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{{#Wiki_filter:8608060052 860730 PDR ADOCK 05000315 P PDR L\i'~~,1 TECHNICAL REPORT TR-5364-1 REVISION 0 BOOK 1 OF 15 DONALD C.COOK NUCLEAR GENERATING PLANT ANALYSIS OP PRESSURIZER SAPBTY/RELKF VALVES DISCHARGE PIPING SYSTEM PER NUREG 073V, ILD.I, UNTF I JUNE 6, 1983 l'i'i F AMERICAN ELECTRIC POWER SERVICE CORPORATION 2 BROAOWAY NEW YORK, NEW YORK 10004 TECHNICAL REPORT TR-5364-1 REVISION 0 BOOK 1 OF 15 DONALD C.COOK NUCI.EAR GENERATING STATION ANALYSIS OF PRESSURIZER SAFETY/RELIEF VALVES DISCHARGE PIPING SYSTEM PER NUREG 0737, II~0.1, UNIT 1 JUNE 6, 1983 N'TELEDYNE ENGINEERING SERVICES 130 SECOND AVENUE WALTHAM, MASSACHUSETTS 02254 61 7-890-3350 4('I~~'I, 1(%h IC t t ,C\r,~~f II 0 I 1 C: 'I j 1 A~r Technical Report TR-5364-1 Revision 0 TABLE OF CONTENTS A TELEDYNE ENGINEERINQ SERVICES PAGE
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                        ~,1 TECHNICAL REPORT TR-5364-1 REVISION   0 BOOK   1 OF 15 DONALD C. COOK NUCLEAR GENERATING PLANT ANALYSIS OP PRESSURIZER SAPBTY/RELKF VALVES DISCHARGE PIPING SYSTEM PER NUREG 073V, ILD.I, UNTF I JUNE 6, 1983


==1.0 INTRODUCTION==
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==2.0 CONCLUSION==
AMERICAN ELECTRIC POWER SERVICE CORPORATION 2 BROAOWAY NEW YORK, NEW YORK    10004 TECHNICAL REPORT TR-5364-1 REVISION 0 BOOK 1 OF 15 DONALD C. COOK NUCI.EAR GENERATING STATION ANALYSIS OF PRESSURIZER SAFETY/RELIEF VALVES DISCHARGE PIPING SYSTEM PER NUREG 0737,  II ~ 0.1, UNIT    1 JUNE  6, 1983 N'TELEDYNE ENGINEERING SERVICES 130 SECOND AVENUE WALTHAM,MASSACHUSETTS 02254 61 7-890-3350
S 3.0 SYSTEM DESCRIPTION/DISCUSSION 4.0 THERMAL FLUIDS ANALYSIS 4.1 Introduction 4.2 RELAP Model 4.2.1 Pressurizer Conditions 4.2.2 Valve Modeling 4.2.3 Discharge Piping 4.2.4 quench Tank 4.3 RELAP Model Control Volumes 4.4 quarter Model 4.5 Unit 1 PORV Model 4.5.1 Condensate Modeled Case 4.5.2 ,PORV Modeled Transient 4.6 Valve Flow Rate Calculation 4.6.1 SV Flow Rate 4.6.2 PORV Flow Rate 4.7 RELAP Plots Book 1 of 15 2-1 3-1 4-1 4-1 4 3 4-3 4-4 4-5 4-5 4-16 4-26 4-'36 4-36 4-36 4-40 4-41 4-.42 4-45 4.7.1 Unit 1-Condensate/Steam Case 4.7.2 Unit 1-400o Solid Liquid Case 4.7.3 quarter Model-Cold Loop Seal/Steam Case 4 46 4-166 4-244 4.8 Force Time History Plots Book 2 of 15 4-260 4.8.1 Unit 1-Condensate/Steam Case 4.8.2 Unit 1-400o Solid Liquid Case 4.8.3 quarter Model-Cold Loop Seal/Steam Case 4.9 RELAP Input 4-261 4-320 4-392 4-420 4.9.1 4.9.2 4.9.3 4.9.4 4.9.5 PORV Condensate/Steam Condensate/Steam Restart PORV Solid 400o Liquid PORV Solid 400o Liquid Restart SV Cold Loop Seal (quarter Model)4-421 4-439 4-448 4-467 4-472 ga'\pl 4 Af t/C~ia<a jh~ra-p E W I'*r" 0 P~(t is/.A''g,J Techni ca 1 Report TR-5364-1 Revision 0 4.10 REP IPE Input TABLE OF CONTENTS Continued)i TELEDYNE ENQINEERINQ SERVICES PAGE 4-478 4.10.1 Unit 1-Model Section A 4.10.2 Unit 1-Model Section B 4.10.3 Unit 2-(quarter Model)4.11 APPENDIX A 5.0 STRUCTURAL ANALYSIS 5.1 Deadweight Analysis 5.2 Thermal Analysis 5.3 Seismic Analysis 5.4 Force/Time History Analysis 5.4.1 PORV Transient 5.4.2 SV Transient 6.0 ANALYTICAL RESULTS 6.1 Stress Su@nary Book 3 of 15 4-479'-489 4-496 5-1 5-2 5-2 5-2 5-7 5-7 5-8 6-1 6-1 6.1.1 6.1.2 6.1.3 6.1.4 6.1.5 6.1.6 Equation A-1 Stresses Equation A-2 Stresses Equation B-1 Stresses Equation B-2 Stresses Equation B-3 Stresses Equation C-1 Stresses 6-6 6-17 6-28 6-39 6-50 6-61 6.2 Support Loads 6.3 Valve Accelerations 6.3.1 DBE Seismic Valve Accelerations 6.3.2 PORV Transient Shock Valve Accelerations 6.4 Nozzle Loads 6.5 Valve Loads 6.6 Miscellaneous Calculations 6.6.1 Thermal Boundary Displ acements 6.6.2 OBE Spectra 6.6.3 DBE Spectra 7.0 DRAWINGS


==8.0 REFERENCES==
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6-72 6-105 6-106 6-110 6-114 6-120 6-126 6-127 6-133 6-140 7-1 8-1 ifqf IN C 4'L Technical Report TR-5364-1 Revision 0 A TELEDYNE ENGlNEERINQ SERV(CES TABLE OF CONTENTS Continued 9.0 COMPUTER ANALYSIS 9.1 9.2 9.3 9.4 9.5 9.6 9.7 RELAP/REP IPE Input Deadweight/Thermal Input/Output OBE Seismic X-Y Input/Output OBE Seismic Y-Z Input/Output DBE Seismic X-Y Input/Output DBE Seismic Y-Z Input/Output PORV Transient Shock Input Book 4 of 15 Book 5 of 15 Books 6, 7 of 15 Books 8, 9 of 15 Books 10, 11 of 15 Books 12, 13 of 15 Books 14, 15 of 15
A TELEDYNE Technical Report                                         ENGINEERINQ SERVICES TR-5364-1 Revision   0 TABLE OF CONTENTS PAGE
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Technical Report TR-5364-1 Revision 0-A-TELEDYNE ENQlNEERING SERVfCES 1.0.INTRODUCTION American Electric Power Service Corporation
{AEP), purchase order number 02676-820-1N, authorized Teledyne Engineering Services (TES)to analyze the Pressurizer Safety/Relief Valve Discharge Piping per NRC NUREG-0737, Item II.D.1, for the Donald C.Cook Nuclear Power Plant, Unit Pl.This activity was performed in accordance with the TES (}uality Assurance program which meets the requirements of 10CFR50, Appendix B, and ANSI N45.2.11 as interpreted by Regulatory Guide 1.64, Revision 2.The scope of work for this effort is described in detail in Teledyne Engineering Services Technical Proposal PR-5653{Reference 1), dated May 4, 1981 and modified as stated in AEP letter dated November 29, 1982, from Mr.Sam Ulan (AEP)to,Mr.L.B.Semprucci (TES)and in AEP letter from Mr.Sam Ulan (AEP)to Mr.P.D.Harrison (TES)dated March 15, 1983 (References 2 and 3).The majority of the analysis was performed after the receipt of AEP letters dated November 29, 1982 and March 15, 1983 (References 2 and 3), which were issued after more complete information was available from, the EPRI data.This analysis was performed using l ar ge di g ital computer programs supplemented with any necessary hand calculations.
The RELAP5 MOD1 Cycle 14 computer program was used to do the thermal fluid transient analysis.The structural analysis, for all loading conditions, was done utilizing the TMRSAP computer program.'he size of the pressuri zer safety/relief valve discharge piping system was so large that the computer models, for both RELAP and TMRSAP, strained the limits of the programs.This condition necessitated multiple RELAP runs in order to execute the thermal fluid transient analysis for the appropriate length of time.For the structural analysis it was necessary to expand the core of the TMRSAP pr ogram in order to avoid an overconservative overlap analysis.
II I'g I t j"I ,ri t)Q'4~~a'El, Techni cal Report TR-5364-1 Revision 0 2-1 r>TELEDYNE ENGINEERINQ SERVICES


==2.0 CONCLUSION==
==1.0    INTRODUCTION==
S The analysi s performed by TES on the Pres suri zer Saf ety/Rel i ef Val ve Discharge Piping System indicates that all criteria of NRC NUREG-0737, Item II.D.1 is met for normal and upset (PORV discharge) conditions and is not met for the emergency (SV discharge) condition.
Book 1 of 15
 
==2.0    CONCLUSION==
S                                                      2-1 3.0    SYSTEM DESCRIPTION/DISCUSSION                                    3-1 4.0    THERMAL FLUIDS ANALYSIS                                          4-1 4.1  Introduction                                                4-1 4.2  RELAP Model                                                4 3 4.2.1  Pressurizer Conditions                              4-3 4.2.2  Valve Modeling                                      4-4 4.2.3  Discharge Piping                                    4-5 4.2.4  quench Tank                                        4-5 4.3  RELAP Model  Control Volumes                              4-16 4.4  quarter Model                                              4-26 4.5  Unit 1 PORV Model                                          4-'36 4.5. 1  Condensate Modeled Case                            4-36 4.5.2  ,PORV Modeled Transient                              4-36 4.6  Valve Flow Rate Calculation                                4-40 4.6.1  SV Flow Rate                                        4-41 4.6.2  PORV Flow Rate                                      4-.42 4.7  RELAP  Plots                                                4-45 4.7.1  Unit 1 - Condensate/Steam Case                      4 46 4.7.2  Unit 1 - 400o Solid Liquid Case                    4-166 4.7.3  quarter Model - Cold Loop Seal/Steam  Case          4-244 4.8  Force Time History Plots                      Book 2 of 15 4-260 4.8.1  Unit 1 - Condensate/Steam Case                      4-261 4.8.2  Unit 1 - 400o Solid Liquid Case                    4-320 4.8.3  quarter Model - Cold Loop Seal/Steam  Case          4-392 4.9  RELAP  Input                                                4-420 4.9.1    PORV Condensate/Steam                              4-421 4.9.2  Condensate/Steam Restart                            4-439 4.9.3    PORV Solid 400o  Liquid                          4-448 4.9.4    PORV Solid 400o  Liquid Restart                  4-467 4.9.5    SV Cold Loop Seal  (quarter Model)                4-472
 
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                                                        )i TELEDYNE Techni ca 1 Report                                        ENQINEERINQ SERVICES TR-5364-1 Revision  0 TABLE OF CONTENTS Continued PAGE 4.10    REP IPE Input                                                4-478 4.10.1  Unit  1 - Model Section A                          4-479 4.10.2  Unit  1 - Model Section B                        '-489 4.10.3  Unit  2 - (quarter Model)                          4-496 4.11    APPENDIX A 5.0    STRUCTURAL ANALYSIS                                  Book 3 of 15  5-1 5.1    Deadweight Analysis                                          5-2 5.2    Thermal Analysis                                            5-2 5.3    Seismic Analysis                                            5-2 5.4    Force/Time History Analysis                                  5-7 5.4.1    PORV  Transient                                    5-7 5.4.2    SV Transient                                        5-8 6.0    ANALYTICAL RESULTS                                                  6-1 6.1    Stress Su@nary                                              6-1 6.1.1    Equation  A-1  Stresses                            6-6 6.1.2    Equation  A-2  Stresses                            6-17 6.1.3    Equation  B-1  Stresses                            6-28 6.1.4    Equation  B-2 Stresses                              6-39 6.1.5    Equation  B-3  Stresses                            6-50 6.1.6    Equation  C-1 Stresses                              6-61 6.2    Support Loads                                                6-72 6.3    Valve Accelerations                                          6-105 6.3.1    DBE Seismic Valve Accelerations                    6-106 6.3.2    PORV Transient Shock Valve Accelerations            6-110 6.4    Nozzle Loads                                                6-114 6.5    Valve Loads                                                  6-120 6.6    Miscellaneous Calculations                                  6-126 6.6.1    Thermal Boundary Displ acements                    6-127 6.6.2    OBE  Spectra                                        6-133 6.6.3    DBE  Spectra                                        6-140 7.0    DRAWINGS                                                            7-1
 
==8.0    REFERENCES==
8-1
 
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A TELEDYNE Technical Report                                      ENGlNEERINQ SERV(CES TR-5364-1 Revision  0 TABLE OF CONTENTS Continued 9.0    COMPUTER ANALYSIS 9.1    RELAP/REP IPE Input                        Book 4 of 15 9.2    Deadweight/Thermal Input/Output            Book 5 of 15 9.3    OBE Seismic X-Y Input/Output              Books 6, 7 of 15 9.4    OBE Seismic Y-Z Input/Output              Books 8, 9 of 15 9.5    DBE Seismic X-Y Input/Output              Books 10, 11 of 15 9.6    DBE Seismic Y-Z Input/Output              Books 12, 13 of 15 9.7    PORV Transient Shock Input                Books 14, 15 of 15
 
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                                                          -A-TELEDYNE Technical Report TR-5364-1                                                      ENQlNEERING SERVfCES Revision    0 1.0    . INTRODUCTION American    Electric  Power  Service Corporation {AEP), purchase order number 02676-820-1N, authorized Teledyne Engineering Services (TES) to analyze the Pressurizer Safety/Relief Valve Discharge Piping per NRC NUREG-0737, Item II. D.1, for the Donald C. Cook Nuclear Power Plant, Unit Pl.
This  activity  was performed in accordance  with the  TES (}uality Assurance program which meets the requirements of 10CFR50, Appendix B, and ANSI N45.2.11 as interpreted by Regulatory Guide 1.64, Revision 2.
The  scope  of work for this effort is described        in detail in Teledyne Engineering Services Technical Proposal PR-5653 {Reference 1), dated May 4, 1981 and modified as stated in AEP letter dated November 29, 1982, from Mr. Sam Ulan (AEP) to,Mr. L. B. Semprucci (TES) and in AEP letter from Mr. Sam Ulan (AEP) to Mr.
P. D. Harrison (TES) dated March 15, 1983 (References 2 and 3).
The  majority of the analysis    was performed after the receipt of AEP letters dated November 29, 1982 and March 15, 1983 (References 2 and 3), which were issued after more complete information was available from,the EPRI data.
This    analysis was performed using l ar ge di g ital computer programs supplemented with any necessary hand calculations.            The RELAP5 MOD1 Cycle 14 computer program was used to do the thermal fluid transient analysis. The structural analysis, for all loading conditions, was done utilizing the TMRSAP computer program.
                      'he size of the pressuri zer safety/relief valve discharge piping system was so large that the computer models, for both RELAP and TMRSAP, strained the limits of the programs. This condition necessitated multiple RELAP runs in order to execute the thermal fluid transient analysis for the appropriate length of time.
For the structural analysis it was necessary to expand the core of the TMRSAP pr ogram in order to avoid an overconservative overlap analysis.
 
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r> TELEDYNE Techni cal Report                                        ENGINEERINQ SERVICES TR-5364-1 Revision  0                              2-1
 
==2.0   CONCLUSION==
S The   analysi s performed by TES on the Pres suri zer Saf ety/Rel i ef Val ve Discharge Piping System indicates that all criteria of NRC NUREG-0737, Item II.D.1 is met for normal and upset (PORV discharge) conditions and is not met for the emergency (SV discharge) condition.
Evaluation of normal and upset conditions required structural analysis for deadweight, thermal, OBE seismic, and PORV transient shock loading conditions.
Evaluation of normal and upset conditions required structural analysis for deadweight, thermal, OBE seismic, and PORV transient shock loading conditions.
Details of the various loadings considered are provided in Section 5.Based on preliminary SV thermal hydrodynamic transient analysis, excessive loads and stresses were anticipated and, therefore, it was decided;for economic reasons, that a quarter model SV thermal tr ansient analysis (RELAP5)should be performed to check the adequacy of the system for the emergency condition.
Details of the various loadings considered are provided in Section 5.
In addition, due to the similarities of the Unit 1 and Unit 2 geometries, it was determined that the results of one unit could be considered applicable to the other unit.The quarter model consisted of the piping from the pressurizer, through valve SV-45C, and continuing down to the quench tank, for Unit 2.The SV transient analysis considered only the effect of valve SV-45C opening.The results of the quarter model analysis indicated substantial failure of the entire quarter model geometry.Considering that TES is required to analyze for the simultaneous opening of all thr ee SV valves (Reference 3), which is a more severe loading condition, it is evident that the quarter model analysis is sufficient to prove the failure, for the emergency condition, of both Units 1 and 2.Therefore, this report for Unit 1 contains no analysis or results for the SV thermal condition or the SV thermal transient shock condition.
Based on   preliminary SV thermal hydrodynamic transient analysis, excessive loads and stresses were anticipated and, therefore, it was decided; for economic reasons, that a quarter model SV thermal tr ansient analysis (RELAP5) should be performed to check the adequacy of the system for the emergency condition. In addition, due to the similarities of the Unit 1 and Unit 2 geometries, it was determined that the results of one unit could be considered applicable to the other unit. The quarter model consisted of the piping from the pressurizer, through valve SV-45C, and continuing down to the quench tank, for Unit 2. The SV transient analysis considered only the effect of valve SV-45C opening.       The results of the quarter model analysis indicated substantial failure of the entire quarter model geometry.       Considering that TES is required to analyze for the simultaneous opening of all thr ee SV valves (Reference 3), which is a more severe loading condition, it is evident that the quarter model analysis is sufficient to prove the failure, for the emergency condition, of both Units 1 and 2.
Results of the SV quarter model analysis performed for Unit 2 are contained in the Unit 2 report, TES Technical Report TR-5364-2 (Reference 6).
Therefore, this report for Unit 1 contains no analysis or results for the SV thermal condition or the SV thermal transient shock condition. Results of the SV quarter model analysis performed for Unit 2 are contained in the Unit 2 report, TES Technical Report TR-5364-2 (Reference 6).
f q~y'I r s~t.s C t a 0 Technical Report TR-5364-1 Revision 0 2-2 r>TEif23YNE ENGINEERINQ SERVICES.Section 6 contains a stress sumary of all node points, a summary of support loads, valve acceleration calculations, a sumary of pressurizer and quench tank nozzle loads, and a listing of the moments on the end of each valve for all loading conditions.
 
