components, a single composite mathematical model, which included integral representations of each of the components and connecting piping, was employed to account for the interacting effects of dynamic coupling. The analysis of these dynamically coupled multi-supported components utilized different time dependent input excitations applied simultaneously to each support.
The analyses of the pressurizer and the surge line piping employed separate, uncoupled, mathematical models and utilized response spectrum techniques.
The input data, time histories and response spectra, applied in the analyses were provided by the analysis of the containment structure internal support structure described in Section 5.8.
The RCS components were analyzed using either modal or proportional (Rayleigh) methods of damping. Except for analysis of the surge line piping, all modal analyses used a constant damping factor of 1% of critical damping for all active modes. In the analysis of the surge line piping, a damping factor of 0.5 % of critical damping was used for each mode. When proportional damping was used, Alpha and Beta were conservatively selected to provide less than 1% of critical damping at the significant frequencies of response of the major components.
4.A-1 Rev. 35
MPS2 UFSAR 4.A.2.2 Mathematical Models In the descriptions of the mathematical models which follow, the spatial orientations are defined by the set of orthogonal axes where Y is in the vertical direction, and X and Z are in the horizontal plane, in the directions indicated on the appropriate figure. The mathematical representation of the section properties of the structural elements employs a 12 by 12 stiffness matrix for the three-dimensional space frame models, and employs a 6 x 6 stiffness matrix for the two dimensional plane frame model. Elbows in piping runs include the in-plane/out-of-plane bending flexibility factors as specified in the ASME Code,Section III.
4.A.2.2.1 Reactor Coolant System - Coupled Components A schematic diagram of the composite mathematical model, designated MS-2, used in the original plant design analyses of the dynamically coupled components of the reactor coolant system is presented in Figure 4.A-1 and 4.A-1A. This model, Figure 4.A-1, includes 19 mass points with a total 47 dynamic degrees of freedom. The mass points and corresponding dynamic degrees of freedom are distributed to provide appropriate representations of the dynamic characteristic of the components, as follows: the reactor vessel, with internals, is represented by 5 mass points with a total of 13 dynamic degrees of freedom; each of the two steam generators are represented by 3 mass points with a total of 7 dynamic degrees of freedom; and each of the four reactor coolant pumps are represented by 2 mass points with a total of 5 dynamic degrees of freedom. The relatively small mass of the interconnecting reactor coolant piping is lumped proportionately with the masses of the adjoining components.
Number of Mass Number of Dynamic Degrees of
<component> Points Freedom Reactor Vessel and Internals 5 13 Steam Generators (2) 6 14 R.C. Pumps (4) 8 20 Total 19 47 The mathematical model, Figure 4.A-1, as defined, provides a complete three dimensional representation of the dynamic response of the coupled components to seismic excitations in both the horizontal and vertical directions. The mass is distributed at the selected mass points and corresponding translational degrees of freedom are retained to include rotary inertial effects of the components. The total mass of the entire coupled system is dynamically active in each of the three coordinate directions.
In addition to Model MS-2 described above, a second model of the coupled components, designated Model RV14, was formulated for the original plant design to incorporate a more detailed representation of the reactor vessel assembly. With the exception of the representation of the reactor vessel assembly, Model RV14 is identical to Model MS-2, Figure 4.A-1. A schematic diagram of the representation of the reactor vessel assembly incorporated into Model RV14 is presented in Figure 4.A-2. This more detailed representation of the reactor vessel assembly 4.A-2 Rev. 35
MPS2 UFSAR consists of 15 mass points with a total of 33 dynamic degrees of freedom and includes a 10 mass point, 22 dynamic degrees of freedom representation of the reactor vessel internals. The representation of the reactor vessel internals was formulated in conjunction with the analysis of the reactor vessel internals discussed in Appendix 3.A, and was designed to simulate the dynamic characteristics of the models used in that analysis. The coupled Model RV14 was used to generate time histories of absolute accelerations at the reactor vessel flange used as forcing functions in the analysis of the reactor vessel internals.
Coupled model RV14, modified to delete the reactor internals representation of the thermal shield and to reflect current design steam generator properties, was also used in analyses to determine the effects of the replacement steam generators on RCS responses. This modified model representation consists of 27 mass points with 63 dynamic degrees of freedom.
