ML20339A035

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9 to Updated Final Safety Analysis Report, Chapter 5, Reactor Coolant System and Connected Systems, Figures
ML20339A035
Person / Time
Site: Ginna Constellation icon.png
Issue date: 11/20/2020
From:
Exelon Generation Co
To:
Office of Nuclear Reactor Regulation
Shared Package
ML20339A309 List: ... further results
References
Download: ML20339A035 (20)


Text

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.2-1 Figure DELETED Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.2-2 Figure DELETED Figure Deleted Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.2-3 Reactor Coolant Leak Detection Sensitivity METHOD I* SENSITIVITY REACTOR COOLANT ACTIVITY Xe-138 = (l.04 µCi/cc Kr-88 = 0.01 µCi/cc LEAK DETECTION TIME (FOR MAXIMUM CIRCULATION IN CONTAINMENT)

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- CONTROL ROD ~ECH. HOUSING CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS WESTINGHOOSE REQUJREH( NTS SHOWN ALL OTHER REQUI REMENTS OE TAIL J TO BE DETERIHNEO BY VESSEL VENDOR (37) REQUIRED.

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DETAIL OF VESSEL KEYWAY (4) REQ'D i- "

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CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS C - 180" & 90° - 270° crnTERLINE OF C - 180° & 90* - 270° KEYWAYS CHAil S MUST PASS THRU OR W[THI" .002 OF THE SAFETY INJECTION NOZZLE THEORETICAL VESSEL CENTERUNE WELD PREPARATION crnTERLlNE OF 90' -270° HYWAYS HUST BE PERPEND[CULAR TO THE CENTERLINE OF THE O' - 100' KEYWAYS W[TH[H . 001/FT NOTES:

I. TOTAL CONCENTRICITY (TOTAL JNOICATOR READING) TO BE EQUAL TO LESS THAN KI.LF OF TOTAL TOLERANCE OF DIAMETERS IN TI-ERl<IAL SHIHD REGION

2. ALL DIMENSIONS ARE RELATED TO A ROCtlEnUt GAi A.ND ELECTRIC CORPORATION TEMPERATURE Of 68°F R.l. OINNA NUCLEAR POWER Pl.ANT 3, SHELL COURSE TOLERANCE I N THE THfRl<IAL SHIELD REGION SHALL BE ~ OPDATlD FO~A.L SAFETY A'IALYILI- RDOIIJT SECTION T- T D~CASEl I Figure 5- l-l. Sheet. 2 l OVALITY CASE 2 Oz Dz FLATNESS Rea<: tor Vessel Scheut.ic:

o1 MINUS o & .005 < 0 FOR CASE I 3 2 2 1 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.3-2 Identification and Location of Beltline Region Material

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ROCHESTER GAS AND ELECTRIC CORPORATION R. E. GINNA N UCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYS IS REPORT Fig u re 5 . 3- 2 Identification a nd Locat i on of Beltline Re g i on ~a teria l REV 7 12/91 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.3-3 Arrangement of Surveillance Capsules in the Reactor Vessel 270° R (3.37 p

SHIELD N

CAPSULE (TYPICAL)

(1. 79 )

( 1. 94) 90° V (3.37)

NOTES:

1. Lead Factors for the capsules are shown in parentheses.
2. In chronological order, capsules V, R, T, S, and N were removed. Ref. Sections 5.3.3.2 and 5.3.3.3.

Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-1 Reactor Coolant Pump MOTOR SHAFT MOTOR ITATOR----

MOTOR SUPP OR 1 IIAND COOLING WAH MAIN FLANGE l

PUMP SHAFT

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- COOLING WAllR OUTLET 1

THERMAL BARRIER _ _ _ _ DIFFUSER IMPELUR - - CASING ADAPTOR DISCHARGE NOZZLE - - - - - CASIN<i ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT Figure 5 . 4-1 React or Coolant Pump Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-2 Reactor Coolant Pump Estimated Performance Characteristics

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0 0 10 zo 30 40 50 60 70 80 90 100 110 FLOW - THOUSANDS OF GALLONS PER MINUTE ROCHESTER GAS ANO ELECTRIC CORl'ORATION R.E. GINNA NUCLEAR l'OWER PLANT Uf'OATEO FINAL SAFETY ANALYS.S REl'ORT F i gure 5.4- 2 Reactor Coolant P ump Estimated Performance Character i st i cs Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-2a Reactor Coolant Pump Composite Curve, Calculated Hot Performance, Total Head and Hydraulic Efficiency Versus Flow TOTAL HEAD-FT HYDRAULIC EFFICIENCY- %

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0 10 20 30 40 50 60 70 80 90 100 110 120 FLOW (X1000) - GPM IMP. SIN 1619/340 Qdeaign

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  • 252 FT ROCHESTER GAS AND ELECTRIC CORPORATION R.E . GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT Figure 5.4-2a Reactor Coolant Pump Composite Curve, Calculated Hot Performance, Total Head and Hydraulic Efficiency Versus Flow REV. 13-1 7/96 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-2b Reactor Coolant Pump Composite Curve, Calculated Hot Performance, Brake Horsepower Versus Flow BRAKE HORSEPOWER 6000  ! 6000 I

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  • 90000 GPM ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT Figure 5. 4-Zb Reactor Coola nt Pump Composite Curve, Calculated Hot Performance , Break Hors epower Versus Flow REV. 13-1 7/96 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-2c Reactor Coolant Pump Composite Curve, Calculated Cold Performance, Total Head and Hydraulic Efficiency Versus Flow TOTAL HEAD -FT HYDRAULIC EFFIC IENC Y--.