It should be noted that valves NRV-151, NRV-152, NM0-151, NM0-152,'nd NMO-153 are in excess of the veritical acceleration criteria of 2g for the PORV thermal shock transient condition.
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These values are considered acceptable per the approval given by AEP in their letter of May 26, 1983 from Mr.Sam Ulan of AEP to Mr.P.D.Harrison of TES (Reference 7).  
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~FC CC C Y~': f F C 2~f A r!:.~s f~~CCC~,~C Techni cal Report TR-5364-1 Revision 0 3-1-r<-TELEDYNE ENGINEERING SERV(CES 3.0 SYSTEM DESCRIPTION/DISCUSSION The Pressurizer Safety/Relief Valve Discharge Piping consists of all of the piping from the pressurizer nozzles, down to the sparger in the quench tank.This information is depicted on TES drawing E-5763, Revision 2, generated from AEP drawings 1-GRC-6, sheets 1,', 3, 4;1-GRC-7;1-GRC-8;and 1-GRC-9.The"Discharge" piping constitutes a very large system resulting in a large computer model.The size and geometrical complexity, which is due mainly to the sweeping curves around the pressurizer, complicates the modification effort in addition to causing longer run times..Modification of this complex system, to attempt to secu're satisfactory"Safety Valve Discharge" results, is limited to draining the SV loop seals.Heating the loop seals is not a viable"fix" because of the size of the loops.These long loops contain sufficient quantity of water such that on SV Discharge, the water seal does not"flash" completely enough to reduce the very high loads caused by the water slug.Modification to the support system is also a poor option because of the very limited space in the annulus around the pressurizer, which makes construction very difficult.
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Another aspect of the system that could be improved is the setting of the constant spring supports.During the data extraction of the deadweight analysis results, it was observed that the supports in the PORV loop area were causing significant upward displacements of the piping system, as detailed'in Section'.2.
 
r> TEif23YNE Technical Report                                         ENGINEERINQ SERVICES          .
TR-5364-1 Revision 0                             2-2 Section 6 contains a stress sumary of all node points, a summary of support loads, valve acceleration calculations, a sumary of pressurizer and quench tank nozzle loads, and a listing of the moments on the end of each valve for all loading conditions. It should be noted that valves NRV-151, NRV-152, NM0-151, NM0-152, NMO-153 are in excess of the veritical acceleration criteria of 2g for the
                                                                                    'nd PORV thermal shock transient condition. These values are considered acceptable per the approval given by AEP in their letter of May 26, 1983 from Mr. Sam Ulan of AEP to Mr. P. D. Harrison of TES (Reference 7).
 
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                                                      -r<-TELEDYNE Techni cal Report                                         ENGINEERING SERV(CES TR-5364-1 Revision   0                             3-1 3.0   SYSTEM DESCRIPTION/DISCUSSION The   Pressurizer Safety/Relief Valve Discharge Piping consists of all of the piping from the pressurizer nozzles, down to the sparger in the quench tank. This information is depicted on TES drawing E-5763, Revision 2, generated from AEP drawings 1-GRC-6, sheets     1,', 3, 4; 1-GRC-7; 1-GRC-8; and 1-GRC-9.
The   "Discharge" piping constitutes a very large system resulting in a large computer model. The size and geometrical complexity, which is due mainly to the sweeping curves around the pressurizer, complicates the modification effort in addition to causing longer run times..
Modification of this complex system, to attempt to secu're satisfactory "Safety Valve Discharge" results, is limited to draining the SV loop seals.
Heating the loop seals is not a viable "fix" because of the size of the loops.
These long loops contain sufficient quantity of water such that on SV Discharge, the water seal does not "flash" completely enough to reduce the very high loads caused by the water slug.       Modification to the support system is also a poor option because of the very limited space in the annulus around the pressurizer, which makes construction very difficult.
Another aspect of the system that could be improved is the setting of the constant spring supports. During the data extraction of the deadweight analysis results,   it was observed that the supports in the PORV loop area were causing significant upward displacements of the piping system, as detailed'in       Section'.2.
The stresses in these regions are high and, although they do not exceed the allowable, they could be r educed by re-adjustment of the spring settings.
The stresses in these regions are high and, although they do not exceed the allowable, they could be r educed by re-adjustment of the spring settings.
h g'=~~~4 IQ il L'~I f A I Technical Report TR-5364-1 Revision 0 4-1-A TELEDYNE ENGINEERING SERVICES 4.0 THERMAL FLUIDS ANALYSIS 4.1 Introduction The following analysis determines the fluid forces which act on the pressurizer safety and relief valve discharge piping of the American Electric Power Donald C.Cook Nuclear power Plant, Units 1 and 2.These forces are generated by the sudden opening of the pressurizer safety and relief valves during one or more of the pressurizer transients described in the AEP supplied 1982 letter to TES.These forces, the resulting stresses they apply to the piping system, the resulting loads they impose on'the pipe supports, and the loads they transmit to the safety and relief valves became of increased concern as a result of the incident at Three Mile Island.Following the Three Nile Island incident, the NRC issued NUREG 0578 and NUREG 0737 which required that each utility determine the effect of safety/relief valve operation upon the valve and the discharge piping.An elaborate progr am involving both testing and analysis was established under the general management of the Electric Power Research Institute (EPRI).Intensive testing of safety and~elief valves was performed at several locations across the country.A full scale model of the pressurizer and discharge piping was built at Combustion Engineering in Connecticut.'imultaneously, an analytical program was initiated to choose and test a computer program which would predict the fluid forces;RELAP5 MODl was chosen.This is the latest in the family of RELAP programs developed at the Idaho National Fngineer ing Laboratory.
 
In this analysis, TES has used RELAP5 MOD1 Version 2.11 as it is made available through Control Data Corp with a post-processor, REPIPE version 3.10, which calculates the fluid forces.
h g   '=
I~'k~$gl P i I A es~C Technical Report TR-5364-1 Revision 0 4-2-ri-TELEDYNE ENGlNEERlNG SERVlCES This version.of RELAPS NOD1 is identified by the following computer job control language at Control Data Corporation:
    ~ ~
BEGIN, REI AP5, R5N2, INPUT=INPUTFILE, SCM=377000B The computer analysis procedure for the thermal analysis portion is included in Appendix A.RELAP5 calculates hydrodynamic data for control volumes in each segment of pipe.REPIPE then takes this data and defines two force time histories for a segment.One set of inlet junction forces, the other outlet junction forces.SAP2SAP adds these force time histories.
      ~   4 IQ         il L   '
Finally, one force time history for each segment of axial, unbalanced loads is analyzed structurally.
  ~ I f
C+w~l Technical Report TR-5364-1 Revision 0 4-3>s-TELEOYNE ENGlNEERINQ SERVICES 4.2 RELAP Model 4.2.1 The D.C.Cook pressurizer was modeled as a single time dependent volume with the following transient conditions as specified by the American Electric Power 11/29/82 letter to LBS, pages 1-7: Case 1::~Sf'll Steam, Loopseal Case Zyoo Zhs'd Pressure l WD/)g p+g R@~49 pP c~o-e-o-p-p p gpg+Palo Zt'o4p p25rg J/O Time (Sec)  
A I
" ('w ,.:f~q;~.~=hl W 4 y/0 Technical Report TR-5364-1 Revision 0 is TELEDYNE ENQINEERlNQ SERVICES PORV Steam/Condensate Slugs Case 2550 2500 2450 Pressure psi 2400 2350 2300 0.8 Time (Sec)1.2 0.4 Case 2: Continuous Warm Water=400oF (Same pressure as PORV, Case 1)4.2.2 Safety valves and power operated relief valves were modeled as RELAP junctions using the following information:
 
Safety Valve manufacturer Crosby HB-BP-86 (Ref.13)0 if'CJJi Ti 0.022 Ft2 0.010 Sec.PORV Masoneilan NO-38-20721 (Ref.14)0.00806 Ft2 1.0 Sec Valve orifice areas were calculated using the EPRI Safety and Relief Valve Test Report (Reference 16)and RELAP (Run ID BAICDRO)implementing rated flows.Calculated values are included in Section 4.6.1.
                                                                      -A TELEDYNE Technical Report TR-5364-1                                         4-1                     ENGINEERING SERVICES Revision    0 4.0     THERMAL FLUIDS ANALYSIS 4.1   Introduction The   following analysis determines the fluid forces which act on the pressurizer safety and relief valve discharge piping of the American Electric Power Donald C. Cook Nuclear power Plant, Units 1 and 2. These forces are generated by the sudden opening of the pressurizer safety and relief valves during one or more of the pressurizer transients described in the AEP supplied 1982 letter to TES.
is'>'ly I'I 1)I' Technical Report TR-5364-1 Revision 0 4 5]<TELEDYNE ENGINEERING SERVICES 4.2.3 Discharge piping was modeled from all safety and power operated relief valves to the quench tank.This discharge piping included the following pipe sizes: 3 inch, 12 inch 4 inch, 6 inch 4 inch 3 inch, 6 inch SCH 40 SCH 40S SCH 120 SCH 160 Friction factors for 1.5 D or short radius bends and reducers were taken from technical paper 8410 by Crane.Calculations of these losses and constants are included in Appendix A.Segment lengths used are listed in Figures 4.2.1 and 4.2.2 for both models.The discharge piping defines segments with segments described as straight sections from elbow to elbow, valve to elbow, etc.Also, a listing of RELAP5 input is included in this report.The SRV model is modeled from one safety valve to the quench tank.This was determined to be an adequate representation of safety discharge piping for both units and will subsequently be referred to as"The Quarter Model".The Quarter Model is modeled utilizing Unit 2's geometry.'.2.4 The Quench Tank was modeled in two parts: the sparger and the tank itself.The Quench Tank is modeled using cylindrical volumes containing water and air.The volume si zes are equal to quench tank volumes provided on Westinghouse Dwg.No.110E272.The sparger for D.C.Cook is a perforated pipe submerged in the water within the quench tank as indicated in Figure 4.2.3 of this report.It is represented in RELAP as a pipe equal in volume and similarly submerged.
These     forces, the resulting stresses they apply to the piping system, the resulting loads they impose on'the pipe supports, and the loads they transmit to the safety and relief valves became of increased concern as a result of the incident at Three Mile Island.
TR->364-I i<TELEDYNE ENGINEERING SERVICES Revision 0 BY~~~DATE+i~CHKO.BY~+T OATE~~woo ds.4CeC reap s, AMPERE E (~JPI/j z JA./IO VV 4S'C SHEET NO.OF I PROJ.NO, OFT Sca Ibo ruOrC A Zs Sr'.C n i~C-Pf CF/X/4 lk lg JFP Q,o 2I P ger NCJFJ 4.$20 25'C~E rf+O I.0 ih:->Z M 2 JF 9$3y~2 IFi Sb SET W9" FIGURE 4.2.1 A t'I 4  
Following the Three Nile Island incident, the NRC issued NUREG 0578 and NUREG 0737 which required that each utility determine the effect of safety/
"'-""i"'""IIi TELEDYNE ENQINEERINQ SERVICES TR-5364-1 Revision 0 BY OATE~CHKO.BY~+DATE+@~4-7 5M&/~Meet~~~c~o~SHEET NO.~(>F (,q9 2.0b FIGURE 4.2.2-1 e ,visgpn 0 BY~g~OATE+~8Z HKO.BYG~OATE~+(SHCET NO.~OF~J 4 lP/I]y4g 5 Eg MEhl 7 ,...-~S-TELEDYNE ENGINEERING SERVICES TR-5364-1 4-8 4/ACL7'(F I GNiE 4.2.2-2  
relief valve operation upon the valve and the discharge piping. An elaborate progr am involving both testing and analysis was established under the general management of the Electric Power Research Institute (EPRI).                       Intensive testing of safety and ~elief valves was performed at several locations across the country.
"""'"'~TELEDYNE ENGINE=RING SERVICES Revision 0 Y~~+.OATE+~H K O.BY~+~0 AT K,~LL~4-9 Qz w&5M pig~.,+oWV i i<<~)A~a~t=t'YTs4 Q.NwlE4)Ogg/I)0 FIGURE 4.2.2-3 e I I"C~P'I I'1  
A full scale model of the pressurizer and discharge piping was built at Combustion Engineering in Connecticut.'imultaneously, an analytical program was initiated to choose and test a computer program which would predict the fluid forces; RELAP5 MODl was chosen. This is the latest in the family of RELAP programs developed at the Idaho National Fngineer ing Laboratory.
~g~rg.C (wJA/.M>Iles A'AL/Egl Wif IEQ iud.ra>swCO d~'>.c,"o" IS bgkwI PRES.V OPS/6 A5AC.IPIA$
In this analysis, TES has used                 RELAP5 MOD1 Version 2.11 as it is made available through Control Data Corp with                   a post-processor, REPIPE version 3.10, which calculates the fluid forces .
'A~~Q'EI=5 Vh'-5/28 A-24)n m x CD M CD 5 O CJl M C/I 4J N O W O 5 CO i Ls VEL 7pgRh1lffE/
 
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Technical Report                       4-2             -ri-TELEDYNE TR-5364-1                                                  ENGlNEERlNG SERVlCES Revision  0 This version. of RELAPS NOD1 is identified by the following computer job control language at Control Data Corporation:
BEGIN, REI AP5, R5N2, INPUT=INPUTFILE, SCM=377000B The computer   analysis procedure for the thermal analysis portion is included in Appendix A.
RELAP5   calculates   hydrodynamic data for control volumes in each segment   of pipe. REPIPE then takes this data and defines two force time histories for a segment. One set of inlet junction forces, the other outlet junction forces.
SAP2SAP   adds these force time histories.     Finally, one force time history for each segment   of axial, unbalanced loads is analyzed structurally.
 
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4-3
                                                        >s-TELEOYNE Technical Report                                            ENGlNEERINQ SERVICES TR-5364-1 Revision 0 4.2   RELAP Model 4.2.1 The   D.C. Cook   pressurizer was modeled as a single time dependent volume with the following transient conditions as specified by the 1-7:
American Electric Power 11/29/82 letter to LBS, pages
:~Sf    'll Case 1:               Steam, Loopseal Case p    o g p+g e
R @~49 o   p-p pP  c~
gpg Zyoo
                                          +Palo Zt'o4p Zhs'd Pressure l WD/)
p25rg J/ O Time (Sec)
 
,.:f" ('w hl W    ~4 q; y /
                ~ .~=
0
 
is TELEDYNE Technical Report                                           ENQINEERlNQ SERVICES TR-5364-1 Revision   0 PORV Steam/Condensate   Slugs Case 2550 2500 2450 Pressure psi 2400 2350 0.8 2300 0.4          Time (Sec)       1.2 Case 2:       Continuous Warm Water = 400oF (Same pressure   as PORV, Case 1) 4.2.2 Safety valves and power operated       relief   valves were modeled as RELAP   junctions using the following information:
manufacturer    0  if'              CJJi      Ti Safety Valve       Crosby             0.022 Ft2            0.010 Sec.
HB-BP-86 (Ref. 13)
PORV              Masoneilan          0.00806 Ft2         1.0 Sec NO-38-20721 (Ref. 14)
Valve orifice areas were calculated using the EPRI Safety and Relief Valve Test Report (Reference 16) and RELAP (Run ID BAICDRO) implementing rated flows. Calculated values are included in Section 4.6.1.
 
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4 5          ]< TELEDYNE Technical Report TR-5364-1                                                       ENGINEERING SERVICES Revision   0 4.2.3 Discharge piping was modeled from all safety and power operated relief valves to the quench tank. This discharge piping included the following pipe sizes:
3             inch, 12 inch   SCH  40 4             inch, 6 inch   SCH 40S 4             inch           SCH  120 3             inch, 6 inch   SCH   160 Friction factors for 1.5       D or short radius bends and reducers were taken from technical paper 8410 by Crane. Calculations of these losses and constants are included in Appendix A. Segment lengths used are listed in Figures 4.2.1 and 4.2.2 for both models. The discharge piping defines segments with segments described as straight sections from elbow to elbow, valve to elbow, etc.
Also, a listing of RELAP5 input is included in this report. The SRV model is modeled from one safety valve to the quench tank. This was determined to be an adequate representation of safety discharge piping for both units and will subsequently be referred to as "The Quarter Model". The Quarter Model is modeled utilizing Unit 2's geometry.'.2.4 The Quench Tank was modeled         in two parts: the sparger and the tank itself. The Quench Tank is modeled using cylindrical volumes containing water and air. The volume si zes are equal to quench tank volumes provided on Westinghouse Dwg. No. 110E272.
The sparger for D.C. Cook is a perforated pipe submerged in the water within the quench tank as indicated in Figure 4.2.3 of this report. It is represented in RELAP as a pipe equal in volume and similarly submerged.
 
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  "'-""i"'""IIi TR-5364-1 TELEDYNE ENQINEERINQ SERVICES Revision 0 4-7 BY              OATE~                             SHEET NO. ~(>F CHKO. BY ~+DATE +     @~             5M&/~ Meet~~
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TR-5364-1            )> TELEDYNE ENQINEERINQ SERVICES Revision  0 4-11 8Y    A        DATE ~                        27ODAL.'D C COOL                                SHEET NO.        OF CHKO. BYMYSAYERS/                    hlUCI-r AR 8ZnJ. ~z-ICQ gg~S rf/2.                      PROJ. NO.
OF 7iVE~v'EA/CH rAdK-Q-//=gYL'-=>15gk>POLI: 'IF IOF.OF 7//E O/BiVCH 7AA/L'O 7E A<AT&#x17d;E~r'FACE:<10M iVI4T=A'U/PRICE, 70 THE C~!JT" A'/7QF IOKIZAAJTAL
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TR->>64-i        ~A~TELEDYNE ENQINEERINQ SERVICES Revision  0 I
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4-13 Technical Report Revision  0
                    ~jr'ELEDYNE ENQINEERINQ SERVICES
( BY  +A +     DATE~/LU              JDoA/ALo        c. coL A                  SHEET NO.        OF~
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Techni cal Report                                                ]5 TELEDYNE TR-5364-1                                                            ENGINEERING SERVICES Revision      0 4-16 4.3    RELAP  Model Control Volumes The  Evaluation of    RELAP5/MOD1  for Calculation of Safet /Relief    Valve Dischar e Pi in H drod namic Loads report prepared by Intermountain Technologies, Inc. recommends using ten or more control volumes per bounded segment while avoiding significant control volume length differences to preserve pressure wave shapes. The ten control volume criteria recommended by ITI was adhered to except in piping arcs and in segments less than three feet in length. The D.C. Cook discharge piping is modeled using as few as one control volume per segment (pipe segments      with lengths less than 0.5 feet)        and up  to thirty-two control volumes per segment.
Arc modeling      for both units is represented in Figures 4.3.1    and 4.3.2.
All    arcs    for Units    1  and  2 were modeled  in  RELAP as    having no  fluid losses.
Essentially, RELAP calculates these as straight sections of pipe. J REPIPE, however, distributes the calculated forces to pre-assigned node points matching the TES
  ~      ~
structural models.
Average control volume lengths used        for the    D.C. Cook RELAP Units  1 and 2 model were:
Pioe Size                            Avera  e  C.V. Len th 3  inch  SCH  160                            0.4644 feet 6 inch    SCH 160                              0.5264 feet 4 inch    SCH  40S                            0.4471 feet 6 inch    SCH 40S                              0.8614 feet 12 inch    SCH  40                            0.8064 feet 3 inch    SCH  40                            0.4744 feet 4 inch    SCH  120                            0.5056 feet schematic of the discharge systems modeled in RELAP for the PORV
                                ~
A Unit 1      model and the SRV 1/4 model for Unit 2 are given in Figures 4.7.1 and
    ~
4.7.2, respectively.
                    ~
  ~  ~                    ~
 
A TlH EDYNE Techni ca 1 Report                                          ENGINEERINQ SERVICES TR-5364-1 Revision  0                            4-17 quench Tank modeling was achieved    using twenty control volumes and twenty junctions. Eighteen volumes comprise the spar ger model while the remaining two are single volumes modeling the water and air spaces of the quench tank. The water and air volumes as determined from Westinghouse Dwg. No. 110E272 were input to RELAP to insure proper quenching capacity. Eighteen control volumes forming the sparger are initially 88K full of water representing a submerged pipe. The discharge holes were modeled as a single hole of equivalent area at the end of the pipe (a conservative assumption).
Finally, the tank rupture disk is modeled as a pressure actuated valve placed on  the air volume and set to blow out at 100 psig discharging to atmosphere.
(Figure 4.2.3 represents    the D.C. Cook Units'    and 2 quench  Tank).
 