Number of Mass Number of Dynamic Degrees of
<component> Points Freedom Reactor Vessel 5 11 Reactor Internals 8 18 Steam Generators(2) 6 14 Reactor Coolant Pumps (4) 8 20 Total 27 63 4.A.2.2.2 Pressurizer The mathematical model employed in the analysis of the pressurizer is shown schematically in Figure 4.A-3. This lumped parameter, planer model provides a multi-mass representation of the axially symmetric pressurizer and includes 5 mass points with a total of 6 dynamic degrees of freedom.
The replacement pressurizer was analyzed using BWSPAN for both operating basis and safe shutdown earthquake using the response spectrum method. The seismic excitation is applied at the support skirt elevation. The significant change to the analysis from the original pressurizer analysis is that the analysis is performed at 65% water level. The seismic directional responses are combined by the absolute sum of each horizontal and vertical response of the spectrum analysis.
4.A.2.2.3 Surge Line The lumped parameter, multi-mass mathematical model employed in the analysis of the surge line is shown schematically in Figure 4.A-4. The surge line is modeled as a three dimensional piping run with end points anchored at the attachments to the pressurizer and the reactor vessel outlet piping. In the definition of the mathematical model, 10 mass points with a total of 27 dynamic degrees of freedom were selected to provide a complete three-dimensional representation of the dynamic response of the surge line. All supports and restraints defined for the surge line assembly 4.A-3 Rev. 35
MPS2 UFSAR are included in the mathematical model. The total mass of the surge line is dynamically active in each of the three coordinate directions.
4.A.2.3 Calculations 4.A.2.3.1 General As applied in the analysis, the simultaneous equations of motion for linear structural systems with viscous damping can be written, Reference 4.A-1:
MX** + CX* + KX = - MY** - K ms X s where:
M = diagonal matrix of lumped masses C = square symmetric damping matrix K = square symmetric stiffness matrix which defines the mass point force-displacement relationship.
Y** = column matrix with elements equal to the absolute acceleration of the datum support in the coordinate direction of the related dynamic degree of freedom of the structural system.
Kms = rectangular matrix of stiffness coefficients which defines the mass point force, non-datum support displacement relationship.
Xs = column matrix of displacements relative to the datum at non-datum supports.
X = column matrix of mass point displacements relative to the datum.
X* = column matrix of mass point velocities relative to the datum.
X** = column matrix of mass point accelerations relative to the datum.
In this form, the equations define the dynamic response of a multi-mass structural system subjected to time dependent support motion. In the analysis of systems with multiple supports, such as the coupled components of the reactor coolant system, the equations provide for different time-dependent input motions at each of the supports. In this case, one of the supports of the system is designated the reference, or datum, from which the motions of all other points of the structural system are measured. The reactor vessel support was designated as the datum in the analyses of the coupled components of the reactor coolant system.
Normal mode theory, as described in References 4.A-1 and 4.A-2, was employed to reduce the equations of motion to a system of independent equations in terms of the normal modes for the modal superposition time-history and spectrum analyses of the reactor coolant system components. For direct integration time-history analyses, the equations of motion were solved 4.A-4 Rev. 35
MPS2 UFSAR using numerical integration methods with an integration time step of 0.001 second. In the analyses, the dynamic response of the components was determined for seismic input excitations in each of the three global coordinate directions: X (east-west), Y (vertical) and Z (north-south). The dynamic responses to vertical seismic excitation were found for both the case of initial support displacement upward and the case of initial support displacement downward. These responses were combined to determine the most severe combinations produced by the effects of seismic excitations in each of the horizontal directions applied simultaneously with either seismic excitation in the vertical direction.
4.A.2.3.2 Frequency Analysis An eigenvalue analysis was performed utilizing the ICES STRUDL II computer code, Reference 4.A-3, to calculate the mode shapes and natural frequencies of the original plant design composite mathematical models. Modifications to the standard ICES STRUDL II program have been implemented by Combustion Engineering to include a Jacobi diagonalization procedure in the eigenvalue analysis and to provide appropriate influence coefficients and stiffness matrices for use in the response and reaction calculations.
