ML17324B003
| ML17324B003 | |
| Person / Time | |
|---|---|
| Site: | Cook  |
| 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
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
1.0 INTRODUCTION
2.0 CONCLUSION
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/.Ag,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
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
~I 1I" l l I C I~I!
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
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).
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.
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).
~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.
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.
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.
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.
Finally, one force time history for each segment of axial, unbalanced loads is analyzed structurally.
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)
" ('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.
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.
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/IS IC64-1)<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"ifÃnJC//~/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.
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.
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.
bN-'4o" SHEET NO.OF 8 FIGURE 4.3.2-2 3'ElAPX 61oDEl oF AIC D ELE'LfA 7/OAJ 4 r'V-IO (AA'C 2)vA ave/Mg.yb'I I gc I~c (N E&C 55/(OS V-~y'e.///8 ,/g+IA E"/, g/hg\pyqp~Bosch-'<+PzwAEA'8-.QgP/+PAL N/g~/Qg/~7~=ran'/rC//(rtZ/JOZZS aiwzu-i'z rivzzu@oars uz~e.~x r coxes~pe)~u)z AdC'PC//hS.
Technical Report TELEDYNE ENGlNEERlNG SERVlCES 4-21 BY DATE~~8~CHKD.BY SC DATE~>i~3 v.C.COO/C, UQI 7 Agg~C~ECbtSZg'/pa aLgg g Q'-'5" SHEET ND.DF 5'IGURE 4~3~2-3 W<~/="L/N e/fee.,e Z~~VA 77iOrV-'-~" (A/CZ)w lg)./L y ceca 8"c ,~s j QT j/T N C')~I g'l/V', j I'i a C654'~F gg/z>>=c//~e P//I/8J~/'c../:,'/JE P~~/AA'A e: dggg~g=,y~//Jo/cn7~srtuCruZAL 4ODFS g//I/r+c/PQ 9E 7 fg/=l'hJ Qg~lg>grjP+Ec'c-pJ7'QHZ="/30pJ/
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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)
SHEET NO.OF s PROJ.NO.S36 f FIGURE 4.3.2-4 Osso Os2s/o~.2%II S'+I O>><IIII'Osss D qll>I pl3 oi~6'SAGE Osoo OIo'2'o.g23', (p~gb 2 O I rt\+3ZAI3 O3 PA O335 F Technical Report TR-5364-l Revision 0 E ENQNEERINQ SERVlCES 4-23 Y OATEN~ciHKD.8Y~+DATE~Z~S r7iec~@4's's" SHEET NO.OF 5 5'IGURE 4.3.2-5 (o a~yoga(o, 0
Technical Report SHEET NO.OF/vM~'r)HA>hl AP.C, cosh)CcTI DP 5 p~A,McHCS+T'E'E.S BY~~DATE~><"~~CHKD.BY+DATE~~~~Remi s i on P]l TELEDYNE ENGINEERING SERVICES 4-24 FIGURE 4.3.3-1 7~SAIC'.f4h/
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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~)
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.
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
@~i p ir ALUrD fr auwS I~a~c u~8 zr~SHEET NO.~OF tS Vii V~8'C r7+Qd q 12'w F=-yO S r B (I W I)PvP&c d.giga Cr g,/0)3~-F f/i,=(H&>8-W p'IZ p)r-r o&r<izorTEA=F'ros (s.FAYEE wr')(v'.ESE, rr r (+SBErr-AT.EFTErr))
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<<Ãr~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
$QRQ[CQ$4-34 CHKO.ST~++OSTE~K~
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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)
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.
Technical Report TR-5364-1 Revision 0 4-37->s-TELEDYNE.
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.
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 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..
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.
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 Junction¹410 Cont.Yol.41101 Cont.Vol.40926 Reference RELAP Run BHFRFGG low Unit.1 200-600 msec So 1 i d Red.Time.408.409 Junction¹410 Flow 111.18 83.424 Cont.Yol.¹40926 0.0 0.0 Cont.Vol.¹41101 p 248.89 245.55 Cont.Vol.¹40926 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 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.
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.
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:
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
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).
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 DATE~~jh CHKD.BY~f~DATE~~
C~SY Yam(V'A 4-VG Q~~~~gag pLoW AQ~Ct0~7pcrA SHEET NO.~OT 2 PROJ.NO.r P~a-aec.77l h'-7.P3.j, I ar8 r7 8.7>>7 2 (r78<)~4,&de/'B.BP-8f iraluc grcur g~ic.h'Sl(c88 4).A Cc puler-P~&TCDQ CixxoexY~t Qclua rr7cnufcctu rr CPS+.SY Vclua c Ceca@.Cc pc p gc,)lo 8 N4 ag 2~:a'o~A.PICC Je~in~Qx'pl~~t pili f'IChheeeC
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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
'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.