Technical Report 1S-TELEDYNE ENGINEERINQ SERVICES e
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Technical Report
                        -ri-TELEDYNE ENQINEERINQ SERVICES 4-20
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Technical Report
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A TELEDYNE Technical Report                                              ENGINEERING SERVICES TR-5364-1                                  4-26 Revision  0 4.4    9        N d  1 Before beginning the as-built analysis for the safety valves,        it was almost certain that the loads would fail the system.            A review of the testing that was done at Combustion Engineering in Connecticut indicated this would be the case. The cold loop seal discharge test at C.E. produced loads of 175 Kips.
The D.C. Cook Units 1 and 2 pressuri zers have three safety valves each with a loop seal larger than the C.E. test facility loop seal. Therefore,          it was decided to make a small RELAP model of the D.C. Cook Safety Valve discharge line. This model contains one safety valve (SV45C) including its loop seal piping and its discharge piping through arc level 669'-2" up to, but not including, the quench tank. This model would be less expensive to run than the full three valve model.
The  results of this small (quarter Model) confirmed our suspicion that the cold loop seal case would fail. It also allowed us to make a paremetric study of loop seal temperature in loads as is shown below. Only the steam discharge proved to be acceptable, therefore, TES has recomnened to drain the loop seals.
Loop Seal Loop Seal      Temperature  Position of Valve Opening        Max Load Condition            oF        Loo  Seal      Time  Sec          LBF Col d            141o      Upstream          0.010          115,000 Col d            141o    Downstream          0.010        174,000 Hot              350o      Upstream          0.010        156,000 Hot              350o      Upstream          0.090          109,000 Hot              350o      Upstream          0.130          124,000 Hot (Sat.        650o      Upstream          0. 090          38,000, Water )
Steam              650o      Upstream          0.010            6,000 The loop seal temperature  distribution  was  calculated to  be  input to RELAP and is included in the Appendix A. The temperatures used for the cold loop
            ~  ~
seal r'anged from 584.4o at the pressurizer to 141.1o at the valve.
                          ~
 
Technical Report TR-5364-l
                      )q  ~LEDYgE EgggEERiNG SERytCES 4-27 BY  +~~          OATE~+Z2
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n-h, -;>HE. ~r FlGURE  4.4.1-3
 
Technical Report R ;; 0          A TELEDYNE ENGINEERING SERVICES 4-30 E
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Technical Report A TELEDYNE ENQlNEERlNG SERVlCES I BY P AYAF      OATE~BZ2-              bw/'1 J'cD/o          v>46M              BMEET NO. OF CHKo. eY  ~~    oaTE ~  ~  ~~
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Technical Report Revision 0      A TElEDYNE ENQlNEERINQ SERV(CES 4-32 CHKD. BY ~++ DATE ~
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Technical Report
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Technical Report A TELEDYNE TR-5364-1                                4-36                  ENGINEERING SERVICES Revision  0 4.5    Unit  1 PORV  Model The  inlet piping to the  PORV's  is sloped toward the valves. Therefore, during normal operating conditions      a saturated water (condensate) loop seal is formed at the inlet to the PORV.
As  specified in American Electric Power's letter of November 29, 1982, referring to PORV transient conditions, the following cases were modeled:
Case                                              Transient Condensate/Steam Discharge 400o Solid Liquid Discharge 4.5.1  The way  in which the condensate/steam case loopseal    was to be modeled was  decided by using two methods on a small sample model.
a~      Low  equality Steam Loop Seal (Saturated Conditions)
: b.      Solid Loop Seal (Saturated Conditions)
A  low  quality steam loop seal produced oscillatory mass flow rates through the valve. These oscillations were severe enough to cause rejection of this model and to choose the solid condensate case. These oscillations are the result of numerical instabilities in RELAP s choking correlation. This is due to the severe change in sonic velocities in the transition range between subcooled water and steam.
4.5.2  Both cases  (loop seal  and 400oF  solid liquid discharge)  were modeled and run on RELAP and REPIPE.          The  resulting force time histories    were compared. It was  not clear at this level which case was more severe. Therefore, the force time histories for both cases were input to the structural program. It could then be seen that the 400oF solid water discharge condition was the governing case.
 
                                                        ->s-TELEDYNE.
Technical Report                                              ENGINEERINQ SERVICES TR-5364-1                                  4-37 Revision  0 Both the loop seal and the  solid water  case exhibited unstable behavior  (o'sci Ilations in the flow rate). The loop seal case showed these oscillations in the transition region at the tail end of the loop seal as it passed through the valve. RELAP tends to cause flow rate oscillations because of the severe change in sonic velocities between subcooled water and low quality steam. These flow rate oscillations result in high forces which tend to be overly conservative.
In the 400oF subcooled water case, the reason for the flow rate oscillation was more obscure. At approximately .400 seconds the flow suddenly decreases approximately 30 Ibm/sec in lmsec.
This can  be seen  in Section 4.7.2. A careful review of the RELAP output did not reveal      a good physical reason for such behavior.      Reasons for such behavior could be
: 1. A sudden  reduction l
in the valve area vs. time data.
: 2. A build  up of back pressure in the discharge line which will cause the valve flow rate to'uddenly decrease..
: 3. A sudden decrease  in pressure in the pressurizer boundary condition which would result in reduced-flow.
All these things were checked to see if they were possible sources  of the flow rate fluctuation. But the review indicated that they were not the source of the problem.
 
r<  TELEDYNE Technical Report TR-5364-1                              4-38                ENGlNEERING SERVlcES Revision  0 A  partial tabulation of this review is      shown below:
UNIT  I Valve Junction
                                          &#xb9;410 Cont. Yol.              Cont. Vol.            Reference 41101                    40926          RELAP Run BHFRFGG Unit. 1  200-600 msec So 1 i d low                            Red Junction        Cont. Yol.        Cont. Vol.        Cont. Vol.
                        &#xb9;410            &#xb9;40926          &#xb9;41101              &#xb9;40926
.        Time
          .408
          .409 Flow 111.18 83.424 0.0 0.0 p
248.89 245.55 p
2342.8 3058.
It  can be seen  that the downstream pressure does not exhibit a sudden increase that would reduce the flow through the valve.              The upstream quality remains zero so that the flow through the valve is subcooled.
The pressure  increases upstream which corresponds to a sudden reduction in flow area. However, the flow area increases it does not decrease.
The pressurizer time dependent volume does not exhibit any sudden change in pressure which would correspond to this flow change.
Past experience with the RELAP programs has shown problems with subcooled water and low quality steam flow. These problems have manifested themselves as severe oscillations in the flow rate. It is our opinion that the results from the RELAP run are highly conservative and overpredict the fluid forces.
 
Technical Report A TELEDYNE TR-5364-1                                                  ENGlNEERlNQ SERVlCES Revision  0 4-39 Mhen  the fluid forces from this RELAP run are combined with the seismic, deadweight, and thermal expansion loads, the allowables were slighlty exceeded. Since the principal fluid loads appear to be a result of an instability in the flow rate predicted by RELAP and not a result of an actual physical phenomena, it was decided that these loads were overly conservative and could justifiably be reduced by 20K. 'he fluid forces presented in Section 4.8 and elsewhere in Section 4.0 are the as calculated loads and have not been reduced by 2(C.
It should be noted  that an alternative modeling practice that could have been employed in the solution of this problem would have been to make the PORV valves time dependent junctions and specify the valve flow rate. Had this been done, the flow rate oscillation and their resulting forces would never have occurred,
 
ri-TELEOYNE ENGINEERING SERVICES Techni,cal Report                          4-40 TR-5364-1 Revision  0 4.6    Valve Flow Rate Calculation TES Flow          Max Rating*
Rate Calculated      For Steam    Bore Area    Opening Valve T    e        LBM/HR          9 3X Accom.  ~IN~          Time Sec C~ros b            523,332            435,000        3.6 in2    0.010 Safety Relief                                                    (Ref. 18)
Val ve Masoneilan          199,000                                        1.0 Op      d                                                (Ref. 16)
Relief Valve
* The  maximum    rating for  steam at 3X accumulation value is from the Crosby Valve J
and Gage Safety Valve Drawing No. H-51688, Revision A.
 
Technical Report
                                                            ]i TELEDYNE TR-5634-1                                                      ENQINEERINQ SERVICES Revision  0 4-41
            ,= 4.6.1 The valve flow rates used in RELAP analysis of the SRVs were obtained by increasing the ASME rated flow by 15K; l(C to consider the ASME underating of the theoretical flow and 5X to cover tolerances.            TES flow rate calculations are included in Figure 4.6.1.
WT =  51.5  AP ASME  rated flow:
WR
                            =  51.5A (1.03P + 14.7)(.9)(.975)C              (Ref. 17) where:
WT =  theoretical flow WR
                  =  rated flow coefficients:
1.03 - applies 3X accumulation 0.975 - valve flow coefficient 0.9 - represents theoretical flow rate reduced 1(C to equal    ASME rating The  equation  TES  uses  to calculate the valve flow rate is Wmax =  1.05 x 51.5A (1.03P + 14.7)C(0.975)
This is    an  increase  of 15K above  the ASME  rated flow    as explained above.
 
                                                    -ri-TELEDYNE ENGINEERING SERVICES Technical Report                      4-42 TR-5364-1 Revision 0 4.6.2  The Masoneilan PORV maximum flow rate for steam was taken from the EPRI Safet and Relief Valve Test Re ort as 199,000 ibm/hr (Table 4.5.1-1b).
A valve opening time of 1.0 seconds is used based on total valve opening times of all Masoneilan valves tested listed in Table 4.5.2-1. Since full open times averaged 2.76 seconds, with a minimum value of 1.64 seconds, TES has assumed 10(C opening in 1.0 second, because independent testing has shown that flow is not always directly proportional to stem travel. Most often full flow is obtained before full stem travel. 8ecause 1 second is a very long opening time, this was not considered overly conservative.
 
Technical Report Revision  0        )<~TELEDYNE ENQlNEERlNQ SERVICES 4-43 sv CHKD. BY~f~DATE~~
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Fig.4.6.1-1
 
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O.OO8O(                  4/      (R ev)
Fig.4.6.1-2
 
                                                      -A TELEDYNE Techni cal Report                        4-45              ENGINEERINQ SERVICES TR-5364-1 Revision 0 4.7  RELAP  Plots The  following plots    represent RELAP mass flows, pressures and qualities at various points along the discharge piping. Since RELAP had to be restarted, the plot time scales may vary (i.e. 0.0 - 0.2 seconds or 0.0 - 0.400 seconds). Also, the ordinate axis may not always be correct; many times multipliers will be off (COC is aware of this problem in RELAP). However, they do depict the trend accurately and are calculated and reported in RELAP every .0.001 seconds.
Correct peaks and times at which they occur are listed with each trace.
Plot Set                                Tr ansi ent 4.7.1  Unit 1                        Condensate/Steam  Case 4.7.2  Unit 1                        400o  Solid Liquid Case 4.7.3    quarter Model                Cold Loop Seal/Steam Case A RELAP volume  schemati c precedes each  plot set.
 
Technical Report
                                                ]i TELEOYNE TR-5364-1 ENGINEERING SERVICES Revision  0 4-46 4.7.1 Unit 1 -  Condensate/Steam  Case
 
Technical RepA    TcLEOYN- ENGILD ~tViNG S RVIC~S TR-5364-1 Revision    0 I
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prRv'5l gl gaol
                                                        ~2 WIIIP    ~
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                              --                          <i/oy S
O o
qo
              'jo d<
gb(bl FIGURE  4.7. 1-1
 
                      <s-TEt EDYNE ENGIN:-ERlNQ SERVICES
              ,,                            4-4,8 BATEMO'87 WEAP /10DEl 9 cd PfAYz'c SHEET NO..      QS~
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3d $ 0/
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                                                                                              ,o4 o
e
                                                                                                    /LP P w oK' Y~CTM V
                                            /5rg '~  oP/4/
tO3>EI ESQ        gP f0 Qadi ni/A vcZ
                                                            ~nEES V
    ~
        /////9 ffEEi if'oo~'gi2t t.S
                                                                    ~rosi FIGURE  4.7.1-2
 
    "'""'"'WWTELEDYNEEiiIGINE            RING SERVICES Revision 0                  4-49 y ~9/      OaTE~+3-.
BY~~DATE~5A P  P ODEUM SCgrPN'7&C              SHEET NO..
PROJ, NO.
                                                                          ~
                                                                        ~~~
OF HKo.
wbJ ST7?Pr1H (gyiu gl3>b eisl f' p(t8I St30/
,                        FIGURE  4.7. 1-3
 
C)
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                                                <'/~
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ei'.DD                                                          Q (0
0.1R      0.15 TltK  (5CCl                                  0M (D
 
RELAPS/NS]/01    OR LOS  OF C93LFNT      'f 15 PR06RN 2g. sPo gg, c86 LR        0.%        L%
TltK tRCl
 
C)
O O m m
                                                            ~ ~
RELAPS/tSQl/0]4 REACTOR LOSS OF CNL AN%.>SOS PROGRAM    s Cl o
ID
 
C7 O
2 0
Dl Pl REUFS/NNI/OI        OR LOS  OF COOL D.C.CMK  UN I] PGRV  OPEN N/lH/  ~
C7 Kl M W
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                                                      ~~
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                                                          &Cl I
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0.00    O.tH      0.00        0.)2        O.l0 TltK  ISKC)
 
RELAPS/tGOI/0]4 fKRCTOR LOSS OF 000I.FAT ANFI 'fSIS PROGRfN Cl QO C)
O Cl 8
8w O IA p O
O O. IS      0.2t        0.32 Ill 0.%
(SEC)
: 0. 40        0.55
 
C)
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RELRPS/F01/01 REA  N LOSS OF CM. SA. S 5 PR  M O.H      ~ .n      O.N    LN        0.%
T]tK tSKCl
 
RELAP5/NSl/0 0 fKACT  LOSS OF COOLFN  AHA. S D.C;COOK UNI    PORIJ'tN 83/  /l O.N                  4.l2 ZlHC tSECl
 
0 C)
O O I    I RELRPS/F01/014 fKRCTOR LOSS  Of COOL%T AN%.WSIS PROGRAM O
O                                                                            I CJl ID QO Ol C)
O ID W  ID S                                                                            0 8                                                                    Vl I
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O o
0.15      0.14      0.52        O.CO      0.44 TINE (SEC)
 
REI.APS/NMll/014 REACTOR LOSS OF    N 'fSIS PRO I    I ID Kl tD I 0 Vl 3 V)
Wo
: 4) g 0  W0 I
C)
R7 ED aO 5
an        aa    aN TltK 1SKCl
 
RQ JPS/t$ 01/014      LOSS OF  CNL O.C.MX UN T  PGRV      83/ /
Cl Kl O
CI r4 O.N      O.N                  L ll T1tK tSEC)
 
O O 2
rn I
RQ.AP5/Nl01/0)l fKACTOR LOSS  Of'OOLfNT AHR. SfS PROGRAM                          d3 gh O
O C) 89.9 '~/~c.
I
                                                                    @a,.~ ~c..            Ch C) fD &#xc3;) A)
I  0 Vl X lA 0    0 CO W
X7 zm lb aO O
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D 0.$ 5      O.B        0.32        0.%        O.Q        0.56 T1HE tSECI
 
RO.missa ra m    oa t. ar Cm. S[S PRMS!f
                                              ~qp l~/~
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Kl W W CD  Kl CD I O Vl M CCl 40 D O  WO C) mz CD a
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                  ?it% (M:C)
 
l                  I  ~ ~ .I~
C7  r O  CD lll fr)
RQAPS/NR /  I                aF D.C.COOK  I  I PORV      / /
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                                                                                    <<E R7WM
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                                                                      ~. I Cl  g                                                                l/l Ch ~.
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0 CD ID CI O
Sm~
O.N        O.N        O. l2    Ooll            0.14 TltC    (SECI
 
le RELAPS/tSDl/014 fKACIOR LOSS Of CtmLt%T ANN.WSfS PROGRAM (p  f.o tgjINC Q o.~s I ~~
I  K7 (D I
CJl 0~
I lA GJ
                                                                        ~e
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                                                                              'n    %m~
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: 0. 24      0. 52      0. 40      0. 41      0.50            O.H TIE    tSECt
 
A X  CU CD REtSPS/NS /Ol REA OR  D  OF    fSR. t S PRONAtl
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M O WO I  Dl CD Kl lTl A) u  %m 5
rt LH      MR        L      LS                1.0l IltK (SD:l
 
IKLAPS/t$0 /          OR LOS  OF          SR.
O.C.CON    UN            OPEN N/ /
KI W CD I
CJl l/I
* 4J Ch O
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Tlat% l5EC)
 
C7 C) rn IUZ ED R~lt  KD D  ~ I 4
REAPS/tSD1/014 REACTOR LOSS  Of COOL%IT AH%.ISIS PRONA11 Cg CI n
M Coo ID
          =
o CI                                                                  CD M CD R                                                                    C  I  0 Vl 0 Vl CO  a)                                                              0  WA I
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CD aO Im Cl O.N                O.R Ill  0.40 (SECl
: 0. 4b
 
RELAPS/t$ 0 /Old fKACTOR I. S    F a
CJ M
~X Kl mN Cl I4 0.55                  o.n        o.a  LN TltC t5ECI
 