The natural frequencies and dominant degrees of freedom calculated are shown in Table 4.A-1 for all modes used in the analysis of the reactor coolant system Model MS-2, the surge line and the pressurizer.
An eigenvalue analysis was also performed utilizing the ANSYS computer code, Reference 4.A-5, to calculate the natural frequencies and mode shapes of modified model RV14 which was used in the analysis to evaluate the effects of the replacement steam generators. A comparison of response frequencies for corresponding mode shapes identified no significant differences from those in Table 4.A-1 (see also Section 4.A.5, Effects of Replacement Steam Generators).
4.A.2.3.3 Mass Point Response Analysis The original plant design time history mass point responses to seismic excitation were computed using TMCALC, a C-E code. This code performs a numerical integration of the equations of motion for singly or multiply supported dynamic systems utilizing normal mode theory, Reference 4.A-2, and Newmarks Beta-Method with Beta equal to one-sixth, Reference 4.A-4.
For the multiply supported system, the separate time histories of each support were imposed on the system simultaneously. The results are time history responses of the mass points. The analysis of the reactor coolant system utilized modal data for all frequencies through 40 cps.
The mass point responses resulting from the spectrum analysis were found utilizing SHAKE, a C-E computer code. This code performs a normal mode response spectrum analysis resulting in the modal inertials loads found using the response spectrum for the pressurizer support. The mass point responses of the surge line were found using an envelope of the support spectra of the interconnected major components.
4.A-5 Rev. 35
MPS2 UFSAR The transient analysis capability of the ANSYS computer code, Reference 4.A-5, was used to compute the responses of the coupled components of the reactor coolant system with existing replacement steam generators and with the reactor thermal shield removed.
4.A.2.3.4 Seismic Reaction Analysis The original plant design dynamically induced loads at all system design points due to the time history support excitations and mass point responses were calculated utilizing FORCE, a C-E computer code. This code performs a complete loads analysis of the deformed structure at each incremental time step by computing internal and external system reactions (forces and moments) by superposition of the reactions due to the mass point displacements and the non-datum support displacements as follows:
R(t) = CmXm(t)+CsXs(t) where:
R(t) = the matrix of all components of the reactions at the system design points.
Cm = the matrix of mass points displacement influence coefficients.
Xm(t) = the column matrix of time history mass point displacements relative to the datum at each time step.
Cs = the matrix of support displacement influence coefficients.
Xs(t) = the column matrix of time history support displacements relative to the datum at non-datum supports at each time step.
The support and mass point displacements due to horizontal and vertical seismic excitations are added algebraically at each time step. The maximum component of each reaction for the entire time domain, and its associated time of occurrence, are selected.
The maximum reactions for the pressurizer and surge line resulting from the response spectrum analysis were found by applying the modal inertial loads for each mode, to the structural model using the STRUDL computer code. The design point reactions due to each modal loading were conservatively combined by summing the absolute values of the modal reactions. For the replacement pressurizer, the design point reactions due to each modal loading were combined using square root sum of the squares. The surge line analysis included consideration of the relative end displacements. The reactions found by statically imposing the maximum relative displacements of the two ends of the surge line were conservatively included by absolute summation with the inertial response from the spectrum analysis.
The system design loads for the coupled components of the reactor coolant system with existing replacement steam generators and with the reactor internals thermal shield removed were calculated using the ANSYS computer code.
4.A-6 Rev. 35
MPS2 UFSAR 4.A.3 RESULTS The reactions (forces and moments) at all design points in the system, obtained from the dynamic seismic analysis, were compared with the seismic loads in each component design specification.
The results of this comparison are summarized in Table 4.A-2 for the points of maximum calculated load.
The maximum seismic loads calculated by the time history techniques are the result of a search and comparison over the entire time domain of each individual component of load due to the simultaneous application of the horizontal and either vertical excitation. The maximum calculated components of load shown in Table 4.A-2 for each design location do not in general occur at the same time, nor for the same combination of horizontal and vertical excitation, and therefore result in a conservative case.
Except for the replacement pressurizer, the maximum seismic loads calculated by the response spectrum techniques are the result of combining the modal reactions due to the horizontal and the vertical excitation on an absolute sum basis.