Technical Report TR-5364-1 Revision 0 4-46]i TELEOYNE ENGINEERING SERVICES 4.7.1 Unit 1-Condensate/Steam Case
Technical RepA TcLEOYN-ENGILD~tViNG S RVIC~S TR-5364-1 Revision 0 BY~~D*TE t CHKD.BY~CHOATE~HZ~8P WoDZC Sclsm~re.~wZr g SoSu'elE1 I ,SHEET NO.~OF~PROJ.NO.~~prRv'5l gl gaol~2 o qo WIIIP~I>'i--S<i/oy O'jo d<gb(bl , FIGURE 4.7.1-1 SHEET NO..QS~PROJ.NO.~+WEAP/10DEl 9 cd PfAYz'c u~-1~)Pi~<WC S HKD.BY~+OATE~EE 5 3d$0/Og ,,<s-TEt EDYNE ENGIN:-ERlNQ SERVICES 4-4,8 BATEMO'87 Aiy/EO<,o4 e o/LP P w oK'Y~CTM V oP/4//5rg'~ESQ gP f0 tO3>EI ni/A vcZ~nEES V~/////9 ffEEi if'oo~'gi2t Qadi t.S~rosi'FIGURE 4.7.1-2
"'""'"'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>.
tu C>C)M tA+D 8 8 m O+4 K ei'.DD 0.1R 0.15 TltK (5CCl tycho<'/~O.IQB SiC Xl W W tb M fD (I O Vl V t/l 0 WO I X7 ID a O lTl Q (0 0 M (D I Vl C)
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 CDÃ7 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.%
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 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$01/014 LOSS OF CNL O.C.MX UN T PGRV 83//Cl Kl O CI r4 O.N O.N L ll T1tK tSEC)
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REUFS/NR1/014 fKACTN LOS.C.GXK UN PORV LR'll TltK (5ECl REl.fit'5/l13OI/014 REAOIOR LOSS OF O I.ISIT ROIS.ISIS PRORRRII D.~gag a.Zua SSC" OD o tll D D D CIS Kl CIS I 0 Ul Z C/I CrJ N 0 440 I CD Kl CD O 5%m d O.ID D.iI O.JD 0.%TltK tSECl 0.$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]
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]
REACfN OF SA.5l5 PRQGRAtl D.C.mt'NIT1 PORV OPEN/M/5.La L l1 IltK lSECI L10 O CD I I rn rn ted I5~1LLL 5C II~RELAPS/NO/Ol REACTOR LOSS OF COOLfST SA.YStS PROGRAM~)cI n D Q Bo 8 III I<CL d P ID W CI)(I rl Ul Y Ul CA>P 0 A O I Ql CD I a o rI'O.I0 O.R 0.40 TilC tSECl 0.54 O.H C3 REUFS/NR/0]REACIOR LOSS OF O.C.COOK LN V EN//5 C)D O D Q 0 Bd Vl ar tO O CD M CD n CJl~'N 4)D 0 w n I Ql C)Kl CD O mz Sm OoH Lle Ll2 0 li l]lK tSEC)
$i O O Pl RE1 RPSlt$01!Old RCACNR LOSS OF CKlhfW YSfS PR06RSt o I CO CD~CD I Cl Vl~N (p)g Ch~0 W A I QI o X7 CD'a O d.O.I0 0.14 0.32 o.e TltK fSKl 0.%o.se-0.H
CD CD CD rn IKLAPS/%0l/Old RE OR OF SA.S PR06RNl.C.COOK UHlll PORV OPEN/N/I lO n Vl K Vl 0 W 0 I Al CD K7 Ib el ID LOI O.D YllC (SECl
<<<<a<<<<~a CD O Dl Pl RELAP5/N01/014 REACTOR LOSS OF'OOLFNT FFHFl.'YSI5 PR06RAN I h3 CD CD Ul CL a AIMS CD M (b Cl CA M Vl O CsO I CD O-59$spc-O.II 0.'Q o.a TttK lSEC)0.%O.N
IKLJF5/t801/014 RGEIOR LOS OF SFL S S PRONA O.C.COOK Nl PNV OP//5.9y'<)2+49.oswscc La L l1 T]%tSECl L li RELAPS/N)Dl/014 REACtOR LOSS OF CNM.RJT RNA'ISIS PROGRAtl.CAP~ZOO 0 C/099-'/S.s895