/NS l/Ol  REACT  OSS        CRLf%
D  .CNX lN l      1t            / /
                            /~C O.074      SeC KIWW lb Kl Cb C l n til GO ~
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C)
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: o. 10t sec, O.N        0.N      ,0.13              0.10 TltC    (SEC)
 
RELAPS/tSOl/0]4 REACTOR  OSS  Of COOLFNT RNR.YSIS PROGRfN O.B          0.3l        0.%
TlNC (SECl
 
REl.AP5/NSl/01 HER  R LOS  DF CQX.f8'NR. S S PRO
                                          > lb/~eC- 6,OS-S aC
            .g ~~/~et Q o.45 >~~
o.n        O.N      LN Z]tK (SEC)
 
0 O m
                                                            '4 REUF5/t$ 01/Ol        R L  S OF a
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                                    @  0  IGt Se(
m O.OI      O.OO          0.12        0.10  OM L24 T]NC tSEC1
 
RELAPS/MDl/Old fKACTOR LOSS  OI'N FNT FIN%. SIS PROQRAII
                                ~ Ib/~ Q g. ~(4 A4 0.%          Oo 44 T]IIL ISECI
 
U D I
m RELAPS/NDl/Ol REACTOR LOSS OF CKL  SFL S S PRONfN bI ID Q0 0
C) o C)
: 0) &#xc3;I CD I
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O  WO I
lD O
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cl 0.%    O.H      o.a        o.e    L%        O,N TltC ISKC)
 
RELfP5/180]/0          OR        OF O.C.COOK  lN l O.N        0.04          0.12 T]tfE lSEC)
 
CD CD  CD I  I m m ILC & XA.S IO Ll~    1 RELfIPS/t$ 01/014 REACTOR LOSS  OF'OOLf8 ANR.ISIS      PROQRAtl o
re Ib/Dcc (9    g. M. I I
                                                                                                    'V CJl go N0 I0 C)
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Vl 2 Vl GO ~
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                                                          -3.O Ib/~(  Q  0,373  3<(
: 0. IO      0.15        0.52        O.Q          O.ES                O.M T]NE ISEC)
 
CD O O m
RELAPS/t$ 0  /0                        S[5 PROGRAM O. Bol ~c CJ go N0 K7WW CD Me I 0 Ul
: 4) D V'A 0  W I
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          >  q  IL/~~ (ao.soS ~c Illo.a tSEC)
O.N
 
C)
RELAPS/t$ 0l/014      OR LOSS OF  IL o..can    UNr>  nevpem    / r  <
R7WW CD  R7  CD n
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enm was eas~ ia st<<es.              IA    Cl RELBPS/tSDl/014  REACTOR LOSS OF CMLFNT ANfL'fS S PROGRAM CS O
C)
O O
                                .1<9  P o,tao    -'~~
: 0. 15      O.R          0.%          O.ED    0. 4b      0 55 Tlt1C lSECl
 
RELAPS/NS)/Ol  IKA  OR  OSS  IF CN  T O.C.CKK ljNIT  P        83/ / l O.N                    O,D TlttC ISECI
 
RELAF5/NN1/0 l RERCGN t.OSS      CM  t RNR. S O.C.CRX UHlTI  P      OP& 83/ / l I
C0 CD
                                                        &#xc3;7WW CD n
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                                                        ~e o  ~N GJ wn I Ql CD          m O.M        0.00        Oe)4        0. Ii  O.X 0.24 TlNC (SECl
 
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                            ~ e \
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RElJFS/t60 /Oll    OR LOSS OF'ts      P 4
S ED M lD I 0
                                                      ~.Vl D lh 0  W I
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                                        .IAhr IWJZ C)  r C) m
                                                                                    '4 RE  /NS /    lKACI  L    &#xc3; O.C.fXNK LNl l PORV    / /
Q D.hfM<
: 0)  W  (D C    I CSI nM l/l 0 QjWO I Q d                                                                      C)
                                                  'l+ I P  Q.I74 me~
O.H        0.00 Ill LLR lSEC) 0.10                    O.Q!
 
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~ LES ll~D  lOllS ~ l~
RELAPS/t$ 01/014 RERCTOR LOSS    OF COOLFNT  ANRASfS PROGRFN D
8 OD O
8 8                                                                          0l M (D O                                                                              I  O Q
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                                              . (p'(3    Q. ' L IO O.N      O.R          O.R          0.<0        0.40              O.lt T]NC (SECI
 
StS PRONNt l
h
 
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I Q)
Ch C  I A VI Ul 2 Ao+ A 0 WOI DI C)
Kl CD C7 O.N      O.OO          Oo tQ  0 lS D.2E TlNC (SKCI
 
mnao>io>e acmroR      t.oss ar    coo.ter ma.>st r Rocaan            d3 Ra                                                                          ~
Pq o
Cl                                                                            I O                                                                            CO O
oa gd fD Xl lD c  i Ol nK N                                                                      M CAD
+d                                                                    O WO Q                                                                        I g2 O
d                = .OQ e  O.Eon    C c
o.ia    0. 24        0.32          0. Cl        0.4b
                                  'fltiC l5ECl
 
RELAPS/NS 1/0 OR  OSS OF  KLFN  NR. S S PR RFN lD Rl lD C  I 0 Ul K 4J K 0 WAI C)
O O.H            10        O.N TltK tSECl
 
                                            ~  ~
                                              '4 REUFSI  /    ACTOR  OS    OF C D..CI lNlT1 PORV OPS    83/  /1 g
O.OI    O.dd Ill 0. lR
[SEC)
Lld  0.%
 
CD O  CD IlCl l~ RALtl  ICh ~ I'Kl                I RELAPS/t$ 0]/0]4 fKRCTOR LOSS OF'fmLfST ANf%.TS]S PROQRBH O
OO 8 ci Kl W W ID Kl IO C I 0 VI CJl ~
0  W I
0 CD Kl m
n o
u O
I Im
                                      ~')        0 LCD -'CC
: 0. 14      0.24          0.32          0.<O  0. 45              0.&
t]HE lSEE]
gflI
 
C7 m m RELBP5/AD /Old REACTN LOSS OF  ESSP    fN D
C3
                                              &#xc3;lWM fb Rl 0)
CJl n~
lA 4J W 0  wn I Ql C)
K7 lb
                                                      'Z5 O  %m O.N        O.TR      D.N        0,%
TlNC (5KCl
 
CD CD m
ameSi  t'ai      Oa L  S 0P 0 C.CRK  ON T  PORV OP  / /
                                      .67/g 0.1'%$ ~c I 0 Vl K g
: 4) >
0 Ch WO I Ql CD O
O.N      0.00        0.1R    0.1I T1NC  tKC)
 
RELAP5/t$ 01/014 fK8CNR LOSS Of COOLfST fNR.YSIS PRONAtl O
                ~ 2 1 P 0.200 Sc<
O CI
 
O O m m
                                                                              ~  I RQ.RPS/N$ 1/014 RERCTOR LOSS    CNL%  FNfLTS IS PROGRAM Pg CD Xl CD I 0 Vl Z lh GO N O WO I Ql Sm g.co (9 /,0 aH        Ln          aa      aN                    l.Ol TIE (5CC)
 
REUFS /0    REACTOR L D.C.COOK UHl  l PORV I 0 o.a        O. ll TltK  ISECI
 
A z  Cg c
7C o o RELAPS/tSOI/Old REACTOR LOSS  OF'IILfST FlNFL'ISIS PROGRfN C) lD
                                                                      'ZJ O
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I. O 0.24        0.$ 2      0.40      0,%                0.ea TIE    ISECI
 
O O m m RELAP5/t$ 0 /Olk REX OR  OSS OF CML  f%fi S S PR RM I
lO
                                                                &#xc3;7 MW ID X7  CD C  I Vl Z 0
Vl Cad M 0 A    0 C)
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CD CD Pl Ptl RELAPS/ND /  1  RGCTOR L    S OF C O.C.COOK UM T    PGRV OPEN 83/(H/11 CD Rl
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IK O.OI        0.01        O. Il      O. II Tlat% tSEC)
 
RELAPS/tSDl/0]4 REACTOR LOSS  Of CKLB4    VStS PROGRAM qi      Q. 52-B 0.24        0.3l        D.40      0.%
TlHE (SIC)
 
CD m
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4 S S PRONf8 D.C. lN          OPEN  /N/
fgO3 g 0,055    c(
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CD CD CD m m IIIIICO M.O IQ    ~ I&                IQ l4 REAPS/t$ 0l/014  RERCTOR L055 OF COOLf%I AHR.TStS PRONfN O
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o a m rn RGfFS/N$ 1/0 4 REACT L OF 84K O.N                      0.10
 
O O m m IV% tSS 4~%  KR II ~    INX                    a RELRPS/t$ 01/Old REACTOR L055  OF CKILFNT RNR VStS PROGRAM I
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REl.RP5/t$ 0 /0 fK OR LOSS OF C  .FN AN . Sl PRO RM Q  1.0 >et O.H                  aa Tlat% tSEC)
 
C. COOK UNIT PORV  OPIA /M/
O.M        0.11 TINE (SEC)
 
CD CD CD m m
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o" K7  WW CD  M CD I
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CD CD CD m m
                                                                          ~  ~
e RD.APS/tSO /Oll REACTOR LOSS  OF'KL    SA. SIS PRONfN l
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RELRPS/tSO /Ol RERCTOR LOSS  &#xc3;    f%A.TS S PROGRN1 O.H      o.n        o,a    LN TltK (SCCA
 
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RELAPS/tSDI/010 REACTOR L055 Of CNILfST 8NR TSIS PROGRAII O.?.19 ~I 0,2$        0. 32      0.%        0.le TII1E (SECI
 
4 RELfPS/tSDl/0]4 fKRCTOR LOSS OF CML I MRlVl W0K R7 I
lD Ul O  WO D  I      Ql Iz C)
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    ~ .H        o.n        o.a              O.N 1.0l TltK (SEC)
 
REUP5/tSO /              S OF COOLfNT O.C.COOK LN    PORV  0    / /
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RELfPS/t$ 0 i/0            L                                S
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ID O O m m RELAPS/tSOl/014 REACTOR LOSS OF COOLFNT RHR.YSIS PROQRAtt I
C)
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RELAPS/ND1/Old RERCTOR LOSS OF C        SA 'fStS PRONN1 St P a779 ~~
O.H        o.n        0.        0.&
                      ?le  ISCC)
 
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RELAPS/t$ 01/014 REACTOR LOSS OF CKILFNT RNR.YSTS PROGRFN e M K7
(~. I CJl l/l Ch O
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0 RELAPS/tSDl/014 REACTOR LOSS OF C93L SR YS PR ED M CD I A
                                              ~'Vl  2 CrJ &
                                                    ~e O  WO I
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o o Pl MI ~ XAL%  IEO      I              I%I IA IIIIIIA  L RELAPS/tSOl/Old  REACTOR LOSS OE CMLFNT    ANI.TSIS PROCRAtl bD g5i l~ /in p ~,~m~
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O O m
RQ.APS/tSOI/O REACTOR LOSS DF COOLSI RN NSl S PR M I
4J C)
O.H                o.a Tl& tSKCI
 
RELAP5/N$ 1/Ol 9  OR    S
                                            /
Of'C.CKK UNI 1      V OPEN  83/
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o o m m
~ INCUS 0        O~ IK          ~        I RELRPS/t$ 0l/0]4 fKACIOR LOS  OF  CH)Lf% MK.YSIS PROGRAM O
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CV CII  ~                                                                      0 WO I CII Q>>                                                                          C)
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RELAPS/ND]/014    OR LOSS IF    f%FLYS S PIOCRAII
                                                      +IONIC 0.4        e.n                        O.N    ) ~
TltC ISECI
 
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RELRPS/tSOI/014 REACTN LOSS  OF CIX)LfST QA.'ISIS PRONRII O.H        Ln          o.a        LN          O.N Tl tK l5KCI,
 
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RELAPS/ND]/0]4 REACTOR LOSS  Of CIX]LEANT f%83S]S PROGRAM a.ia T]HE ]SEC]
 
REi.APS/t$ 0l/0 4 REACNR LOSS  OF COOLNIT NH. S S PROGRAM 0 4I 0Ql C)
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RELAPS/tSD1/Dld fKACTIN LOSS OF CKL  SR YStS PRONfN 0.% '.H              o.n TltC aa (5CCI O.N
 
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CD rn RELAPS/N301/014 fKACTOR L055  OF CMLfST RNR.YSI5 PROGRFN (18    /in<
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RELAPS/NSI/O fKACTOR LOSS &#xc3; C&#xc3;lM          lS PROGRAM I /in~ Q o707  sec fp9 O.H                                        LN
                    ?ltd tSECl
 
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RENPS/t$ 0 /0    OR LOSS OF    LFN      SS PRO A is7l  i I 'e o.n        o.a        AH lltK ISCCI
 
REUFS    /          OR  L D.t'.CSX tN  T  PORV    / /
C      0 Vl I
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RELAPS/tSOI/OIW REACTOR LOSS Of  CMl.fM ANR.YSTS PROGINll O W I
0 C>
O.l4        0.32        0.40      0.44      0.55    O.N TltiE (SEC)
 
4 RQ.APS/tSD1/0 4 REA OR LOSS OF      93L                        e Q) gO
~r g
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R CO K7 Pl ED O                                                            O  %m O.H        o.n        o.a                    1.04 IltC  (SEC)
 
/  /0  RGKVOR L      OF
        .CMK UNIT) PORV O.OI      0.00      0. IR TltK  (SEC)
 
4 RELAPS/t$ 01/Old fKACTOR LOSS OF'tmt.fNT AHB.YSfS PROGRAtt                      8 t+3 / ~L Qo.m~ ~
Kl W
( Vl lD I
Vl Ol O
I C)
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0.&          0.52        0. 40    0.48                O.N TltiE tSEC)
 
o o m m
                                                              ~ ~
a RELAPS/NSl /0 OR l.OSS OF      f8  RHR.'fS 5 P Nl ID 1. 4  /i<<Q o.747'-~4 R7WW lD &#xc3;I fD I 0
                                                      ~.Ol GJ
                                                            ~
A O WO I
o.a TltK  lSECl
 
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O.C. UNl    V  0 / /
I Ch CO 0 W  0 I Ql C)
O.N        L l2    Oo ll LRl TNC (5ECl
 
C)
C7 m
MRS 5 X RELAPS/tSOI/014 REACTOR LOSS  OF'LFNT  ANR.'ISIS PROGRfN b~OD
                                                                              >2.O
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RELAPS/tSQl/0 l REACTOR LOSS      SS Rt Kl W CD    CD I  O CJl M GJ Ch O      O I
0O K7 CD o
O.N        o.n        e.e          1.0l TllC (SEC)
 
IKLRPS/t$0l /0
                        .CNX lN    PORV  6' Qa xX o
e4 0.00      O,N                    L l0 lit%  lSEC)
 
tD C) m KII ~ I&
4 RELAPS/tSOl/O]4 REACTOR LOSS  Of Cm)LfST fNfiDSIS PR06RRi 4y bO
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RELAPS/t60]/0 4 IKACTOR LOSS OF      fS f%R. SlS  PROCRN)
                                ) ~~ 'Ib/y)a. ~ Q O.H        o.n        0.          IN
                        ?ltK fSK)
 
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Q C
0
 
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o  O rn rn RELAPS/tSO /0      OR  L S  &#xc3; CKNJ%T  AHfLTSt5 PROCRfN I
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O O I I m m RD.APS/tSO]/0  REACTOR LOSS OF CtmL  N.VS  S PROGRAM I
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U O m m Q~ l&h RELRP5/i%01/0)4 fKACTOR LOSS      GF CNLl%T RHH. SIS PROGRSf gran.Z        .VlC s  c
                                                                            'Og. f, a. saic.
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A)
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0.)l        0.'R          0.4l      0.4I                      O.H
                                      ?ltd  (SEC)
 
0 REGIS/NSl/014  fKACTOR 1.05  OF              S P
          .C.COOK  lN    PORV OPEN  /  /1
                                    /we. A LOI          o.a        Lll        L II TllC  l5EC)
 
RELRPS/t$ 01/01  REACTOR LOSS OF COOL@IT Mi.YSIS PROCRRN 8/2i      < . dZ I bI
-R Z) -'I lD I
CJl Vl CXh doB.3o    - 72$ Mc-  O I
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        /5L./5 .Zoo        sac 0.24
 
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l r    4 IKLfFS/NSl/Ol0  RGICTOR L        C
                                                      ~ Q) 4g
          .C.COOK UNIT  PORY OP    / /
5& A/5 I
Ol K7 M fD R3 <D I 0 Vl 0  W I
0 CD Sm z
LN                    0.11 TIE  (SEC) 8
 
RELAPSINO)IO]1 RERCEOR LOSS OF  CKLfS RUB. S S PROGRAM lWKKZ.WZ, sac I
Ch lD M tD
                                                          ~~Vl V n
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Ia X!
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0.14                  0.40                4.%    4.M TltfC (SECI
 
O O m m RELRPS/NS /0]4  fKA GR      OF        QA. PR
          .C.COOK LNlT  PORV OPEN    / / 5 gp Pre@ ./FR      sEc II) X7 II)
C
                                              >.03I  0 VI 4) g 0  W I
0Ill CD III oI  %m IL ll T]!C (5KCI
 
e.a RELRPS/NlDl/014 REACTOR LOSS Of COOLNT AH%.TSIS PROGRAM I
i.di5.    . 536  sEc 00 CD Kl CD I 0 Vl K Vl GJ M Wo 0%A+
I CU C)
Kl Sm CD I3 O
0.24                  0.%        0.4I TltK (RCl
 
RELAPS/NN1/Ol d REACTOR LOS                PR D.C.COOK U I  1  PORV  P  /  /15 LN          LQ      L ll tltC  l5ECI
 
O O rn RELAP5/tSD]/0]4 fKACTOR  LOSS OF CMl AHR.WSIS PROGRAM CI I
CO CD D
OO RIME CD n
Vl M Vl 0 AI h
Cl x
CD Xl Pl Cb aO Im e4 0.! I                0. 1R      0.40              0,54  O.H TlNC lSECl
 
lKLAPS/NN]/    REA R  0  OF C O.C.COOK UNlTl PORV    fN / /
LN        LQ
                    'tltK l5Kl
 
a V
 
CU O O m m RQ.flP5/t601/Old REACTOR l.OSS OF'&#xc3;L    NR.'fSIS PROGRN1 tD M CD CJl n~
0 QwI nDl K7 I IP o
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IKLRP5/NSI/014  REACTOR                        PR
                    .C, CMK    H      V  0  /M/5.
kt~.@
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l4 LCN    aW        ~ - La        Ll2    L lO twas ISCCI
 