The results shown are for the Operational Basis Earthquake. For conservative determination of results due to the Design Basis Earthquake, both the calculated results and specification values have been multiplied by a factor of 2.0, rather than 0.17/0.09 = 1.89, the ratio of DBE to OBE maximum ground accelerations.
4.A.4 EFFECTS OF THERMAL SHIELD REMOVAL An engineering evaluation was made to assess the effects of the thermal shield removal on the dynamic response characteristics of the reactor vessel and the reactor coolant system. The main effect of the thermal shield removal was a reduction in the weight of the reactor vessel. This reduction was approximately two percent (2%). Since the stiffness of the connection between the reactor vessel and internals did not change, it was concluded that the dynamic response characteristics of the reactor vessel and, therefore, the reactor coolant system would not change significantly with the removal of the thermal shield. Reactor vessel flange motions, originally used for a more detailed evaluation of the internal structures in Appendix 3.A, also remain unchanged.
4.A.5 EFFECTS OF REPLACEMENT STEAM GENERATORS The most significant effects of the replacement steam generators were increases in weights and center of gravity elevations of approximately 2.7% and 13.2 inches, respectively, for these components. Modified model RV14, which includes these changes in addition to those due to removal of the reactor internals thermal shield, was used in a reanalysis of the dynamically coupled components of the RCS. The changes in steam generator properties resulted in a reduction of approximately 4.5% in the fundamental frequencies in which the steam generator response is predominant. Corresponding changes in loads which are attributed to the replacement steam generators are generally insignificant with no design governing load increases of more than 4.A-7 Rev. 35
MPS2 UFSAR 7%. The loads from this reanalysis, incorporating the effects of both thermal shield removal and steam generator replacement, are included in Table 4.A-2.
Reactor vessel flange motions were compared with those originally used in the detailed evaluation of the internal structures in Appendix 3.A. This comparison concluded that use of the original flange motions is conservative for reactor internals design.
4.A.6 CONCLUSION It is concluded that the seismic loadings specified for the design of the reactor coolant system components and supports are adequate. All seismic loads calculated by the dynamic seismic analysis are less than the corresponding loads in the component design specification.
4.A.7 REFERENCES 4.A-1 Przemieniecki, J. S., Theory of Matrix Structural Analysis, Chapter 13, McGraw-Hill Book Company, New York, New York, 1968.
4.A-2 Hurty, W. C., and Rubinstein, M. F., Dynamics of Structures, Chapter 8, Prentice Hall, Inc., Englewood Cliffs, New Jersey, 1964.
4.A-3 ICES STRUDL II Engineering Users Manual, R68-91, Department of Civil Engineering, Massachusetts Institute of Technology, Cambridge, Massachusetts.
4.A-4 Newmark, N. M., A Method of Computation for Structural Dynamics, Volume 3, Journal of Engineering Mechanics Division, A.S.C.E., July, 1959.
4.A-5 DeSalvo, G. P., and Swanson, J. A., ANSYS - Engineering Analysis System, Swanson Analysis Systems, Inc., Elizabeth, PA., 1972.
