ML20004E243

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Forwards Acceptance Review Copy of Fsar,Previously Submitted on 810331
ML20004E243
Person / Time
Site: Catawba  Duke Energy icon.png
Issue date: 06/08/1981
From: Thies A
DUKE POWER CO.
To:
Office of Nuclear Reactor Regulation
References
NUDOCS 8106110388
Download: ML20004E243 (3)
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Text

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1 SARGENT & LUNDY E N G1N E E R S CHICAGO Proj. No.: 4391-00/4683-00 Acc. No.: EMD-019178 Calc. No.: 1FW-04 Rev.: 04 Date: 7-17-80 ( Page 2 of 19 SIGNATURE PAGE / ) D / _DATE: PREPARED BY: { .i, J. Feb "M S'O ' M DATE: REVIEWED BY: a [b n A ~~ Prasad R.- /0 0 3.

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DATE: _ APPROVED BY: / B. Tat 6sian / k_ .L P00R ORIGINAL 2 THIS ANALYSIS SUPERSEDES: h REV.: 03 DATE: /.,.-K -?$ ACC NO.: EMD- 005C21 2 l,l l !} \\.(; I' l ( i

SARGENT & LUNDY E N GIN E E R S C HIC #.C O Proj. No.: 4391-00/4683-00 I Acc. No.: EMD-019178 Calc. No.: 1FW-04 ( Rev.: 04 Date: 7-17-80 Page 3 of 19 1 .e t ~-h-TABLE OF CONTENTS s Part I - To Be Filmed Page 1 I 1. Title Page....................................... 2 2. Signature Page................................... 3. Table of Contents................................ 3 3 h 4. Subsystem Documentation.......................... 4 5. Analyses Performed............................... 5 ?' 6. Checklist........................................ 6-11 7. General Notes.................................... 12-13 14 8. Subsystem Plot................................... 9. Analytical Drawing............................... 15-18 10. Equipment Nozzle Reactions and Allowables........ 19 11. Miscellaneous.................................... = 12. Calculations..................................... l. Part II - Do Not Film Check 1. Combined Reactions j a. Input........................................ E) b. Max. Combined Anchor / Valve-End Reactions..... [3 c. Max. Rigid Restraint Loads................... E) $f d. Thermal Mvt. At The Nodes.................... g e. Spring Hanger Data........................... g f. Hydraulic Snubber Data....................... g !i ,,I 2. Miscellaneous ~ Welded Attachment Calculations..................... ( l* ! s I' ' t i i. i !4 I i Part III i '] Computer Output Microfiche (COM) t Includes " Analyses Performed" as listed in'Part I/Page 5 Number of COM cards 2 f 4

r SARGENT & LUNDY E N GIN E E R S CHICAGD Proj. No.s4391-00/4603-00 ~ Acc. No.: EMD- 019178 Calc..No.: 1FW-04 ( Rev.: 04 Dato: 7-17-80 Page 4 of 19 SUBSYSTEM DOCUMENTATION Feedwater 1FN-04 System: Subsystem: B Seismic X Yes No Piping Classification Group: X Initial Formal Certified Analysis \\ REFERENCES 1. Certified System Design Spec.: No.: Rev.: Date: 1FW-04 Rev.: O/!. Date: ? ~/- ?C) 2. Anal. Drawing: No.: 3. P&ID Drawings: No.: See analytical 'Rev.: Date: 4. Equip. Spec.: No.: Rev.: Date: a 5. Seismic Information: Stm. Gen. Feedwater Nozzle-OBE(WO-NS,VR,EW) Cont. Bldg. El. 399 Stm. Gen. Support (205-OB-NS,EW,204-OB-VS) Cont. Bldg. El. 394 Outer Wall (201-OB-NS,VW,EW) 6. Other : l 1 1 1

. I) SARGENT & LUNDY E N GIN E E R S CHICOGO Proj. No.:4391-00/4683-00 } Acc. No.: EMD- 019178 I \\ Calc. No.: 1FW-04 Rev.: 04 Date:7-17-80 e Page 5 of 19 i g ti); ANALYSES PERFORMED

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's ? Check-j list Sec. Comments ( Loadings Date Item 0 No. 1.0 C ~ DATA 1 7-17-80 2.0 D j THERMAL 1 7-17-80 MAX. OPER. 567 a 3.0 E WEIGHT 1 7-17-80 5.0 F SEISMIC 1 7-17-80 6.0 I TRANSIENT 2 7-17-80 i} COMBINED 8.0 A STRESSES 7-17-80 I l 'u COMBINED 9.0 B q i {'. REACTIONS 7-17-80 T' I 4 i 1-( v l 1

\\. Proj. No.: 4391-00/4683 v0 Acc. No.: EMD- 019173 DIVISIONAL g 8;7C'll,Mljj',jM Calc. No.