D D Ill IL% XS II.IL'D M II ~
REAPS/NOI/OIN REACTOR LOSS  Of m.FAT SJR.YSIS PROCRAI1 o
O
                              .9MZ~      . L,lb Mc O
riI eAIMS X7 III I n
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o wn I Ql C)
Kl
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5 5:
: 0. I4    0.Q4      O.Q          o.e      L%                0.44 TIlK ISECI
 
m
                                                                            '4 IKUP5/tSO /Old    OR  OS  OF      SA. S S  ON%
O.C.CNK UHITl PORV  OP% / /  5
( M 0M CD I
CJl CD CD CD CD o  Sm
                                                .oSS    . Zo Mc Lll      L li      OM      O.QI TltC I5KCI
 
RG.APS/tQDl/014 RERCTOR LOSS OF COOLFNT RNR. SlS PROGRRt
            .0358        .Zm  s  c, D
85 o
d O.tS      0.24      O.R          O.CI                0.54 Tlat% (SECl
 
REUFS/NR1/014 fKACTN LOS
          .C.GXK UN  PORV LR  'll TltK (5ECl
 
REl.fit'5/l13OI/014 REAOIOR  LOSS OF  O  I.ISIT ROIS.ISIS PRORRRII D
                .~gag        a    . Zua SSC" OD o
CIS Kl CIS tll D                                                                                I  0 Ul C/I CrJ Z
N 0 440I D                                                                          CD D                                                                                  Kl CD O
5
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O. ID        D.iI        O.JD        0.%                      0.$ l TltK  tSECl
 
REurS/mO  /
                      .C.COOK UHltl PGRY      / /
a    . 8$    Q  OsG' Ql 8
                                                    . ZooSEC d
LN                  La        eo lh    LII TltC    ISKCI
 
O O 114 A.ILCS  SC  ll ~  1M RELflPS/tGOl/014 fKflCTOR LOSS OF CRW.f%T SADSIS PROGRfN CI g  Z    u .Zce) SEC 0+
D
          +a 0O O
O. li      0.34        O.R        Oo 40 fly tSECl
 
IKUFS/NS I/014  KACTOR LOS                  S S PRONfN
                .C.COOK UHI  PORV  % S3/  / 5.
a d
aa                            L l2      Lll T]tK t5KCl
 
CU o o rn m
+~serum~          3i RD.BPS/tSO1/0] REttCTOR l.OSS Ot COOt.SIT BNB.TStS PRONN1 oQ Q go C/l CL
    ~  O                                                                0  W I
n O
CO Cl d.
0.1$                0.5R        0.40        0.4I T]NC tSEC)
 
O O m m REUFS/tSO /0 l4 REACTOR    S tN    P OF'.C.COOK U        OP / 115.
I
( Vl 0 lD .Xl I
CD V'A O  WO I
C)
Kl    m P
lD a
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U D m m ac~air.~il RQ.APS/t$ 0l/Old REACTOR LOSS  Gf COOLFN  RNH.ISIS PROGRAM d
nO <
Sd' lD %7 fD I
Ol 0
V'e K0
      ~                                                                    0  wn O                                                                      I Z
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: 0. J4                  O.Q                    D.il
                                        ?ltd  (SEC)
 
RELAP5/NR)/0] REACfN        OF    SA. 5l5 PRQGRAtl D.C.mt'NIT1    PORV OPEN /M/ 5.
La          L l1    L10 IltK lSECI
 
O  CD I  I rn rn ted I5~1LLL  5C  II ~
RELAPS/NO /Ol REACTOR LOSS OF COOLfST SA.YStS PROGRAM
                ~)
cI nD Q Bo 8                                                                      ( WUl rlY ID I
CI)
III I<
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CD Iao rI' O. I0                O.R        0.40                0.54  O.H TilC  tSECl
 
C3 REUFS/NR /0]  REACIOR LOSS OF O.C.COOK LN        V    EN / /  5 C)
D O
D Q0 Bd CD M CD CJl n~
ar Vl                                                'N 4) D 0 w I Ql n
C)
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OoH        Lle        Ll2      0 li l]lK tSEC)
 
                                                                                  $i O O Pl RE1 RPSlt$ 01!Old RCACNR LOSS OF CKlhfW    YSfS PR06RSt I
o CO CD ~I ClCD N
Vl  ~
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                                                                              'aCD O
d.
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CD CD CD rn IKLAPS/%0l/Old  RE  OR      OF    SA. S PR06RNl
          .C.COOK UHlll PORV OPEN /N/
I lO Vl K n
Vl 0  W I
0Al CD K7 Ib el ID LOI                    O.D YllC  (SECl
 
CD O Dl Pl
<<<<a    <<<<~a RELAP5/N01/014 REACTOR LOSS OF'OOLFNT FFHFl.'YSI5 PR06RAN I
h3 CD CD AIMS CD M (b Cl Ul Vl CA  M CL a                                                                        O CsO I
CD O
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IKLJF5/t801/014 RGEIOR  LOS  OF      SFL  S S PRONA O.C.COOK  Nl  PNV    OP / /  5
              . 9y'<)2+49 . oswscc La        L l1    L li T]% tSECl
 
RELAPS/N)Dl/014 REACtOR LOSS    OF CNM.RJT RNA 'ISIS PROGRAtl
                    .CAP      ~ ZOO 0  C
      /099-'/S.s895        c.
 
4 RELAPS/t$ 01/0 I 0 IK        S              lS RON                              8 C.COOK UHIT  P    V OPEN / /
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M C)
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        .58          . oz8  'saic Im All                      0.24 T]tK    lSECI
 
RQAFS/tSDI/Dll REACTOR LOSS OF'ODLFN  ANR VSTS PROCRfN I
PO C)
R7 WM CD M CD I 0 Vl V M GJW 0  W  0 o      f
:  Sm O.R        0.52      o.a      0.4I              O.M TltK tSEC)
 
CD m
RELfPS/t$ 01/0]4 fKACTOR L055    Of'N            SlS P O.C. COOK UN 1  PORV OP    /    /15.
                      ,9c7+gC)Q 0$ 'g    Sk'C I
M CD Ol
                                                                                      ~E
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I  0 CD P1 Im Z/Spy'    Zoo SEC O. Il                          D.R4 TIE    ISECl
 
o o IQR 4CD M.lt.&  S%  ~ l&l  ~      p REI.OPS/tS01/0]l REACIOR  LOSS OF  CKLfSZ RNfi.ISIS PADNAG
                                . Z/3dg no D
gl CC
              ~n O
                              .o 3    S      ~ 9/8  ~Bc 8
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O O I I rn aaaa ua.a m  a~
RELAP5/NS1/014  REACTOR LO 5                  SIS PRONOUN O.C.COOK  lN T  PORV OPEN 83/  /15.
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d 4a                            LQ        411 TltK ISECl
 
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0 A    0 I Ql C)
K7 CD O
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CD  O I  I m
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va-A>64-1)<TELEDYNE ENQINEERINQ SERVICES Revision 0 BY SA 2 DATE'/-XF-83 CHKD.BYE+DATE~4-15 Z)ON A I D C.COO/Qg+LEpp((y 5/lj.a7 871&J~IV ITS 4 r~Z.kE~LiV'5"if&#xc3;nJC//~/I AJAR P~L/Alb.SHEET NO.OF~PROJ.NO.I E Qw~~o-pZ I I ji ,t I o Wk fj.I I~j>~I~C 1q I-I-I I Q 0 0~S I!FIGURE 4,2,3-6 Techni cal Report TR-5364-1 Revision 0 4-16]5 TELEDYNE ENGINEERING SERVICES 4.3 RELAP Model Control Volumes The Evaluation of RELAP5/MOD1 for Calculation of Safet/Relief Valve Dischar e Pi in H drod namic Loads report prepared by Intermountain Technologies, Inc.recommends using ten or more control volumes per bounded segment while avoiding significant control volume length differences to preserve pressure wave shapes.The ten control volume criteria recommended by ITI was adhered to except in piping arcs and in segments less than three feet in length.The D.C.Cook discharge piping is modeled using as few as one control volume per segment (pipe segments with lengths less than 0.5 feet)and up to thirty-two control volumes per segment.Arc modeling for both units is represented in Figures 4.3.1 and 4.3.2.All arcs for Units 1 and 2 were modeled in RELAP as having no fluid losses.Essentially, RELAP calculates these as straight sections of pipe.REPIPE, however, J distributes the calculated forces to pre-assigned node points matching the TES~~structural models.Average control volume lengths used for the D.C.Cook RELAP Units 1 and 2 model were: Pioe Size Avera e C.V.Len th 3 inch SCH 160 6 inch SCH 160 4 inch SCH 40S 6 inch SCH 40S 12 inch SCH 40 3 inch SCH 40 4 inch SCH 120 0.4644 feet 0.5264 feet 0.4471 feet 0.8614 feet 0.8064 feet 0.4744 feet 0.5056 feet A schematic of the discharge systems modeled in RELAP for the PORV~~~~~~Unit 1 model and the SRV 1/4 model for Unit 2 are given in Figures 4.7.1 and 4.7.2, respectively.
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Techni ca 1 Report TR-5364-1 Revision 0 4-17 A TlH EDYNE ENGINEERINQ SERVICES quench Tank modeling was achieved using twenty control volumes and twenty junctions.
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Eighteen volumes comprise the spar ger model while the remaining two are single volumes modeling the water and air spaces of the quench tank.The water and air volumes as determined from Westinghouse Dwg.No.110E272 were input to RELAP to insure proper quenching capacity.Eighteen control volumes forming the sparger are initially 88K full of water representing a submerged pipe.The discharge holes were modeled as a single hole of equivalent area at the end of the pipe (a conservative assumption).
Finally, the tank rupture disk is modeled as a pressure actuated valve placed on the air volume and set to blow out at 100 psig discharging to atmosphere.(Figure 4.2.3 represents the D.C.Cook Units'and 2 quench Tank).