4.A-8 Rev. 35
MPS2 UFSAR TABLE 4.A-1 NATURAL FREQUENCIES AND DOMINANT DEGREES OF FREEDOM Mode Frequency Dominant Degrees of Freedom Number (cps) Names Directions Locations 1 3.07 M66 Z Pump 1B 2 3.08 M43 Z Pump 2B 3 3.21 M61 Z Pump 1A 4 3.23 M52 Z Pump 2A 5 3.32 RI1 Z Reactor Internals 6 3.32 RI1 X Reactor Internals 7 5.11 M61 X,Y Pump 1A 8 5.14 M52 X,Y Pump 2A 9 5.21 M66 X,Y Pump 1B 10 5.23 M43 X,Y Pump 2B 11 10.51 SG5A, SG5B X Steam Generators 1 & 2 12 10.52 SG5A, SG5B X Steam Generators 1 & 2 13 10.60 M61 X Pump 1A 14 10.74 M52 X Pump 2A 15 10.98 M66 X Pump 1B 16 11.11 M43 X Pump 2B 17 12.14 RI2 Z Reactor Internals 18 12.16 RI2 X Reactor Internals 19 20.40 SG9A Z Steam Generator 1 20 20.42 SG9B Z Steam Generator 2 21 23.65 RI1 Y Reactor Internals 22 27.26 SG9, 10, A & B X Steam Generators 1 & 2 23 27.79 SG5A, SG5B Y Steam Generators 1 & 2 24 27.82 SG5A, SG5B Y Steam Generators 1 & 2 25 28.99 M65, M42 Z Pumps 1B & 2B 26 29.91 M65, M42 Z Pumps 1B & 2B 27 30.37 M42 Z Pump 2B 28 31.43 M60 Z Pump 1A 29 31.92 M51 Z Pump 2A 4.A-9 Rev. 35
MPS2 UFSAR TABLE 4.A-1 NATURAL FREQUENCIES AND DOMINANT DEGREES OF FREEDOM Mode Frequency Dominant Degrees of Freedom Number (cps) Names Directions Locations 30 37.51 V1, V3, V4 X, Z Reactor Vessel 31 39.34 SG5B Z Steam Generator 2 32 39.41 SG5A Z Steam Generator 1 1 13.78 - X, Z Replacement Pressurizer 2 44.65 - X, Z Replacement Pressurizer 3 48.99 - X Replacement Pressurizer 4 62.35 - X, Z Replacement Pressurizer 5 75.86 - X, Z Replacement Pressurizer 6 75.97 - Y Replacement Pressurizer 7 99.45 - X, Z Replacement Pressurizer 1 5.75 7, 8, H3 Y Surge Line 2 11.29 5, 7, H1 X Surge Line 3 15.98 5, H1 Y Surge Line 4 21.79 8, 9, H3 Z Surge Line 5 25.81 9, H3 Y Surge Line 6 32.12 8, 9 X Surge Line 7 40.35 10 X Surge Line 8 73.64 5 Z Surge Line 9 108.52 3 X Surge Line 10 129.12 10 Y Surge Line 11 151.51 7, H3 X Surge Line 12 155.03 7 Y Surge Line 13 174.76 7, H1 Y Surge Line 14 186.39 H1 X Surge Line 15 229.90 10, 11 Z Surge Line 16 260.38 11 X Surge Line 17 304.86 3 Y Surge Line 18 320.52 7 X Surge Line 19 503.60 H1 X Surge Line 20 525.21 8 Y Surge Line 21 535.87 8 X Surge Line 22 542.64 11 Z Surge Line 4.A-10 Rev. 35
MPS2 UFSAR TABLE 4.A-1 NATURAL FREQUENCIES AND DOMINANT DEGREES OF FREEDOM Mode Frequency Dominant Degrees of Freedom Number (cps) Names Directions Locations 23 668.06 4 X Surge Line 24 752.11 4 Z Surge Line 25 938.66 11 Y Surge Line 26 1327.41 8 Z Surge Line 27 1807.56 4 Y Surge Line 4.A-11 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Reactor Vessel Outlet Nozzle Fx 107.0 69.0 Fy 3.0 172.0 Fz 65.0 63.0 Mx 1237.0 2168.0 My 7329.0 7521.0 Mz 382.0 38474.0 MR 7443.0 39263.0 Reactor Vessel Inlet Nozzle Fx 97.0 75.0 Fy 98.0 105.0 MPS2 UFSAR Fz 107.0 108.0 Mx 7719.0 22392.0 My 5402.0 10085.0 Mz 16910.0 14087.0 MR 19358.0 28312.0 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-12 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined East-West and Vertical Reactor Vessel Outlet Nozzle Fx 196.0 241.0 Fy 39.0 253.0 Fz 4.0 10.0 Mx 67.0 1042.0 My 360.0 972.0 Mz 3277.0 43773.0 MR 3298.0 43796.0 Reactor Vessel Inlet Nozzle Fx 81.0 220.0 Fy 97.0 146.0 MPS2 UFSAR Fz 110.0 63.0 Mx 5963.0 9638.0 