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RELAPS/t$01/0 I 0 IK S C.COOK UHIT P V OPEN//lS RON 4 8/ooo-zoo&c I M C).58.oz8'saic CD M (D I 0 Ol~Vl GJ~O W O m Im All T]tK lSECI 0.24
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 OlÃ7 W W fb Kl A)I 0~E IS CD P1 Im O.Il TIE ISECl Z/Spy'Zoo SEC D.R4
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 O.IS O.R 0.32 Oa 40 O.SS TltK lRC)
O O I I rn aaaa ua.a m a~RELAP5/NS1/014 REACTOR LO 5 O.C.COOK lN T PORV OPEN 83//15.SIS PRONOUN.ooo o MSkC O 0 X7 4 4 fD M A)I 0.9'o/6j Q O M<d 4a LQ TltK ISECl 411 RG.RPSINl01/Old RERCTOR l.OSS OF CmlLfWF SA.S S PROCRN}I C)CD Xl W M ID M Al C I 0 CJl 3 VI Gd M 0 W A Pl Sm 0.24 0.%TltK tSEC)O.H C)O 0 REUFS/NS 1/0]0 REACTOR O'QXW CD K7 CD C I A~.CJl~0 A 0 I Ql C)K7 CD O LQ LN liter lSEC)
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~
n ca Z C 7C CD CD CD m m REUFS/NS/Ol REACTOR L05 D.C,IK UNl VOP//l.0000~oo SEC.$8gCP OI O SSC..K7 M I Kl I Vl V)CJl O I CD Kl II)a O 5 rt o.a O.Q TllK tMX:l 8 JW~
RQ.APS/NDl/0]l fKRCTOR l.OSS OF CMLSJT RHFl.SIS PROGRAM.O.l<LR 0.40 Lib TlNC tSEC)0.'%
I~I I I I I II t/r I~I'I C)O O I Pl Pl~~lKUFS/F01/014 REACTOR LD S C NR.S PR fN O.C.COOK UH T V N M//1.(Bj.o4.+pic.Kl M tD I~.Ol Vl Ch 0 I LH.2/ZPZ.2'mac OM Oe QE
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ID o o foal%St~l1.lLV~N W IM RD.APS/F601/Old RERCTOR LOSS GF COOLl%l'NR.YSlS PROGRNt Yl D Ul~~O 0 8 O.LI O.il 0.%0.%TltK (SECl 0.%0.50
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~~l' CD CD m m Q o I ri g IKLAPS/NSl/Ol REACTOR LOSS COOL fSR.lS PR Nl C.CNK UH Tl PORV OP%//5.C7 O r4 o Z 0 hj~O IO IL CbÃ7 CD I 0 M CrJ W 0 W O dO a 0 Q*C.'.0!AN AII tltK tSKCI v J~I~
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fKACIOR LOSS Of CN)L QA.1SlS PROGRAt1 I PO C)/5 5.~~zdo$<c%7 W W CDÃI CD I 0 Vl K III GJ A R~0 W 0 I QI C)Pl Im O.Q 0.40 TltK lSECl 0.5b O.M 4~4' mmsmo]io]mcrw ioss or S D.C.CGX UHl PORY OP//5.L 4.Q Lll T]lC (SEC)K7 M M ID Kl A)n Vl&M 4)Z 0 WO I Cu tDm-:Sm g V)
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O CD m m lKUFS/NR I/014 RE OR I.S T IS 4 Pv Q D~Q X~.C.COOK UNIT P RIt PEN//5.~O Pi Xa
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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]/
l W S or.C.CKK UHlll PORV OPEN//5 VS<5 P 8tl~E i Vl 40+~e O W O I Ql CD X7 CD o 5 o a OWC I.a Oo IQ TltK (SECl P aa V>>taV f<">>h q C.I~PP P L jLI 0 ga vr~P 4L r~~'>>~~r)~~LP~LP~VVL~LP 1~I~PL*I*~~P P~'L'P'L Rl.lR.SR~RO ft/RL 1RRR O O Pl RELBPS/t60t/Ot4 REOCIOR LOSS OF CmtLff/1 tR/fLISfS~PRO RRtl Qo zS o ao szc O.ll O.Q O.R 0.4)TltK (SEC)0.4b D.Sl IQ t A Q)y j mtp jc>M~t=~~U'5)J'I@tent~~)
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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