Technical Report 1S-TELEDYNE ENGINEERINQ SERVICES e BY+DATE CHKO.BY~+~OATE~'7 83~om<~Pq Mooel@@9-Z g~i f'3 SHEET NO.<>'S//FIGURE 4.3.1 ggP: a&(cg~c t2-9/-8 I 0 nq Yl~4'I/E'~P!~Q r.ro V',o ,/,/.~o',, i b b T S T O/4 1 0 E'S Qgc S4 O IN O ES IIO Y T Technical Report Reyision P I I TELEDYNE ENGlNEERlNQ SERVlCE$4-19 BY-DATE CHKD, BY~C~DATE 2 I~83 SHEET NO.OF PROJ, NQ.FIGURE 4.3.2-1 IZ~AFM02)eZ.OF nile (a~~EVW77OV 4~9'-2" (A/C X)~S T I/)S 5+r=-r.rsv''~I I/p.>ok l a.~c~&559'l0 C"eP SCb VALVE'i.I3.70" Technical Report-ri-TELEDYNE ENQINEERINQ SERVICES 4-20 By'8 DATE~~CHKO BY~OATS~+s c.cook'A'/7-4 ARC~&~oem/'~'@zL~V.
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Technical Report Revision 0 A TELEDYNE ENQINEERINQ SERYlCES 4-22 eY<>+DAve>~s 4>CHKO BY, OATEYT 23 so J un i z i waRv sEc.ri o~RE't A'P HobGL.(D>~<5TPCRM)
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Technical Report-rS-TELEDYNE ENQINEERINQ SERVICES 4-25 ST<-<ORTS~>><~CHKO.BY++DATE~~~+~oN tT'PoRV St=c T>cM BRAW)cRE5+75ES SHEET NO.OF z z PROJ, NO,+3++FIGURE 4.3.3-2 702 54&c3 oA yH Z~n 0 ta SNAKC.g uu EJ5M-+ISZ9 Si3 gN~tuN 3PAMC//l 5///9 5 lg.5N6 L vs Go+$N&VUH+pe SHC L~N~, I HoI2S BRANCH Jog 0/(yP zZSri~)40$SNAB gZu~hJ 0 08 SNGLJ uhl go~gg goy'BRANCH 4090/(EJJ sr~OJF~)
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Technical Report TR-5364-1 Revision 0 4-26 A TELEDYNE ENGINEERING SERVICES 4.4 9 N d 1 Before beginning the as-built analysis for the safety valves, it was almost certain that the loads would fail the system.A review of the testing that was done at Combustion Engineering in Connecticut indicated this would be the case.The cold loop seal discharge test at C.E.produced loads of 175 Kips.The D.C.Cook Units 1 and 2 pressuri zers have three safety valves each with a loop seal larger than the C.E.test facility loop seal.Therefore, it was decided to make a small RELAP model of the D.C.Cook Safety Valve discharge line.This model contains one safety valve (SV45C)including its loop seal piping and its discharge piping through arc level 669'-2" up to, but not including, the quench tank.This model would be less expensive to run than the full three valve model.The results of this small (quarter Model)confirmed our suspicion that the cold loop seal case would fail.It also allowed us to make a paremetric study of loop seal temperature in loads as is shown below.Only the steam discharge proved to be acceptable, therefore, TES has recomnened to drain the loop seals.Loop Seal Loop Seal Temperature Position of Valve Opening Max Load Condition oF Loo Seal Time Sec LBF Col d Col d Hot Hot Hot Hot (Sat.Water)Steam 141o 141o 350o 350o 350o 650o 650o Upstream Downstream Upstream Upstream Upstream Upstream Upstream 0.010 0.010 0.010 0.090 0.130 0.090 0.010 115,000 174,000 156,000 109,000 124,000 38,000, 6,000 The loop seal temperature distribution was calculated to be input to~~~RELAP and is included in the Appendix A.The temperatures used for the cold loop seal r'anged from 584.4o at the pressurizer to 141.1o at the valve.
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Technical Report TR-5364-l)q~LEDYgE EgggEERiNG SERytCES 4-27 BY+~~OATE~+Z2 CHKD.BY~>+DATE~/g/J//"/p~/O Vdtb'~c~/gc.c v/~wc nl+<%Y SHEET NO.OF 1 i/F7<V4'//, nlR'y/5 3/c o Wrac/~<: 8'HE'W~4.d~4~ovggrrsr-rrFAFE=(r~gFr s-jest,.z@)r=r=rE g 9g F r ggyp/-r., goo C4 CM-~"/.%9O~r i~25/os&z5 C/o DFl//O<)gcr2 Ff Z4>PC 7P y)PA.Vg-4 2 Q 5q F r g.(18)jF FIG.4.4.1-1 Technical Report 8>TELEDYNE ENGINEERING SERVlCES 4-28 sv~~+oAva~~>8~CHKO.BY~Es CATE~~TEST
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Y~~~Spy/ru'E~&f i v-aux<s~jzr+pr ipse'ud 4)z.-gw9 wr FIGURE 4.4.1-2 Technical Report Reyi si on p 9E TELEDYNE ENQINEERINQ SERVICES 4-29 SY<~~DATE'i 8~;4<<f CHKD.BY~DATE~<A grD Vague&a<ggrV Prod Pea v w'g~p SHEET NO.OF 8 b 8b'g zv zr X y5ZPr iso 0.9r//Fr Er v<<&#xc3;r~4<dgg wy~i@+i j~g y</>"-O'P 7~~,-S9=9.2/87'<n-h,-;>HE.~r FlGURE 4.4.1-3 Technical Report R;;0 A TELEDYNE ENGINEERING SERVICES 4-30 E ST~~~OATS~SEE S CHKO.BY~~DATE>~j/~rgb Vol 6'~8 ggzgyg h'Pont Age'>447 E SHEET NO.OF E PROJ, NO./d//Uec-bi-/7.-fc US&U'A, YflP-/$$0$y" (/P/J)r=d.ro fH/./QN/+Z',<pz/7/.S'/O/A,+y,/d US'AF)(!/"$+F P<BQOgFF)I r)r~j//',/z&o 7dr8 c.cq g/g/PM AJ F DxN A A.use<gnarl+~'L (.</P<-o'za)FIGURE 4.4.1-4 Technical Report A TELEDYNE ENQlNEERlNG SERVlCES I B Y P AYAF OATE~BZ2-CHKo.eY~~oaTE~~~~bw/'1 J'cD/o v>46M E'P~cvuFM~~
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BMEET NO.OF vH~vZ az: NAY/5I ac///'eo p/r/Nc r7KEE-O.d9$5 r 7<88 g g/g M4M',/p F'r a.co8 pr 0 F~Cgcc~c.c~;g.g.'9 K Cl d.25'2 ii I/7o~+E vened=y za(F/z.~zw~d.Ei8 g W r FIGURE 4.4.1-5 Technical Report Revision 0 A TElEDYNE ENQlNEERINQ SERV(CES 4-32CHKD.BY~++DATE~~~Drtfr1'c&ro vo4uwz 5z<u~no~~agv'e'<E<SHEET NO.k<>F&I=a.rotag+r jy=M ia W v.cr)<(u.its~~<<)g3 Jr'.@~9'oui vying'iu i-i.u<zsiic i-w gian r us~)2.&S P FIGURE 4.4.1-6 Technical Report-ri-TELEDYNE ENQINEERINQ SERVICES 4-33 cHKD.8Y~QATK~TT PaEV}PfcE'w-'LOS.t~oQELEQ Fog QQQp~.'3N lT'HEET Np./pF PROD.NP.2&Oo p ic 4)ue+I gP'i 15 z'JC+i l<gC~'7 i(ol~...g=.09zl r4 Abut ,c 885~+hg"g-(, O92i H-')/j.oo 8~>l')l.~(~PP fi)/(, (ZOC 2, il'8~)=.f~77 L~,@77 T,TZI-'f.(;z.@X','=-~Yd'>'gieuiC i/)i/OS m POl l.I)'tO-;i.oa5V kf~3,tu i Ng~~r i i'QA-)/(6 c ei-~4.98 7 Lh~(,age I f)~)/(,,molo8 Il i)of J.J)8 FIGURE 4.4.2-1 Technical Report p)g~LQDYQQ fNQpJQQQgQ
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Technical Report TR-5364-1 Revision 0 4-36 A TELEDYNE ENGINEERING SERVICES 4.5 Unit 1 PORV Model The inlet piping to the PORV's is sloped toward the valves.Therefore, during normal operating conditions a saturated water (condensate) loop seal is formed at the inlet to the PORV.As specified in American Electric Power's letter of November 29, 1982, referring to PORV transient conditions, the following cases were modeled: Case Transient Condensate/Steam Discharge 400o Solid Liquid Discharge 4.5.1 The way in which the condensate/steam case loopseal was to be modeled was decided by using two methods on a small sample model.a~b.Low equality Steam Loop Seal (Saturated Conditions)
                  ~ a~ t wio *vs  ~
Solid Loop Seal (Saturated Conditions)
~
A low quality steam loop seal produced oscillatory mass flow rates through the valve.These oscillations were severe enough to cause rejection of this model and to choose the solid condensate case.These oscillations are the result of numerical instabilities in RELAP s choking correlation.
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This is due to the severe change in sonic velocities in the transition range between subcooled water and steam.4.5.2 Both cases (loop seal and 400oF solid liquid discharge) were modeled and run on RELAP and REPIPE.The resulting force time histories were compared.It was not clear at this level which case was more severe.Therefore, the force time histories for both cases were input to the structural program.It could then be seen that the 400oF solid water discharge condition was the governing case.
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Technical Report TR-5364-1 Revision 0 4-37->s-TELEDYNE.
IW  - 4                                       jv&
ENGINEERINQ SERVICES Both the loop seal and the solid water case exhibited unstable behavior (o'sci Ilations in the flow rate).The loop seal case showed these oscillations in the transition region at the tail end of the loop seal as it passed through the valve.RELAP tends to cause flow rate oscillations because of the severe change in sonic velocities between subcooled water and low quality steam.These flow rate oscillations result in high forces which tend to be overly conservative.
I A
In the 400oF subcooled water case, the reason for the flow rate oscillation was more obscure.At approximately
tp t'
.400 seconds the flow suddenly decreases approximately 30 Ibm/sec in lmsec.This can be seen in Section 4.7.2.A careful review of the RELAP output did not reveal a good physical reason for such behavior.Reasons for such behavior could be 1.A sudden reduction in the valve area vs.time data.l 2.A build up of back pressure in the discharge line which will cause the valve flow rate to'uddenly decrease..
                                                                  ~l C'r II
3.A sudden decrease in pressure in the pressurizer boundary condition which would result in reduced-flow.
                                                                                  'I I
All these things were checked to see if they were possible sources of the flow rate fluctuation.
                                                                                    'e t
But the review indicated that they were not the source of the problem.
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Technical Report TR-5364-1 Revision 0 4-38 r<TELEDYNE ENGlNEERING SERVlcES A partial tabulation of this review is shown below: UNIT I Valve Junction&#xb9;410 Cont.Yol.41101 Cont.Vol.40926 Reference RELAP Run BHFRFGG low Unit.1 200-600 msec So 1 i d Red.Time.408.409 Junction&#xb9;410 Flow 111.18 83.424 Cont.Yol.&#xb9;40926 0.0 0.0 Cont.Vol.&#xb9;41101 p 248.89 245.55 Cont.Vol.&#xb9;40926 p 2342.8 3058.It can be seen that the downstream pressure does not exhibit a sudden increase that would reduce the flow through the valve.The upstream quality remains zero so that the flow through the valve is subcooled.
l A                                                               ~ W      I~
The pressure increases upstream which corresponds to a sudden reduction in flow area.However, the flow area increases it does not decrease.The pressurizer time dependent volume does not exhibit any sudden change in pressure which would correspond to this flow change.Past experience with the RELAP programs has shown problems with subcooled water and low quality steam flow.These problems have manifested themselves as severe oscillations in the flow rate.It is our opinion that the results from the RELAP run are highly conservative and overpredict the fluid forces.
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Technical Report TR-5364-1 Revision 0 4-39 A TELEDYNE ENGlNEERlNQ SERVlCES Mhen the fluid forces from this RELAP run are combined with the seismic, deadweight, and thermal expansion loads, the allowables were slighlty exceeded.Since the principal fluid loads appear to be a result of an instability in the flow rate predicted by RELAP and not a result of an actual physical phenomena, it was decided that these loads were overly conservative and could justifiably be reduced by 20K.'he fluid forces presented in Section 4.8 and elsewhere in Section 4.0 are the as calculated loads and have not been reduced by 2(C.It should be noted that an alternative modeling practice that could have been employed in the solution of this problem would have been to make the PORV valves time dependent junctions and specify the valve flow rate.Had this been done, the flow rate oscillation and their resulting forces would never have occurred, Techni,cal Report TR-5364-1 Revision 0 4-40 ri-TELEOYNE ENGINEERING SERVICES 4.6 Valve Flow Rate Calculation Valve T e TES Flow Rate Calculated LBM/HR Max Rating*For Steam Bore Area 9 3X Accom.~IN~Opening Time Sec C~ros b Safety Relief Val ve 523,332 435,000 3.6 in2 0.010 (Ref.18)Masoneilan 199,000 Op d Relief Valve 1.0 (Ref.16)*The maximum rating for steam at 3X accumulation value is from the Crosby Valve J and Gage Safety Valve Drawing No.H-51688, Revision A.
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Technical Report TR-5634-1 Revision 0 4-41]i TELEDYNE ENQINEERINQ SERVICES ,=4.6.1 The valve flow rates used in RELAP analysis of the SRVs were obtained by increasing the ASME rated flow by 15K;l(C to consider the ASME underating of the theoretical flow and 5X to cover tolerances.
RELfFS/Cg /01  REACTDR    S      CMLfS
TES flow rate calculations are included in Figure 4.6.1.WT=51.5 AP ASME rated flow: WR=51.5A (1.03P+14.7)(.9)(.975)C where: (Ref.17)WT=theoretical flow WR=rated flow coefficients:
            .C.CMK  UM  I PORV  0      / /
1.03-applies 3X accumulation 0.975-valve flow coefficient 0.9-represents theoretical flow rate reduced 1(C to equal ASME rating The equation TES uses to calculate the valve flow rate is Wmax=1.05 x 51.5A (1.03P+14.7)C(0.975) explained above.This is an increase of 15K above the ASME rated flow as
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Technical Report TR-5364-1 Revision 0 4-42-ri-TELEDYNE ENGINEERING SERVICES 4.6.2 The Masoneilan PORV maximum flow rate for steam was taken from the EPRI Safet and Relief Valve Test Re ort as 199,000 ibm/hr (Table 4.5.1-1b).
yp  I ~ I~
A valve opening time of 1.0 seconds is used based on total valve opening times of all Masoneilan valves tested listed in Table 4.5.2-1.Since full open times averaged 2.76 seconds, with a minimum value of 1.64 seconds, TES has assumed 10(C opening in 1.0 second, because independent testing has shown that flow is not always directly proportional to stem travel.Most often full flow is obtained before full stem travel.8ecause 1 second is a very long opening time, this was not considered overly conservative.
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Technical Report Revision 0)<~TELEDYNE ENQlNEERlNQ SERVICES 4-43 sv DATE~~jh CHKD.BY~f~DATE~~
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=~>>~~~~i'j.-Fig.4.6.1-1 Technical Report Revision 0 A TELEDYNE ENGINEERING SERVICES 4-44 CHKD.BY~DATE~CQciwel'~>
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vA<YE'~p~rhea~@km GA~LA~SHEET HO.~OF 2 PROJ.NO.S<id,fQ/SZ S,g'/o.OS r hr=/'/S, 37~/oec THE'ornrTvTEiz
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'Qoor BA z~p'roloe.foll efoen cree in/he ron iw+cK)0 o&z.t+iloo rc,4e.Q C il ofen'g-ISO.if/~c R~ro/e.C?goto oo~;~of/l.e~l E.~/Sa oi+l~c.I RCLAPS floso c'eo'i'oh etLuErw lrilesx)E/S B7~l~e(Col&4e O8 bif inWfool;*ion, IQb y7-138.DI AAoo=o./T o//.o rg (o coed)O Q2.M 4>(v)O.OO8O(4/(R ev)Fig.4.6.1-2 Techni cal Report TR-5364-1 Revision 0 4-45-A TELEDYNE ENGINEERINQ SERVICES 4.7 RELAP Plots The following plots represent RELAP mass fl ows, pressures and qualities at various points along the discharge piping.Since RELAP had to be restarted, the plot time scales may vary (i.e.0.0-0.2 seconds or 0.0-0.400 seconds).Also, the ordinate axis may not always be correct;many times multipliers will be off (COC is aware of this problem in RELAP).However, they do depict the trend accurately and are calculated and reported in RELAP every.0.001 seconds.Correct peaks and times at which they occur are listed with each trace.Plot Set Tr ansi ent4.7.1 Unit 1 4.7.2 Unit 1 4.7.3 quarter Model Condensate/Steam Case 400o Solid Liquid Case Cold Loop Seal/Steam Case A RELAP volume schemati c precedes each plot set.
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Technical Report TR-5364-1 Revision 0 4-46]i TELEOYNE ENGINEERING SERVICES 4.7.1 Unit 1-Condensate/Steam Case
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D CI m m RELAPS/tGOl/Old fKACZOR LOSS OF CKLfNT AHfi.TSIS PROGRAM fD  M lb I 0
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"'""'"'WWTELEDYNE EiiIGINE RING SERVICES Revision 0 y~9/OaTE~+3-.HKo.BY~~DATE~5A 4-49 P P ODEUM SCgrPN'7&C wbJ ST7?Pr1H (gyiu SHEET NO..~OF PROJ, NO.~~~gl3>b eisl f'p(t8I St30/, FIGURE 4.7.1-3 C)O U Pl O.C.rp)X iWlrl Vpuy nulli'mC~t>.
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RELAPS/NS]/01 OR LOS OF C93LFNT'f 15 PR06RN 2g.sPo gg, c86 LR 0.%L%TltK tRCl C)O O m m RELAPS/tSQl/0]4 REACTOR LOSS OF CNL AN%.>SOS PROGRAM~~s Cl o ID C7 O 0 2 Dl Pl REUFS/NNI/OI OR LOS OF COOL D.C.CMK UN I]PGRV OPEN N/lH/~C7 Kl M W CD&#xc3;7 CD (I Cl~~Ol l/7 wo+w, 0&Cl I Xl CD O O d 0.00 O.tH 0.00 0.)2 TltK ISKC)O.l0 RELAPS/tGOI/0]4 fKRCTOR LOSS OF 000I.FAT ANFI'fSIS PROGRfN Cl Q O C)O Cl 8 8 w O IA p O O O.IS 0.2t 0.32 0.%Ill (SEC)0.40 0.55 C)O O m RELRPS/F01/01 REA N LOSS OF CM.SA.S 5 PR M O.H~.n O.N LN T]tK tSKCl 0.%
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RELAP5/NSl/0 0 fKACT LOSS OF COOLFN AHA.S D.C;COOK UNI PORIJ'tN 83//l O.N 4.l2 ZlHC tSECl 0
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C)O O I I RELRPS/F01/014 fKRCTOR LOSS Of COOL%T AN%.WSIS PROGRAM O O I CJl ID Q O Ol C)O S 8 m O ID~X: O n ID W ID I 0 CJl~Vl 0 WO I.QI C)ID O O o 0.15 0.14 0.52 O.CO TINE (SEC)0.44 REI.APS/NMll/014 REACTOR LOSS OF N'fSIS PRO I I ID Kl tD I 0 Vl 3 V)4)g Wo 0 W 0 I C)R7 ED a O 5 an aa TltK 1SKCl aN RQ JPS/t$01/014 LOSS OF CNL O.C.MX UN T PGRV 83//Cl Kl O CI r4 O.N O.N L ll T1tK tSEC)
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O O 2 rn RQ.AP5/Nl01/0)l fKACTOR LOSS Of'OOLfNT AHR.SfS PROGRAM I d3 gh O O C)-89.9'~/~c.@a,.~~c..I Ch C)O~l fD&#xc3;)A)I 0 Vl X lA 0 W 0 CO X7 lb a O z m O D 0.$5 O.B 0.32 0.%T1HE tSECI O.Q 0.56 RO.missa ra m oa t.ar Cm.S[S PRMS!f-~qp l~/~Q IO~c(Kl W W CD Kl CD I O Vl M CCl 40 D O WO C)CD a O mz Rm O.H~.a O.IO LN?it%(M:C)loOl
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REl.AP5/NSl/01 HER R LOS DF CQX.f8'NR.
RELfF5/tSQ /     RE  OR    5      CM  % T PRONATE
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01/014 REACTOR LOSS OF'OOLf8 ANR.ISIS PROQRAtl o re Ib/Dcc (9 g.M.I I'V CJl go N 0 I0 C)O CI gO o c4 I AIMS ID R7 CD n Vl 2 Vl GO~0 wn CD R7 ID O-3.O Ib/~(Q 0,373 3<(0.IO 0.15 0.52 O.Q T]NE ISEC)O.ES O.M CD O O m RELAPS/t$0/0 S[5 PROGRAM O.Bol~c CJ go N 0 K7WW CD Me I 0 Ul V'A 4)D 0 W 0 I Ql CD X7 tD C5 O>q IL/~~(ao.soS~c o.a Ill tSEC)O.N C)RELAPS/t$0l/014 OR LOSS OF IL o..can UNr>nevpem/r<R7WW CD R7 CD n CJl M l/l 4J~EZl~0 A n I QP C)X7 CD a O O.N 0.00 O.Q TIE (SEC)0.1I O.XI a 0~~7 Q O.i97~C 0 24
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RELAPS/INOI/OI4 REACTOR LOSS OF'INLFN ANfl. SIS PROGRAM
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Technical Report A TELEDYNE ENQINEERINQ SERVICES 4-245
  ~g        DATE  1 /i-88              pl oQE'g        SRv      0 Isa'Hatt.ce SHEET NO. I  OF
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O O m m RQ.RPS/N$1/014 RERCTOR LOSS CNL%FNfLTS IS PROGRAM~I Pg-g.co (9/,0 CD Xl CD I 0 Vl Z lh GO N O W O I Ql Sm aH Ln aa aN-TIE (5CC)l.Ol REUFS/0 REACTOR L D.C.COOK UHl l PORV I 0 o.a O.ll TltK ISECI A Cg z c 7C o o RELAPS/tSOI/Old REACTOR LOSS OF'IILfST FlNFL'ISIS PROGRfN C)lD'ZJ O C+I.O 0.24 0.$2 0.40 TIE ISECI 0,%0.ea
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01/014 IKACTOR LOSS OF C93L AIR.S[5 PROQRfN RELfPS/t$0 i/0 L 0.COOK LN I PORV OP//4 S qg97 Q pa a<I lO O~.CJI Dm:" Sm O.Ol 0.00 0,!2 IJlK lSEC)O.l0 ID O O m m RELAPS/tSOl/014 REACTOR LOSS OF COOLFNT RHR.YSIS PROQRAtt I C)K7WW CD Kl CD I 0 CJl~Vl 0 W 0 I AJ C)Xl CD CI O 0.24 0.52 0.%TIHC tSECl 0,44'.M RELAPS/ND1/Old RERCTOR LOSS OF C SA'fStS PRONN1-St P a779~~O.H o.n 0.0.&?le ISCC)
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/Ol OR LOSS OF US.5 PROGRfN Q o xR'I--~>X'+/n<]ad At.O mO~<i A o a AH ATl ACI Ill l5ECl
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RELAPS/tSDl/014 REACTOR LOSS OF C93L SR YS PR ED M CD I A~'Vl 2 CrJ&~e O WO I C)ED Cl O CV'.M o.n~.a ltlC tSECl REUFS/NS I/O O.C.CQX UH Tl PORV O.N O.M 0.)2 TlNC lSCCI