My 3803.0 5981.0 Mz 11763.0 12770.0 MR 13726.0 17080.0 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-13 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Steam Generator Inlet Nozzle Fs 88.5 144.0 Fa 89.0 230.0 Mb 3901.7 4000.0 Mt 2584.0 2640.0 Steam Generator Outlet Nozzles Fs 134.8 202.0 Fa 54.0 104.0 Mb 8990.0 13200.0 Mt 10517.0 14800.0 Combined East-West and Vertical Steam Generator Inlet Nozzle Fs 97.1 144.0 MPS2 UFSAR Fa 175.0 230.0 Mb 4239.0 4000.0 Mt 113.0 2640.0 Steam Generator Outlet Nozzle Fs 126.1 202.0 Fa 49.0 104.0 Mb 7681.0 13200.0 Mt 11224.0 14800.0 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-14 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Pressurizer Surge Line Nozzle Fx 1.74 2.26 Fy 0.91 4.85 Fz 2.71 8.75 MR 192.7 690.9 Combined East-West and Vertical Pressurizer Surge Line Nozzle Fx 1.07 5.70 Fy 0.59 4.77 Fz 1.22 2.71 MR 121.5 617.1 Forces = Kips; Moments = Inch - Kips MPS2 UFSAR MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-15 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Reactor Coolant Pump Nozzle Fx 108.0 83.6 Fy 61.0 93.2 Fz 53.0 114.1 Mx 6289.0 12030.0 My 5632.0 10188.0 Mz 11867.0 10095.0 MR 14564.0 18719.0 Reactor Coolant Pump Outlet Nozzle Fx 137.0 93.2 Fy 98.0 71.3 MPS2 UFSAR Fz 43.0 97.8 Mx 10457.0 22770.3 My 2244.0 7514.4 Mz 2244.0 8957.0 MR 7797.0 25596.0 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-16 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined East-West and Vertical Reactor Coolant Pump Inlet Nozzle Fx 119.0 143.6 Fy 50.0 104.5 Fz 35.0 33.9 Mx 5291.0 8709.0 My 4479.0 5238.0 Mz 12263.0 16662.5 MR 14087.0 19517.0 Reactor Coolant Pump Outlet Nozzle Fx 134.0 263.8 Fy 97.0 145.8 MPS2 UFSAR Fz 37.0 109.9 Mx 5099.0 4072.0 My 2964.0 13317.0 Mz 6269.0 16648.0 MR 8608.0 21796.0 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-17 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Reactor Vessel Outlet Piping MR 7443.0 11514.0 Steam Generator Inlet Piping MR 4680.0 4361.0 *
- Note: Piping design is controlled by combined East-West and vertical seismic excitation.
Steam Generator Outlet Piping MR 13836.0 13836.0 Pump Inlet Piping MR 13148.0 13836.0 Pump Outlet Piping MR 13236.0 18528.0 Reactor Vessel Inlet Piping MR 18522.0 18528.0 Combined East-West and Vertical Reactor Vessel Outlet Piping MR 3298.0 11581.0 Steam Generator Inlet Piping 4241.0 9658.0 MPS2 UFSAR MR Steam Generator Outlet Piping MR 13601.0 13836.0 Pump Inlet Piping MR 13632.0 13836.0 Pump Outlet Piping MR 8608.0 18528.0 Reactor Vessel Inlet Piping MR 13726.0 18528.0 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-18 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Surge Line RCS Nozzle Fx 4.41 6.0 Fy 1.45 4.0 Fz 3.25 4.0 MR 277.6 468.0 Combined East-West and Vertical Surge Line RCS Nozzle Fx 2.55 6.0 Fy 0.84 4.0 Fz 1.31 4.0 MR 155.5 468.0 Combined North-South and Vertical Surge Line Hanger H4 Fx 0.150 0.18 MPS2 UFSAR Fy 0.439 2.0 Surge Line Hanger H2 Fy 0.209 1.0 Fz 0.078 0.11 Combined East-West and Vertical Surge Line Hanger H4 Fx 0.083 0.18 Fy 0.335 2.0 Surge Line Hanger H2 Fy 0.145 1.0 Fz 0.016 0.11 Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-19 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined North-South and Vertical Reactor Vessel Outlet Support Fy 165.0 392.0 Fz 325.0 663.0 Reactor Vessel Inlet Support Fy 314.0 692.0 FH 191.0 304.0 Steam Generator Lower Support Fy 219.0 431.0 Fz 195.0 397.0 Mx 20345.0 24422.0 My 2335.0 10332.0 Steam Generator Upper Support Fx 20.0 24.0 MPS2 UFSAR Fz 219.0 240.0 Pump Support Fy 2.6 9.2 Replacement Pressurizer Support Fy 14.1 80.0 a Fz 80.1 84.0