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Page 6 of 19 STANDARD EMD CIIECKLIST FOR -PIPING SYSTEM STRESS ANALYSIS X p7pgyg NOiiEAT SRVA Validat'ed Programs Used: ? l Checked l Comments Description 1.0 Basic Design Data (Output Section C) 3 Are all branch lines per Ref. 1.1 included where I /IB <E 7.0? R Are all m'aterial types coded in 1.2 agreement with Ref. 2? { Are all pipe / fitting thicknesses 1.3 I, and uniform weights in agreement ( with Ref. 2? Are all motor or pneumatic operated / No V.alves i 2 e/' 1.4 j valves modeled using lumped masses (I and cg's? .e Some too short elements u Is the system modeled correctly modeled due to fitting j 1.S (length ratios, etc.) ? configuration. Are all hangers / restraints modeled m S modeled at 40A in-o. y f, 1.6 correctly per Ref. 2? stead of 40B. or Are there any special modeling Restraints at 73 & 75 1.7 techniques used in the analyses 50 modeled interchanges. ~ (equipment flexibility, special etc.)? restraint configurations, i j N Are all node types coded correctly? / 1.8 t' Is the internal pressure (max. op. d 1.9 pressure from Ref. 2) coded in t f Psig? (%

4391-00/4663-00 l Proj. No.: Iscc. No.: EMD-01917o 1W-04 DIVISIONAL 0,9]3H[My))'f Calc. No.: 04 Date : 7-17-80 () TECllNICAL Rev.: . =,.., g PROCEDURE ""*^ Page 7 of 19 Checked Comments ) Description l 2.0 Thermal Analysis (Output Section 7. Are the analyzed thermal modes in 2.1 agreement with Ref. 2? 3 Are the anchor movements in agree-2.2 ment with Ref. 2? l Deflection of order of 2" at some nodes. Check Are all the deflections reasonable 2.3 j (if over 1.5", specify)? for interfereace. Weight Analysis _ (Output Section E) ( 3.0 3.1 Is the overall support system balanced? / I Are all pipe deflections within [f 3.2 0.2 inches? 3.3 For hydro-run, verify that all N/A 'l spring hangers were pinned per i the appropriate standard. Eauivalent Static Load Analyses l 4.0 t a b c d e f g h ! l-i ~(Outpu t Section D) The following: analyses are l l*i performed using the PIPSYS static analysis routine: l 4 l l-a- G b-c- mo d- !l e-n f- .w g-S h-Are all design parameters in n 4.1 .i agreement with Ref. __? l ca Are the forces input correctly Cf. 4.2 in the PIPSYS with respect to J direction and point ,/ magnitude, of action? ,l ye l' ! 4.3 Has the ef fect of seismic j e$ differential anchor movements l been considered (Reference)? o k

Proj. No. : 4391-00/4683-00 DIVI ~IONAL acc. No.: EMD-o_9173 Calc. No.: 1FW-04 OMU3b{j]'/ Rev.: 04 Date: 7-17-80 (* TECIINICAL PROCEDURE _; ;c;; ;.u.; J C " 'C ^C C' Page 8 of 19 Checked Comments Description 5.0 Dynanic Analyses ab c d ef g h (Output Section F) 5.1 The following analyses are performed using response spectra method (Seismic in PIPSYS Output) : / 1/ a-Seismic b-c- d-l e-i k. f_ g-SSE spectra not h-used - a more . 5.1.1 Are the latest revisions of r c nservative response spectra used for the / estimate used analysis (Raference)? instead. / 5.1.2 Are the length ratios accept- / able? 5.1.3 Does cut-of f frequency cover / f ([. the peak acceleration value? S.1.4 Is the square root of the [ double sum method used to combine the modal responses? \\.. / 5.1.5 Are all the deflections i l G reasonable (if over 1.0" / l OBE, specify)? uo m 5.1.6 Ilas the ef fect of seismic differentia) anchor movements been considered (Reference)? a. w 5.2 The following analyses are per-formed using the forcing func-y tion method ~ (Transient in [g ] M PIPSYS Output): y a-fuK? TR\\f l b- = C- '4 d-a x e-f- 9-o h- .. ~. - - -- i