o o Pl MI~XAL%IEO I I%I IA IIIIIIA L RELAPS/tSOl/Old REACTOR LOSS OE CMLFNT ANI.TSIS PROCRAtl b D-g5i l~/in p~,~m~~D 8 Qa lD CI Vl 0 wn I QI C)(0-:Im 0.!4 0.&0.00 TltlC lSEC)0.40 O.H O O m RQ.APS/tSOI/O REACTOR LOSS DF COOLSI RN NSl S PR M I 4J C)O.H o.a Tl&tSKCI RELAP5/N$1/Ol 9 OR S Of'C.CKK UNI 1 V OPEN 83//O.lk TltK (SIC)0 Ib o o m m~INCUS 0 O~IK~I RELRPS/t$0l/0]4 fKACIOR LOS OF CH)Lf%MK.YSIS PROGRAM O te CV CII~Q>>K7 M M CD Kl CD C I A~.CJl~Ill GD~0 WO I CII C)X7 CD a O C+lTl lm O.I4 0.&0.52 0.40 0,4b 0.50 T1NE (SfCl O.M RELAPS/ND]/014 OR LOSS IF f%FLYS S PIOCRAII 0.4 e.n TltC ISECI O.N)~+IONIC
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C)O O m m h%%8 SM 0 IW~L RELAPS/tSD]/0]4 REACTOR LOSS OF'KLFNT 8Hfi.YSIS PROCRfN~~0 8V C)Xl I a O o.Le 0.3l o.io TltK (SECl 0.45 O.M r%%II f i'I I II'I'il W i~r r s g U 0 IJ l RELAP5/t$01/0 OR OF C 0 C.CNX N/t POAV OPEN//O.M O.N O.lR LLS TIE l SEC)
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REUFS/NR1/014 fKACTN LOS.C.GXK UN PORV LR'll TltK (5ECl REl.fit'5/l13OI/014 REAOIOR LOSS OF O I.ISIT ROIS.ISIS PRORRRII D.~gag a.Zua SSC" OD o tll D D D CIS Kl CIS I 0 Ul Z C/I CrJ N 0 440 I CD Kl CD O 5%m d O.ID D.iI O.JD 0.%TltK tSECl 0.$l REurS/mO/.C.COOK UHltl PGRY//a.8$Q OsG'Ql 8 d LN La eo lh LII TltC ISKCI.ZooSEC O O 114 A.ILCS SC ll~1M RELflPS/tGOl/014 fKflCTOR LOSS OF CRW.f%T SADSIS PROGRfN CI g Z u.Zce)SEC 0+D+a 0 O O O.li 0.34 O.R Oo 40 fly tSECl IKUFS/NS I/014 KACTOR LOS.C.COOK UHI PORV%S3//5.S S PRONfN a d aa L l2 Lll T]tK t5KCl CU+~serum~3i o o rn m RD.BPS/tSO1/0]
CT t. 5 Of'MLfMNFL)Sl    PROGRNl BEP UNtT2    1N  REUPS  10  /05.
REttCTOR l.OSS Ot COOt.SIT BNB.TStS PRONN1 o Q Q go C/l CL~O O 0 W n I CO Cl d.0.1$0.5R 0.40 T]NC tSEC)0.4I O O m m REUFS/tSO/0 l4 REACTOR S OF'.C.COOK tN P U OP/115.I lD.Xl CD (I 0 Vl V'A O WO I C)Kl lD a O P m Im 4N 4ll Tlirt (MXl)421 ac~air.~il U D m m RQ.APS/t$0l/Old REACTOR LOSS Gf COOLFN RNH.ISIS PROGRAM d n O<Sd'K~0 O lD%7 fD I 0 Ol V'e 0 wn I (D O Z Ill Im d 0.J4 O.Q?ltd (SEC)D.il RELAP5/NR)/0]
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RQAFS/tSDI/Dll REACTOR LOSS OF'ODLFN ANR VSTS PROCRfN I PO C)R7 W M CD M CD I 0 Vl V M GJW 0 W 0 o f: Sm O.R 0.52 o.a TltK tSEC)0.4I O.M CD m RELfPS/t$01/0]4 fKACTOR L055 Of'N SlS P O.C.COOK UN 1 PORV OP//15.,9c7+gC)Q 0$'g Sk'C I M CD Ol&#xc3;7 W W fb Kl A)I 0~E IS CD P1 Im O.Il TIE ISECl Z/Spy'Zoo SEC D.R4
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I II CD O I I m Il4t ZES CLILZR~~CNS RQ.RPS/tNOl/Ol REACTOR LOSS OF ILfS AN8.Sl S PROGRAM CS.Zd5 5~/9.g/5 SiC-I CD Oo o 8 Qo lA C CC:~n O.0 3/44 s CD M CD C I 0 CJl~Vl 040 I Ol CD Kl CD O C+0.14 0.Q4 0.40 TINE ISECl 0.44 0.44 I k.*t~
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REACTOR LOSS Of CMLfS QA.VSIS PROGRAM ID M Ib I 0 CJI D I/I 0 W 0 I Al CD X7 ID el O I rs I tr.-i'P'I-I 4 k t"/tl h: t I~'E 1 I f t t l'g~r S a waie a~v 4 RCurSnao>ip>c mcrOR L or c SI P.C.CMK l PORV OP/5.-gg (Q 0 SF-C-1N O.ll 0 tl T]IK lSECI ply~P'hl'Jl r 1 1~~t r a'<)I~~~%-P
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01/014 RERC1'OR LOSS OF CRN.SJT RNFl.fS[S PROCRAtl g O 8 X<<5.S MC>EGAD o mn I Al CD a Z3gg.d'c D.ID 0.%0.40 TltC lSEC)0.50 O.H D~
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4 REACTOR 0 OF'C.COOK lNl l PORV OP%/M/l5.~~~I tD X7 (b c i n Ul M Vl 0 W n I C)LOI Ll1 TltC l5KC)
~II W'A 4W 5~~<<7'<~I'I'I 1\0~I 1 f~p~4 I t I i f~I I , Wa<<I<<1 W<<j i I~" I~'I~"1 1." I RELAPS/tSOI/O 4 REACTOR LOSS OF'OOLfST RNFL SlS PROGRFN O.R TltK tSECI II I 4 II lt I i'I'L 1Q l f I 4*1 ,*m'At WO I'I Og'N'~A&%4 A RELAP5/%0/0 fKACTOR L S o 3/7 Q 0 SEC g 4~A~V h, I l 3 t I~l I E 4 l.I VA~~)J&"~1'.?t.4 I I I t-~~l I V'~.c'f I a IV~~n'v l l I,,'hV REI.APS/tS01/OIW fKRCKR LOSS Of'HMRT AN%.'ISIS PROGRNI CD M A)n Vl K M o wn I 0.14 0.5R 0.40 ZltlE I SEC I 0.55 l~i g I;I~Jv I k rC at, j I~'I I jv II IL IS 11 Ie RELAPS/t$01/Old REACTOR LOSS OF CNILf8 R.VSIS PROGRAM.Zoo SEC O.R oe tltK ISECI 0.%O.Q A I i l J'1~f*S (P C'I I j~.~o Il e~k'l I 4 i 4~*~)4'tA A Wy~I&I'J f~<<~N 4+=~~8"~4 O 0 I I m m C.COOK Nl PORV OPEN nH<15../9'fsEc I M C)/.z/~s.c.L l2 TltK (50:l LLI Lit 4,~Vl g 44 4%gal!'4l/I 4 4 g 4~.g*MO~t jr k I l''~IJ'4 4 J 4'I i jl l L)~'0 Q>'4~~4'I 44\l C I\4 p I'4~4"~~+" 4 eve CU O O rn RQSPS/N01/0 4 REACTOR LOSS OF CHX.FAT AH%.'fSIS PRODRRN Qo X r P4 QA 8 Ra Cl 0.lD Kl O.Q 0.24 4.XR 4.C TltC (SKCI 4%4.50 4.N VW lee V I!t j'WV l I jlj e I~&rv ew fVW g~~~I s e~~~~~\I~~
CD CD CD RELBPS/mO]/
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RKUFS/t$01/014 REACTOR LOSS OF C RA.PRON C.COOK N PORK OP/M/5.
joel f l j~fe J j l l I;I Ie 1(Sl~IP 0 5~~-~5 I re 55 yen 5 O O I m aa scca si~i~ex RQ.APS/t$0l/Old fKRCTOR LOSS OF CMLFN ANR.'JS 5 PROGRRN SE N S S R I 0 CJl~M O W O I QI C)o O.N 0.34 Oo52 0.40 TlnC (SECI 0.55 O.H
~a~t wio*vs~~g f!l'l 0~gnat\IW-4 jv&I A tp t'~l!Cd 4l v~A ClH;J gl J'w~v+~t~V I t l C'r II'I'e g l~W I~~E c~;~c I'I'$I%I)I g ().c (v<" I lrP~pl~wW W M V RELfFS/Cg/01 REACTDR S CMLfS.C.CMK UM I PORV 0//o O SEc.LN A I1 lit%ISECI A 1$
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/RE OR 5 CM%T PRONATE.C.CNK UNtT PORV 0//~K~&sEp O,N O.Ii 0N TltK (SECl t4+C7 C P~t~t>>IC t i~y I 1~I t I t i.grQ RELAPS/INOI/OI4 REACTOR LOSS OF'INLFN ANfl.SIS PROGRAM.3 O.D ill@ISECI
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Qo R IKUPS/NR/Q1<OR OSS DF.t.'.COQK UHITl PORY OPEN//15.o R O/F.pow cz Q sKc LN AN Llk TltK (SKCl S'."3DVP38.-
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*Technical Report TR-5364-1 Revision 0 4-244 A TELEDYNE ENGINEERINQ SERVICES 4.7.3 uarter Model-Cold Loo Seal/Steara Case
~~~I'II Vl Il AI I I I%I,+V W pV ft 5~JE~r'p I I,C JI~JS r E~E, I V'E V A Technical Report A TELEDYNE ENQINEERINQ SERVICES 4-245~g DATE 1/i-88 CHKO.BY CHOATE~pl oQE'g SRv 0 Isa'Hatt.ce g.///g gh/t 7 2 SHEET NO.OF I FROJ.NO$(R'w~~y 4 A'g oog , PQQ~RJIZ'5g 7%OP Vo<one S/0 y~~CPv'os 5 XwE:CE'OE.
OO9 JA'CtW d/0///s'//Q/ce i82n I+3 4 carer 0/f;~orvd L o/s numb II 2$ilail//5'4 I/SPJ~g/g~gol/Ik IJE I/~FIGURE 4.7.2-1 p,Q~~l J)<<~f~~J4-y~.;-'M(R38 Gal).@~YlP~~Tl" t I I t J gn<.t l'Cy I I)fr';C t)la+tl r I'I*I%~fib~~~V All'I ew E CC l i*A lg y fS l QI M t" 5 0'i''I tg l'I P~t CD M CD C 1 0 Vl 2 Vl 0 W 0 I Dl ED Kl CD O I OMIT RELRPS/NSl/0 fKRCTOR LOSS OF'NUS FNR.'fSlS PROCRSl REP UNII2 L NE 5 3/2/05.o~l D OO 8ci CI CD h 0.0 0.2 IltK lSECI 0.4 OA I~4~aa-.g$l a)~t,'g'aQ,Q p~.tacan, III W III (I 0 Vl K Ih CttI O O W 0 I At tD Xl A)'13 O I rt'ELRPS/t$
0/0 fKA OR L S%Rtt 5 PRO RNI UNf I LINE RE 5 83/02/05 o 0+Ho D O III Eg W D 0 n Ct d 0.0 O.R 0,4 O.N
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Latest revision as of 02:23, 24 February 2020

Rev 0 to Books 1-3 of Analysis of Pressurizer Safety/Relief Valves Discharge Piping Sys Per NUREG-0737,II.D.1,Unit 1.
ML17324B003
Person / Time
Site: Cook American Electric Power icon.png
Issue date: 06/06/1983
From:
TELEDYNE ENGINEERING SERVICES
To:
Shared Package
ML17324B004 List:
References
RTR-NUREG-0737, RTR-NUREG-737, TASK-2.D.1, TASK-TM TR-5364-1, TR-5364-1-R, TR-5364-1-R00, NUDOCS 8608060052
Download: ML17324B003 (392)


Text

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~,1 TECHNICAL REPORT TR-5364-1 REVISION 0 BOOK 1 OF 15 DONALD C. COOK NUCLEAR GENERATING PLANT ANALYSIS OP PRESSURIZER SAPBTY/RELKF VALVES DISCHARGE PIPING SYSTEM PER NUREG 073V, ILD.I, UNTF I JUNE 6, 1983

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AMERICAN ELECTRIC POWER SERVICE CORPORATION 2 BROAOWAY NEW YORK, NEW YORK 10004 TECHNICAL REPORT TR-5364-1 REVISION 0 BOOK 1 OF 15 DONALD C. COOK NUCI.EAR GENERATING STATION ANALYSIS OF PRESSURIZER SAFETY/RELIEF VALVES DISCHARGE PIPING SYSTEM PER NUREG 0737, II ~ 0.1, UNIT 1 JUNE 6, 1983 N'TELEDYNE ENGINEERING SERVICES 130 SECOND AVENUE WALTHAM,MASSACHUSETTS 02254 61 7-890-3350

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A TELEDYNE Technical Report ENGINEERINQ SERVICES TR-5364-1 Revision 0 TABLE OF CONTENTS PAGE

1.0 INTRODUCTION

Book 1 of 15

2.0 CONCLUSION

S 2-1 3.0 SYSTEM DESCRIPTION/DISCUSSION 3-1 4.0 THERMAL FLUIDS ANALYSIS 4-1 4.1 Introduction 4-1 4.2 RELAP Model 4 3 4.2.1 Pressurizer Conditions 4-3 4.2.2 Valve Modeling 4-4 4.2.3 Discharge Piping 4-5 4.2.4 quench Tank 4-5 4.3 RELAP Model Control Volumes 4-16 4.4 quarter Model 4-26 4.5 Unit 1 PORV Model 4-'36 4.5. 1 Condensate Modeled Case 4-36 4.5.2 ,PORV Modeled Transient 4-36 4.6 Valve Flow Rate Calculation 4-40 4.6.1 SV Flow Rate 4-41 4.6.2 PORV Flow Rate 4-.42 4.7 RELAP Plots 4-45 4.7.1 Unit 1 - Condensate/Steam Case 4 46 4.7.2 Unit 1 - 400o Solid Liquid Case 4-166 4.7.3 quarter Model - Cold Loop Seal/Steam Case 4-244 4.8 Force Time History Plots Book 2 of 15 4-260 4.8.1 Unit 1 - Condensate/Steam Case 4-261 4.8.2 Unit 1 - 400o Solid Liquid Case 4-320 4.8.3 quarter Model - Cold Loop Seal/Steam Case 4-392 4.9 RELAP Input 4-420 4.9.1 PORV Condensate/Steam 4-421 4.9.2 Condensate/Steam Restart 4-439 4.9.3 PORV Solid 400o Liquid 4-448 4.9.4 PORV Solid 400o Liquid Restart 4-467 4.9.5 SV Cold Loop Seal (quarter Model) 4-472

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)i TELEDYNE Techni ca 1 Report ENQINEERINQ SERVICES TR-5364-1 Revision 0 TABLE OF CONTENTS Continued PAGE 4.10 REP IPE Input 4-478 4.10.1 Unit 1 - Model Section A 4-479 4.10.2 Unit 1 - Model Section B '-489 4.10.3 Unit 2 - (quarter Model) 4-496 4.11 APPENDIX A 5.0 STRUCTURAL ANALYSIS Book 3 of 15 5-1 5.1 Deadweight Analysis 5-2 5.2 Thermal Analysis 5-2 5.3 Seismic Analysis 5-2 5.4 Force/Time History Analysis 5-7 5.4.1 PORV Transient 5-7 5.4.2 SV Transient 5-8 6.0 ANALYTICAL RESULTS 6-1 6.1 Stress Su@nary 6-1 6.1.1 Equation A-1 Stresses 6-6 6.1.2 Equation A-2 Stresses 6-17 6.1.3 Equation B-1 Stresses 6-28 6.1.4 Equation B-2 Stresses 6-39 6.1.5 Equation B-3 Stresses 6-50 6.1.6 Equation C-1 Stresses 6-61 6.2 Support Loads 6-72 6.3 Valve Accelerations 6-105 6.3.1 DBE Seismic Valve Accelerations 6-106 6.3.2 PORV Transient Shock Valve Accelerations 6-110 6.4 Nozzle Loads 6-114 6.5 Valve Loads 6-120 6.6 Miscellaneous Calculations 6-126 6.6.1 Thermal Boundary Displ acements 6-127 6.6.2 OBE Spectra 6-133 6.6.3 DBE Spectra 6-140 7.0 DRAWINGS 7-1

8.0 REFERENCES

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A TELEDYNE Technical Report ENGlNEERINQ SERV(CES TR-5364-1 Revision 0 TABLE OF CONTENTS Continued 9.0 COMPUTER ANALYSIS 9.1 RELAP/REP IPE Input Book 4 of 15 9.2 Deadweight/Thermal Input/Output Book 5 of 15 9.3 OBE Seismic X-Y Input/Output Books 6, 7 of 15 9.4 OBE Seismic Y-Z Input/Output Books 8, 9 of 15 9.5 DBE Seismic X-Y Input/Output Books 10, 11 of 15 9.6 DBE Seismic Y-Z Input/Output Books 12, 13 of 15 9.7 PORV Transient Shock Input Books 14, 15 of 15

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-A-TELEDYNE Technical Report TR-5364-1 ENQlNEERING SERVfCES Revision 0 1.0 . INTRODUCTION American Electric Power Service Corporation {AEP), purchase order number 02676-820-1N, authorized Teledyne Engineering Services (TES) to analyze the Pressurizer Safety/Relief Valve Discharge Piping per NRC NUREG-0737, Item II. D.1, for the Donald C. Cook Nuclear Power Plant, Unit Pl.

This activity was performed in accordance with the TES (}uality Assurance program which meets the requirements of 10CFR50, Appendix B, and ANSI N45.2.11 as interpreted by Regulatory Guide 1.64, Revision 2.

The scope of work for this effort is described in detail in Teledyne Engineering Services Technical Proposal PR-5653 {Reference 1), dated May 4, 1981 and modified as stated in AEP letter dated November 29, 1982, from Mr. Sam Ulan (AEP) to,Mr. L. B. Semprucci (TES) and in AEP letter from Mr. Sam Ulan (AEP) to Mr.

P. D. Harrison (TES) dated March 15, 1983 (References 2 and 3).

The majority of the analysis was performed after the receipt of AEP letters dated November 29, 1982 and March 15, 1983 (References 2 and 3), which were issued after more complete information was available from,the EPRI data.

This analysis was performed using l ar ge di g ital computer programs supplemented with any necessary hand calculations. The RELAP5 MOD1 Cycle 14 computer program was used to do the thermal fluid transient analysis. The structural analysis, for all loading conditions, was done utilizing the TMRSAP computer program.

'he size of the pressuri zer safety/relief valve discharge piping system was so large that the computer models, for both RELAP and TMRSAP, strained the limits of the programs. This condition necessitated multiple RELAP runs in order to execute the thermal fluid transient analysis for the appropriate length of time.

For the structural analysis it was necessary to expand the core of the TMRSAP pr ogram in order to avoid an overconservative overlap analysis.

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r> TELEDYNE Techni cal Report ENGINEERINQ SERVICES TR-5364-1 Revision 0 2-1

2.0 CONCLUSION

S The analysi s performed by TES on the Pres suri zer Saf ety/Rel i ef Val ve Discharge Piping System indicates that all criteria of NRC NUREG-0737, Item II.D.1 is met for normal and upset (PORV discharge) conditions and is not met for the emergency (SV discharge) condition.

Evaluation of normal and upset conditions required structural analysis for deadweight, thermal, OBE seismic, and PORV transient shock loading conditions.

Details of the various loadings considered are provided in Section 5.

Based on preliminary SV thermal hydrodynamic transient analysis, excessive loads and stresses were anticipated and, therefore, it was decided; for economic reasons, that a quarter model SV thermal tr ansient analysis (RELAP5) should be performed to check the adequacy of the system for the emergency condition. In addition, due to the similarities of the Unit 1 and Unit 2 geometries, it was determined that the results of one unit could be considered applicable to the other unit. The quarter model consisted of the piping from the pressurizer, through valve SV-45C, and continuing down to the quench tank, for Unit 2. The SV transient analysis considered only the effect of valve SV-45C opening. The results of the quarter model analysis indicated substantial failure of the entire quarter model geometry. Considering that TES is required to analyze for the simultaneous opening of all thr ee SV valves (Reference 3), which is a more severe loading condition, it is evident that the quarter model analysis is sufficient to prove the failure, for the emergency condition, of both Units 1 and 2.

Therefore, this report for Unit 1 contains no analysis or results for the SV thermal condition or the SV thermal transient shock condition. Results of the SV quarter model analysis performed for Unit 2 are contained in the Unit 2 report, TES Technical Report TR-5364-2 (Reference 6).

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TR-5364-1 Revision 0 2-2 Section 6 contains a stress sumary of all node points, a summary of support loads, valve acceleration calculations, a sumary of pressurizer and quench tank nozzle loads, and a listing of the moments on the end of each valve for all loading conditions. It should be noted that valves NRV-151, NRV-152, NM0-151, NM0-152, NMO-153 are in excess of the veritical acceleration criteria of 2g for the

'nd PORV thermal shock transient condition. These values are considered acceptable per the approval given by AEP in their letter of May 26, 1983 from Mr. Sam Ulan of AEP to Mr. P. D. Harrison of TES (Reference 7).

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-r<-TELEDYNE Techni cal Report ENGINEERING SERV(CES TR-5364-1 Revision 0 3-1 3.0 SYSTEM DESCRIPTION/DISCUSSION The Pressurizer Safety/Relief Valve Discharge Piping consists of all of the piping from the pressurizer nozzles, down to the sparger in the quench tank. This information is depicted on TES drawing E-5763, Revision 2, generated from AEP drawings 1-GRC-6, sheets 1,', 3, 4; 1-GRC-7; 1-GRC-8; and 1-GRC-9.

The "Discharge" piping constitutes a very large system resulting in a large computer model. The size and geometrical complexity, which is due mainly to the sweeping curves around the pressurizer, complicates the modification effort in addition to causing longer run times..

Modification of this complex system, to attempt to secu're satisfactory "Safety Valve Discharge" results, is limited to draining the SV loop seals.

Heating the loop seals is not a viable "fix" because of the size of the loops.

These long loops contain sufficient quantity of water such that on SV Discharge, the water seal does not "flash" completely enough to reduce the very high loads caused by the water slug. Modification to the support system is also a poor option because of the very limited space in the annulus around the pressurizer, which makes construction very difficult.

Another aspect of the system that could be improved is the setting of the constant spring supports. During the data extraction of the deadweight analysis results, it was observed that the supports in the PORV loop area were causing significant upward displacements of the piping system, as detailed'in Section'.2.

The stresses in these regions are high and, although they do not exceed the allowable, they could be r educed by re-adjustment of the spring settings.

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-A TELEDYNE Technical Report TR-5364-1 4-1 ENGINEERING SERVICES Revision 0 4.0 THERMAL FLUIDS ANALYSIS 4.1 Introduction The following analysis determines the fluid forces which act on the pressurizer safety and relief valve discharge piping of the American Electric Power Donald C. Cook Nuclear power Plant, Units 1 and 2. These forces are generated by the sudden opening of the pressurizer safety and relief valves during one or more of the pressurizer transients described in the AEP supplied 1982 letter to TES.

These forces, the resulting stresses they apply to the piping system, the resulting loads they impose on'the pipe supports, and the loads they transmit to the safety and relief valves became of increased concern as a result of the incident at Three Mile Island.

Following the Three Nile Island incident, the NRC issued NUREG 0578 and NUREG 0737 which required that each utility determine the effect of safety/

relief valve operation upon the valve and the discharge piping. An elaborate progr am involving both testing and analysis was established under the general management of the Electric Power Research Institute (EPRI). Intensive testing of safety and ~elief valves was performed at several locations across the country.