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  • 10000 8PM ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY .ANALYS IS REPORT Figure 5.4-2c Reacto r Coolan t Pump Compos ite Curve, Cal culated Cold Perfo rmance , Total Head and Hydrau lic Efficie ncy Versus Flow REV. 13- 1 7/96 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-2d Reactor Coolant Pump Composite Curve, Calculated Cold Performance, Brake Horsepower Versus Flow BRAKE HORSEPOWER 8000 8000 7600 - '

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  • 80000 GPM ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT Figure 5. 4 - 2d Reactor Coolant Purnp Composite Curve, Calculated Cold Performanc e, Brake Horsepower Versus Flow REV. 13-1 7/96 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-3 Reactor Coolant Pressure Shaft Seal Arrangement Figure 5.4-3 Reactor Coolant Pressure Shaft Seal Arrangement l ~OTOR SEALING SURFACE NO. 3 TO REACTOR t==:Jr=~- RltlG CLAMP

- - - - - + - t - - NO. 3 SEAL RUNNER COOLANT -

DRAI N TANK NO. 2 SEAL HOUSING NO. 2 SEAL SPACER TO SEAL WATER HEAT EXCHANGER NO. 2 SEAL RI NG ASSEMBLY SEALI NG SURFACE uo. 2

--;;;;;;;;;;;;;;;..f--i:

.,_--+-t-- NO. 2 RUNNER NO. I RUNNER RETAI NER SLEEVE L---i+/---t-- MODIFIED NO. 1 SEAL t;: RING INSERT WITH

~ SHUTDOWN SEAL (SDS) f-iJ~--__::'-'1 r- ASSE~BLY

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NO. I SEAL RING NO . I SEAL RUNNER ASSEMBLY SEALI NG SURFACE NO. I t l MPHLER PARAMETERS AOCHISffR QAI AND EL ECTRIC COR,ORATION IrlLET SEAL PRESS (ps f a) FLOW RATE A.I. OINNA NUCLIAA fl'OW I R !'LANT

~no FINAL WETY ANALYSIS REPORT NO. 1 '\,2250 "'3. gpm Fi g-ure 5. 4- 3

, .50

.l NO. 2 110. 3 'l,j 8

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  • '1.100 cm' / hr Resctor Coo lant Pressuce Sha!t Seal Ar range men t REV 3 4/19 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-4 Reactor Coolant Pump Flywheel 75 .75 in .

I*

J_ 7.25 in.

T 4.45 in.

1 65 i n. T BORE OF ~8- 3/8 in . DIAMETER WITH 3 KEYWAYS "0CHEITER GAi AND ELECTRIC COflP'ORATION R.E. GINNA NUCLEAR POWtR ,LANT UflOATED FINAL SAFETY ANAL VIII REl'OAT Figure 5. 4- 4 Reactor Cool ant Pump Flywheel Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-5 Reactor Coolant Pump Flywheel Primary Stress at Operating Speed 24 22 FLYWHEEL 0. D. 75 in .

20 18

.., 16 TANGENTIAL STRESS VERSUS FLYWHE EL RADIUS a

X 14 V) a.

12 1500 rpm - 0VERSPEED V)

V) w 10

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SHAFT

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2 0

6 8 10 12 14 16 18 20 22 2, 26 28 30 32 31 36

' RADIUS (in . )

ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT Figure 5 . 4-5 Reactor Coolant Pump Flywheel Primary Stress at Ope r ating Speed Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-6 Replacement Steam Generator STEAM OUTLET NOZZLE WI TH ------------ MANWAY (l)

FLO\.l RESTRICTOR ~

DECK LUGS(6) SECONDARY SEPARATOR PRIMARY SEPARATOR LIFTING TRUNNIONS STEAM ORUM (UPPER) SHELL R£CIROJLATION NOZZLE FEEOWATER NOiZLE FEEO\.IATER HEADER CONICAL TRANSITION S£CTICVII F.U.R. ASSEMBLY INSPECTION PORTS (14)

HANOHOLES (2 IN CONE)

LATTICE GRID ASSEMBLY LOWER SHELL LOWER HANOHDLES(4)

SHELL OR1'1N(l) 6L0\.100WN NOZZLE(2 PRIMARY HEAD PRIMARY NOZZLE~ (2)

ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT rigure 5. 4-6 Replacement Steam Generator REV. 13-1 7/96 Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-7 Figure DELETED Figure Deleted Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-8 Pressurizer t - - - - - - - - S P R A Y NOZZLE

,-----SAFETY NOZZLE UPPER HEAD INSTRUMENTATION NOZZLE REL IEF NOZZLE

' LIFTING TRUNNION SHELL HEATER SUPPORT PLATE I NSTRUMENTATION NOZZLE LOWER HEAD ELECTRICAL

( HEATER ROCHESTER GAS AND ELECTRIC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SAFETY ANALYSIS REPORT

. . . _ - - - - - - - S U R G E NOZZLE Figure 5. 4-8 Pressurizer Revision 29 11/2020

GINNA/UFSAR CHAPTER 5 REACTOR COOLANT SYSTEM AND CONNECTED SYSTEMS Figure 5.4-9 Pressurizer Relief Tank PRESSURIZER SAFETY AND RELIEF VALV E DISCHARGE NITROGEN VENT DEMINERALIZED _,/ MANWAY A~~s7 CONNECTION\ CONNECTION SPRAY WATER / SAFETY HE' l [

PERFORATED DISTRIBUTION HEADER LEVEL GUAGE TEMPERATURE CONNECTION CONNECTION ROCHESTER GAS AND ELECTR IC CORPORATION R.E. GINNA NUCLEAR POWER PLANT UPDATED FINAL SA FETY ANALYSIS REPORT Figure 5.4-9 Pressurizer Relief Tank Revision 29 11/2020