'Proj. No.: 4391-00/4653-00 Acc. No.: EMD 019178 DIVISIONAL SJ'.03EOTSUJ.~2?/ Calc. No.: 1ru_04 TECIIMICAL C' ' Fev.: 04 Date: 7-17-80 PROCCDURE c,g,w n.c m _ Page 9 of 19 C*C^ l Checked l Comments l Description a b c d e f g h see DD-013046 5.2.1 Is the force calculation per-formed per the appropriate I documents (Reference)? 5.2.2 Are all necessary design parameters specified in this analysis (opening / closing times, flow rates, etc.)? (f 5.2.3 If force calculations are not attached to this analysis, reference. \\' 5.2.4 If a safety / relief valve analysis is performed: Does the steam stagnation ( a. pressure and density re- 's s flect the S/RV set point? \\ b. Are the pipe ID and seg-f ment lengths input cor-(- rectly in the SRVA pro-L- gram? ( c. Is the pipe submerged length correctly calcu-lated and input? G d. Is the correct density used in the calculation? \\ \\ N o 5.2.5 Are the forces input correct-y ly in the PIPSYS with respect to magnitude, direction and Sh point of accion? 5.2.6 Are.the equipment reactions { included with the correct s n load set? ~ m n' 6.0 Thermal Transient Analysis (ASME Class 1 Piping Only) N/A i [,. I g 6.1 Are the results of transient g analysis attached to this report? l 5 4

~ Proj. No. :439l-00/4683-00 Acc. No.: EMD 019173 DIVISIONAL Calc. No.: lW-04 b[$}3(([bl,{.))y Rev.: 04 Da te : 7-17-80 ' (') TECllMICAL - =;- ~2,q. PROCEDURE C "C ^ Page 10 of 19 Checkhd Comments Description 6.2 Are all transient stresses identi-fied and are the NOHEAT RUNS properly documented? / i 6.3 Are thermal transient conditions and cycles cort.::t per Ref. l? ( 6.4 Are all discontinui' ties considered? Check film coefficients, densities 6.5 and material thermal conductivity. tr 6.6 Are correct time steps used in v. performing the transient analysis? 7.0 Hand Calculations 7.1 If hand calculations are not attached to this analysis, reference. Are the calculations reviewed in 7.2 accordance with GO-3.08? () A detailed review of original calculation. ( A review by an alternate, simplified or approximate method of calculation. f A review of a representative sample of repetitive calculation wo A review of the calculation against a similar calculation m k E previously performed, ~ l (Output Section A) r 8.0 Combined Stresses 8.1 Are the stresses within the / f m allowables? for the Are the ' allowable stresses 8.2 materials used in the analysis in r(- agreement with the Code? l D Ci 8.3 Is the design pressure in agreement with Ref. 2? g

Proj. No.: 4391-00/4683-00 Acc. No.: EMD- 019178 Calc. No.: lW-04 DIVISIONAL O."C32((((1],-j[jf/ Rev.: 04 Date: 7-17-80 TECllNICAL e,y3:.g 3.g 19 PROCEDURE c -ic eo Page 11 of Checked l Comments Description Are all thermal load combinations S.4 specified per Ref. l? Are all mechanical loads listed, per as service 8.5 the design specification, 16 vel B, C or D? Are the number of earthquake cycles N/A calculated per the design specifi-8.6 cation or per SRP-3.7.3? N/A Are all high-stress / usage' factor ./ (over.1) points run with the 8.7 detailed output? Combined Reactions _ (Outp'ut Section B) 9.0 - Are all applicable forces and moments considered for both upset 9.1 and emergency conditions? 9.2 -Are all the equipment nozzles identified correctly? Are equipment loads and valveHave they i 9.3 accelerations acceptable? been forwarded to the EMD/CAS? f -( Are the vendor supplied component L supports able to carry the imposed 9.4 loads? Are all Type 3 restraints reviewedto determine if th _e 9.5 l u 0 by rigid restraints? l e Method used to combine the loads: f 9.6 SRSS Absolute Sum x )> n" l s b % 1 m. W E c_ -v

U SARGENT & LUNDY C N GIN C E R S CMacAco Proj. No.: 4391-00/4633-00 Acc. No.: EMD- 019179 Calc.'No.: IW-05 ~ Rev. : 04 Date :7-14-80 Page 120 f 19 GENERAL NOTES The analysis is based on the following Code and S&L Prograns: I. 2 of' 1975 issue. ASME Code, Sec. III - Class issue. ANSI B31.1 of issue. b. " PIPSYS" -(Prog. No.' 09.5.065-5.0 ) of 6-13-80 ) of issue. "SRVi" (Prog. No. "NOHEAT" (Prog. No. 09.5.075. ) of issue. i II. Coordinate Systems: Y b M 4M b y ~ el M N ( .g z a Z g GLOBAL LOCAL III. Conclusions & Design Requirement. The pipe stresses'are within Code allowables. l 1. j The following support changes were made: 2. Node 15A & 75 - add Sx skew (horiz. A to pipe) 1 Node 15A, 40A, 82 - Add Sy Node 45 - add Sx Node'65B - add Sz skew (' axial to pipe) The loads on the' Steam Generator nozzle are within 3. Westinghouse allowables. \\ ~ -~.,.._-% ~ ~ ~ ^ " * - - - - -

d SARGENJ & LUNDY ENGINEEH$ CHIC AGO Proj. No. : 4391-00/4683-00 Acc. No.: EMD 019179 ~ 'r"-os cato no = O ~ Rev.: 04 Date :7-14-80 Page 13 of 19 GENERAL NOTES - cont. 4. Tee Information: The instrument taps at nodes, I'i'1, IT2 & IT3 (all 16x16x2-3/4) need no additional reinforcement. ( Compressive loads occur on the hangers at the 5. -(.. following node points: 55B & 75. 6. Loads from FW Pump Trip Hydraulic Transients were considered in this analysis. e 4 h - (" w C ew 1 1 0l 131 i~ O I'