A full scale model of the pressurizer and discharge piping was built at Combustion Engineering in Connecticut.'imultaneously, an analytical program was initiated to choose and test a computer program which would predict the fluid forces; RELAP5 MODl was chosen. This is the latest in the family of RELAP programs developed at the Idaho National Fngineer ing Laboratory.

In this analysis, TES has used RELAP5 MOD1 Version 2.11 as it is made available through Control Data Corp with a post-processor, REPIPE version 3.10, which calculates the fluid forces .

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Technical Report 4-2 -ri-TELEDYNE TR-5364-1 ENGlNEERlNG SERVlCES Revision 0 This version. of RELAPS NOD1 is identified by the following computer job control language at Control Data Corporation:

BEGIN, REI AP5, R5N2, INPUT=INPUTFILE, SCM=377000B The computer analysis procedure for the thermal analysis portion is included in Appendix A.

RELAP5 calculates hydrodynamic data for control volumes in each segment of pipe. REPIPE then takes this data and defines two force time histories for a segment. One set of inlet junction forces, the other outlet junction forces.

SAP2SAP adds these force time histories. Finally, one force time history for each segment of axial, unbalanced loads is analyzed structurally.

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>s-TELEOYNE Technical Report ENGlNEERINQ SERVICES TR-5364-1 Revision 0 4.2 RELAP Model 4.2.1 The D.C. Cook pressurizer was modeled as a single time dependent volume with the following transient conditions as specified by the 1-7:

American Electric Power 11/29/82 letter to LBS, pages

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is TELEDYNE Technical Report ENQINEERlNQ SERVICES TR-5364-1 Revision 0 PORV Steam/Condensate Slugs Case 2550 2500 2450 Pressure psi 2400 2350 0.8 2300 0.4 Time (Sec) 1.2 Case 2: Continuous Warm Water = 400oF (Same pressure as PORV, Case 1) 4.2.2 Safety valves and power operated relief valves were modeled as RELAP junctions using the following information:

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PORV Masoneilan 0.00806 Ft2 1.0 Sec NO-38-20721 (Ref. 14)

Valve orifice areas were calculated using the EPRI Safety and Relief Valve Test Report (Reference 16) and RELAP (Run ID BAICDRO) implementing rated flows. Calculated values are included in Section 4.6.1.

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4 5 ]< TELEDYNE Technical Report TR-5364-1 ENGINEERING SERVICES Revision 0 4.2.3 Discharge piping was modeled from all safety and power operated relief valves to the quench tank. This discharge piping included the following pipe sizes:

3 inch, 12 inch SCH 40 4 inch, 6 inch SCH 40S 4 inch SCH 120 3 inch, 6 inch SCH 160 Friction factors for 1.5 D or short radius bends and reducers were taken from technical paper 8410 by Crane. Calculations of these losses and constants are included in Appendix A. Segment lengths used are listed in Figures 4.2.1 and 4.2.2 for both models. The discharge piping defines segments with segments described as straight sections from elbow to elbow, valve to elbow, etc.

Also, a listing of RELAP5 input is included in this report. The SRV model is modeled from one safety valve to the quench tank. This was determined to be an adequate representation of safety discharge piping for both units and will subsequently be referred to as "The Quarter Model". The Quarter Model is modeled utilizing Unit 2's geometry.'.2.4 The Quench Tank was modeled in two parts: the sparger and the tank itself. The Quench Tank is modeled using cylindrical volumes containing water and air. The volume si zes are equal to quench tank volumes provided on Westinghouse Dwg. No. 110E272.

The sparger for D.C. Cook is a perforated pipe submerged in the water within the quench tank as indicated in Figure 4.2.3 of this report. It is represented in RELAP as a pipe equal in volume and similarly submerged.

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4-13 Technical Report Revision 0

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Techni cal Report ]5 TELEDYNE TR-5364-1 ENGINEERING SERVICES Revision 0 4-16 4.3 RELAP Model Control Volumes The Evaluation of RELAP5/MOD1 for Calculation of Safet /Relief Valve Dischar e Pi in H drod namic Loads report prepared by Intermountain Technologies, Inc. recommends using ten or more control volumes per bounded segment while avoiding significant control volume length differences to preserve pressure wave shapes. The ten control volume criteria recommended by ITI was adhered to except in piping arcs and in segments less than three feet in length. The D.C. Cook discharge piping is modeled using as few as one control volume per segment (pipe segments with lengths less than 0.5 feet) and up to thirty-two control volumes per segment.

Arc modeling for both units is represented in Figures 4.3.1 and 4.3.2.

All arcs for Units 1 and 2 were modeled in RELAP as having no fluid losses.

Essentially, RELAP calculates these as straight sections of pipe. J REPIPE, however, distributes the calculated forces to pre-assigned node points matching the TES

~ ~

structural models.

Average control volume lengths used for the D.C. Cook RELAP Units 1 and 2 model were:

Pioe Size Avera e C.V. Len th 3 inch SCH 160 0.4644 feet 6 inch SCH 160 0.5264 feet 4 inch SCH 40S 0.4471 feet 6 inch SCH 40S 0.8614 feet 12 inch SCH 40 0.8064 feet 3 inch SCH 40 0.4744 feet 4 inch SCH 120 0.5056 feet schematic of the discharge systems modeled in RELAP for the PORV

~

A Unit 1 model and the SRV 1/4 model for Unit 2 are given in Figures 4.7.1 and

~

4.7.2, respectively.

~

~ ~ ~

A TlH EDYNE Techni ca 1 Report ENGINEERINQ SERVICES TR-5364-1 Revision 0 4-17 quench Tank modeling was achieved using twenty control volumes and twenty junctions. Eighteen volumes comprise the spar ger model while the remaining two are single volumes modeling the water and air spaces of the quench tank. The water and air volumes as determined from Westinghouse Dwg. No. 110E272 were input to RELAP to insure proper quenching capacity. Eighteen control volumes forming the sparger are initially 88K full of water representing a submerged pipe. The discharge holes were modeled as a single hole of equivalent area at the end of the pipe (a conservative assumption).

Finally, the tank rupture disk is modeled as a pressure actuated valve placed on the air volume and set to blow out at 100 psig discharging to atmosphere.

(Figure 4.2.3 represents the D.C. Cook Units' and 2 quench Tank).

Technical Report 1S-TELEDYNE ENGINEERINQ SERVICES e

BY + DATE ~om<~ Pq Mooel SHEET NO. / <>'S /

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Technical Report Revision 0 A TELEDYNE ENQINEERINQ SERYlCES 4-22 eY <>+ DAve > ~s 4> un i z i waRv sEc.ri o~ SHEET NO. OF s CHKO BY, OATEYT 23 so RE't A'P HobGL. ( D>~<5TPCRM) PROJ. NO. S36 f J

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A TELEDYNE Technical Report ENGINEERING SERVICES TR-5364-1 4-26 Revision 0 4.4 9 N d 1 Before beginning the as-built analysis for the safety valves, it was almost certain that the loads would fail the system. A review of the testing that was done at Combustion Engineering in Connecticut indicated this would be the case. The cold loop seal discharge test at C.E. produced loads of 175 Kips.

The D.C. Cook Units 1 and 2 pressuri zers have three safety valves each with a loop seal larger than the C.E. test facility loop seal. Therefore, it was decided to make a small RELAP model of the D.C. Cook Safety Valve discharge line. This model contains one safety valve (SV45C) including its loop seal piping and its discharge piping through arc level 669'-2" up to, but not including, the quench tank. This model would be less expensive to run than the full three valve model.

The results of this small (quarter Model) confirmed our suspicion that the cold loop seal case would fail. It also allowed us to make a paremetric study of loop seal temperature in loads as is shown below. Only the steam discharge proved to be acceptable, therefore, TES has recomnened to drain the loop seals.

Loop Seal Loop Seal Temperature Position of Valve Opening Max Load Condition oF Loo Seal Time Sec LBF Col d 141o Upstream 0.010 115,000 Col d 141o Downstream 0.010 174,000 Hot 350o Upstream 0.010 156,000 Hot 350o Upstream 0.090 109,000 Hot 350o Upstream 0.130 124,000 Hot (Sat. 650o Upstream 0. 090 38,000, Water )

Steam 650o Upstream 0.010 6,000 The loop seal temperature distribution was calculated to be input to RELAP and is included in the Appendix A. The temperatures used for the cold loop

~ ~

seal r'anged from 584.4o at the pressurizer to 141.1o at the valve.

~

Technical Report TR-5364-l

)q ~LEDYgE EgggEERiNG SERytCES 4-27 BY +~~ OATE~+Z2

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Technical Report Revision 0 A TElEDYNE ENQlNEERINQ SERV(CES 4-32 CHKD. BY ~++ DATE ~

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Technical Report

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Technical Report A TELEDYNE TR-5364-1 4-36 ENGINEERING SERVICES Revision 0 4.5 Unit 1 PORV Model The inlet piping to the PORV's is sloped toward the valves. Therefore, during normal operating conditions a saturated water (condensate) loop seal is formed at the inlet to the PORV.

As specified in American Electric Power's letter of November 29, 1982, referring to PORV transient conditions, the following cases were modeled:

Case Transient Condensate/Steam Discharge 400o Solid Liquid Discharge 4.5.1 The way in which the condensate/steam case loopseal was to be modeled was decided by using two methods on a small sample model.

a~ Low equality Steam Loop Seal (Saturated Conditions)

b. Solid Loop Seal (Saturated Conditions)

A low quality steam loop seal produced oscillatory mass flow rates through the valve. These oscillations were severe enough to cause rejection of this model and to choose the solid condensate case. These oscillations are the result of numerical instabilities in RELAP s choking correlation. This is due to the severe change in sonic velocities in the transition range between subcooled water and steam.

4.5.2 Both cases (loop seal and 400oF solid liquid discharge) were modeled and run on RELAP and REPIPE. The resulting force time histories were compared. It was not clear at this level which case was more severe. Therefore, the force time histories for both cases were input to the structural program. It could then be seen that the 400oF solid water discharge condition was the governing case.

->s-TELEDYNE.

Technical Report ENGINEERINQ SERVICES TR-5364-1 4-37 Revision 0 Both the loop seal and the solid water case exhibited unstable behavior (o'sci Ilations in the flow rate). The loop seal case showed these oscillations in the transition region at the tail end of the loop seal as it passed through the valve. RELAP tends to cause flow rate oscillations because of the severe change in sonic velocities between subcooled water and low quality steam. These flow rate oscillations result in high forces which tend to be overly conservative.

In the 400oF subcooled water case, the reason for the flow rate oscillation was more obscure. At approximately .400 seconds the flow suddenly decreases approximately 30 Ibm/sec in lmsec.

This can be seen in Section 4.7.2. A careful review of the RELAP output did not reveal a good physical reason for such behavior. Reasons for such behavior could be

1. A sudden reduction l

in the valve area vs. time data.

2. A build up of back pressure in the discharge line which will cause the valve flow rate to'uddenly decrease..
3. A sudden decrease in pressure in the pressurizer boundary condition which would result in reduced-flow.

All these things were checked to see if they were possible sources of the flow rate fluctuation. But the review indicated that they were not the source of the problem.

r< TELEDYNE Technical Report TR-5364-1 4-38 ENGlNEERING SERVlcES Revision 0 A partial tabulation of this review is shown below:

UNIT I Valve Junction

¹410 Cont. Yol. Cont. Vol. Reference 41101 40926 RELAP Run BHFRFGG Unit. 1 200-600 msec So 1 i d low Red Junction Cont. Yol. Cont. Vol. Cont. Vol.

¹410 ¹40926 ¹41101 ¹40926

. Time

.408

.409 Flow 111.18 83.424 0.0 0.0 p

248.89 245.55 p

2342.8 3058.

It can be seen that the downstream pressure does not exhibit a sudden increase that would reduce the flow through the valve. The upstream quality remains zero so that the flow through the valve is subcooled.

The pressure increases upstream which corresponds to a sudden reduction in flow area. However, the flow area increases it does not decrease.

The pressurizer time dependent volume does not exhibit any sudden change in pressure which would correspond to this flow change.

Past experience with the RELAP programs has shown problems with subcooled water and low quality steam flow. These problems have manifested themselves as severe oscillations in the flow rate. It is our opinion that the results from the RELAP run are highly conservative and overpredict the fluid forces.

Technical Report A TELEDYNE TR-5364-1 ENGlNEERlNQ SERVlCES Revision 0 4-39 Mhen the fluid forces from this RELAP run are combined with the seismic, deadweight, and thermal expansion loads, the allowables were slighlty exceeded. Since the principal fluid loads appear to be a result of an instability in the flow rate predicted by RELAP and not a result of an actual physical phenomena, it was decided that these loads were overly conservative and could justifiably be reduced by 20K. 'he fluid forces presented in Section 4.8 and elsewhere in Section 4.0 are the as calculated loads and have not been reduced by 2(C.

It should be noted that an alternative modeling practice that could have been employed in the solution of this problem would have been to make the PORV valves time dependent junctions and specify the valve flow rate. Had this been done, the flow rate oscillation and their resulting forces would never have occurred,

ri-TELEOYNE ENGINEERING SERVICES Techni,cal Report 4-40 TR-5364-1 Revision 0 4.6 Valve Flow Rate Calculation TES Flow Max Rating*

Rate Calculated For Steam Bore Area Opening Valve T e LBM/HR 9 3X Accom. ~IN~ Time Sec C~ros b 523,332 435,000 3.6 in2 0.010 Safety Relief (Ref. 18)

Val ve Masoneilan 199,000 1.0 Op d (Ref. 16)

Relief Valve

  • The maximum rating for steam at 3X accumulation value is from the Crosby Valve J

and Gage Safety Valve Drawing No. H-51688, Revision A.

Technical Report

]i TELEDYNE TR-5634-1 ENQINEERINQ SERVICES Revision 0 4-41

,= 4.6.1 The valve flow rates used in RELAP analysis of the SRVs were obtained by increasing the ASME rated flow by 15K; l(C to consider the ASME underating of the theoretical flow and 5X to cover tolerances. TES flow rate calculations are included in Figure 4.6.1.

WT = 51.5 AP ASME rated flow:

WR

= 51.5A (1.03P + 14.7)(.9)(.975)C (Ref. 17) where:

WT = theoretical flow WR

= rated flow coefficients:

1.03 - applies 3X accumulation 0.975 - valve flow coefficient 0.9 - represents theoretical flow rate reduced 1(C to equal ASME rating The equation TES uses to calculate the valve flow rate is Wmax = 1.05 x 51.5A (1.03P + 14.7)C(0.975)

This is an increase of 15K above the ASME rated flow as explained above.

-ri-TELEDYNE ENGINEERING SERVICES Technical Report 4-42 TR-5364-1 Revision 0 4.6.2 The Masoneilan PORV maximum flow rate for steam was taken from the EPRI Safet and Relief Valve Test Re ort as 199,000 ibm/hr (Table 4.5.1-1b).

A valve opening time of 1.0 seconds is used based on total valve opening times of all Masoneilan valves tested listed in Table 4.5.2-1. Since full open times averaged 2.76 seconds, with a minimum value of 1.64 seconds, TES has assumed 10(C opening in 1.0 second, because independent testing has shown that flow is not always directly proportional to stem travel. Most often full flow is obtained before full stem travel. 8ecause 1 second is a very long opening time, this was not considered overly conservative.

Technical Report Revision 0 )<~TELEDYNE ENQlNEERlNQ SERVICES 4-43 sv CHKD. BY~f~DATE~~

DATE~~jh C~SY Yam( V'A 4-VG SHEET NO. ~OT 2 PROJ. NO.

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Fig.4.6.1-1

Technical Report Revision 0 A TELEDYNE ENGINEERING SERVICES 4-44 CQciwel'~> HO.~OF CHKD. BY ~DATE~ rhea ~ @km vA<YE'~p~

GA~LA~

SHEET PROJ. NO.

2 S<

id, SZ S,g'/o.OS fQ/ r hr = /'/S, 37 ~/oec THE'ornrTvTEiz 'Qoor BA z~p

'roloe. foll efoen cree in /he ron iw+cK) 0 o&z. t+

iloo rc,4e. Q C il ofen'g - ISO.if /~c R~ ro/e. C? goto oo~;~ of/l.e I

~l E. ~ /Sa oi +l~c.

RCLAPS floso c'eo 'i'oh etLuErw lrilesx )E/S B7 ~l~e(

Col& 4eO8 bif inWfool;*ion, IQb y7- 138.DI AAoo = o. / T o / /.o rg (o coed)

O Q2.M 4>

( v)

O.OO8O( 4/ (R ev)

Fig.4.6.1-2

-A TELEDYNE Techni cal Report 4-45 ENGINEERINQ SERVICES TR-5364-1 Revision 0 4.7 RELAP Plots The following plots represent RELAP mass flows, pressures and qualities at various points along the discharge piping. Since RELAP had to be restarted, the plot time scales may vary (i.e. 0.0 - 0.2 seconds or 0.0 - 0.400 seconds). Also, the ordinate axis may not always be correct; many times multipliers will be off (COC is aware of this problem in RELAP). However, they do depict the trend accurately and are calculated and reported in RELAP every .0.001 seconds.

Correct peaks and times at which they occur are listed with each trace.

Plot Set Tr ansi ent 4.7.1 Unit 1 Condensate/Steam Case 4.7.2 Unit 1 400o Solid Liquid Case 4.7.3 quarter Model Cold Loop Seal/Steam Case A RELAP volume schemati c precedes each plot set.

Technical Report

]i TELEOYNE TR-5364-1 ENGINEERING SERVICES Revision 0 4-46 4.7.1 Unit 1 - Condensate/Steam Case

Technical RepA TcLEOYN- ENGILD ~tViNG S RVIC~S TR-5364-1 Revision 0 I

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gb(bl FIGURE 4.7. 1-1

<s-TEt EDYNE ENGIN:-ERlNQ SERVICES

,, 4-4,8 BATEMO'87 WEAP /10DEl 9 cd PfAYz'c SHEET NO.. QS~

HKD. BY ~+OATE~EE 5 u~- 1 ~)Pi~ <WC S PROJ. NO. ~+

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~rosi FIGURE 4.7.1-2

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BY~~DATE~5A P P ODEUM SCgrPN'7&C SHEET NO..

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