- Mx 15107.6 22768.9 17036.0
- Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2 4.A-20 Rev. 35
MPS2 UFSAR TABLE 4.A-2 SEISMIC LOADS ON REACTOR COOLANT SYSTEM COMPONENTS FOR OPERATIONAL BASIS EARTHQUAKE (CONTINUED)
SEISMIC LOAD COMPONENT AND DESIGN COMPONEN CALCULATE DESIGN SEISMIC EXCITATION LOCATION T D MAXIMUM BASIS Combined East-West and Vertical Reactor Outlet Support Fy 309.0 473.0 Fz 47.0 42.0 Reactor Vessel Inlet Support Fy 227.0 469.0 FH 375.0 1020.0 Steam Generator Lower Support Fy 278.0 624.0 Fz 32.0 29.0 My 356.0 455.0 Mz 8792.0 24383.0 Steam Generator Upper Support Fx 281.0 296.0 MPS2 UFSAR Fz 12.0 10.0 Reactor Coolant Pump Support Fy 1.6 4.3 Replacement Pressurizer Support Fx 55.6 81.0
- Fy 14.1 80.0
- Mz 15746.9 16949.0
- Forces = Kips; Moments = Inch - Kips MR = [Mx2 + My2 + Mz2]1/2 FH = [Fx2 + Fz2]1/2
- a. Note that the design basis values are based on original pressurizer design and are retained here for historical purposes only.
4.A-21 Rev. 35
MPS-2 FSAR FIGURE 4A-1 REACTOR COOLANT SYSTEM SEISMIC ANALYSIS MODEL MS2 KEY Note: Representation of reactor internals not shown.
+y STEAM GENERATOR #1 KEY NODE 152 STEAM GENERATOR #2 SNUBBER NODE 143 PUMP2A NODE 135
/
+z
{NORTH)
+X
@ MASS POINT {WEST)
Rev. 24.2 JULY 1988
MPS-2 FSAR FIGURE 4A-1A REACTOR COOLANT SYSTEM - SEISMIC ANALYSIS MODEL MS2 AND RV14 NODE 118 ---""'~
PUMP "f COLD LEG 2 COLD LEG 1
~
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COLD LEG 2 NODE 105 GOBAL
+Fx (WEST)
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MAY 1994 Rev. 24.2
MPS-2 FSAR FIGURE4A-2 RV14 REACTOR AND INTERNALS SEISMIC ANALYSIS MODEL DEGREE OF 0 MASS POINT FREEDOM
- MASS POINT RJ3 , 15, 18 X, Y, Z o STRUCTURAL JOINT 1, RJ3 , RJ4 , RJ5 }- SUPPORT POINT 1, 4, 9, 10 X, Z E- MEMBER RELEASES 16, 17, 19, 20 y
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UPPER GUIDE STRUCTURE CORE SUPPORT BARREL
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J I
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9 / /
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/ / bas is ma the ma tica l mo del .
17 /
- - ,:-:;;!J RJl I 16 /
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RJ5 JULY 1998 Rev. 24.2
MPS-2 FSAR FIGURE 4A-3 PRESSURIZER SEISMIC ANALYSIS MODEL 5
- MASS POINT o STRU CTUR AL JOINT 3- SUPP ORT POINT E- MEMB ER RELE ASES 4
y x*
3 2
Mass Point Degree of Freedom 1 1 thru 4 x 5 X, Y
\
JULY 10 1982 Rev. 24.2
MPS-2 FSAR FIGURE 4A-4 SURGE LINE SEISMIC ANALYSIS MODEL
- MASS POINT y o STRUCTURAL JOINT t- SUPPORT POINT E- MEMBER RELEASES z x PRESSURIZER Mass Point Degree of Freedom 3, 7 X,Y H3 Z,Y 4, H1, 5, 8, 9,10,11 X,Y,Z Support Name i Support Restraint Directions H1 Fx H2 Fy, Fz H3 Fz H4 Fx, Fy H5 I Fx, Fy, Fz JUN 10 1982 Rev. 24.2