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(#ll,i-l De ",h* [0 ~~T'- l ;:*' ' Byron /Braidwood Units 1 & { 0 "'- f ch.n Connonwea1! h Edi;ipLCoppM1Y M.-- 2 ne,:r.ed by g A:ere red.by [ h,4391,92/4683,S gOf}g, - ~ ~ * - ..-..--.n. -: - - * ~ * ' ! ~ ~ ~~ Equipr.'.ent No.:/,O #/ N ~ k"' 1. 2. Pipe Line: /#ts 63l'y",- //, Class: 8 . P' Y,J Allo.wable 2.707. Thickness: 3. Pipe Size: g,, - - memo EMD- 020130 T ickness:,pe/J Nozzle Size / 4, .___.._!.......2----- 4. Nczzle Connection:[b) [^[6 7 //S3'f/'~'f,.._;..__ _,. ;. S. Pressure: 5. Max. Op. Tcm!'. ff7eg !!oments in f t-lbf Forces in lbf M, M .i 3, E,,, !!x y_ F y,( LOAD F F x -~ g 7 j 3'l / - 93 17 ^ 9 i *M'

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j /,..:. c. 2a 7 l ,in. IG H,i , REACTIO:!S j -'-'D j.nyp llg)g10 } f,pd O f0N '/S;'~~ & w MC1Gil? ypp ' 'I ALLOWADLES { f s ' ',' W-.I ** N. OBE -..,-(,3 g gj g $?. Q.(#- y(> c(-Q lO, REACTIO2iS l ~ e 13,w' T3;"' " 1l 14:'# l p/cao co nD z w/ \\. onS i ALLGWADLES j, l & CIF~ .!sf,jt} iL~h7 h -{,)'s s.41. t 2 ?$ hllh. > \\'..- i SSE ? u 3 ~ I. REACTIONS /png Q,yg gp 9 6'O gpf l0C}ddd l0.; O 0' A s l SSL 8 / / ALLOUAELr.S i -i o [ ' .,s.. g i' t*' W t< : - t it :f ( ' w-4/ / $(J; 9')G}, .)-S\\?$ '(.*S'!i . s.. I h REACTIO:JS = '~ LC'. a B E N.l 0,;',?. ' / Y-A'#- / 71, % OVER j ~^ Pro). No.:4 391-0G/-;6 33-00 ~~~~~~ A.. No.: E t,1 D - 01917 8 l Av pvertical) ( s e3u~ d3. 1Fh. 0 4 ( i y i West.inqhouse M '/)Y' / Rcv.: 04 Date: 7-17-80 Coordinates: f / 3xa / 5'Me 19 of 19 Sj!k tft y i [. % lb6 f./[ // l e __ aw 'a .. ~__,...., w

D08 WEP"" l SARGENT ANU LONDY ENGINEERS . INTEGRATED PIPING ANALYSIS *ROGRAM . PIPSYS 09.5.065-5.0 JUN 13 1960 ............e........ COMBINED REACTIONS 17 JUL 80 4391-00 8/9 1 1FW-04 REV 4 AJP ... CONTENTS OF FILE 13 ON 17 JUL 80... 4391-00 8/8-1 1FW-04 REV 4 AJP LOAD DATE RUNID CormENTS iFi B ^Jul18 itMS o8E SEISM 1C AN c SIS-INE u IA 1 UT 1 17 JUL 80 247AJP WEIGHT ANALYSIS 2 TH 1 17 JUL 80 247AJP EXPANSION ANALYSIS AT 567F 3 TR 1 17 JUL 80 684AJP HYDRAULIC TRANSIENT TIME HISTORY ANALYSIS 4 MAXIMUM VJMBER OF ANALYSES THAT CAN BE SAVED FOR THIS SUBSYSTEM IS 20 ? A

E08 M"2 4391-00 8/8-1 IFW-04 REV 4 AJP LOADINGS FOR COM INED REACTIONS 17 JUL 80 WEIGHT LOADING 1 TNERMAL LOADING (S) 1 SEISMIC (08E) LOADING 1 SEISMIC (08E) LO@ING 2.00*(08E LOM1W ) HYORALLIC TRANSIENT LOADING UPSET COMITION 1 EMERGENCY CflNDITION 1 ANCHOR /DISPLACENDIT LOA 0(S) (NOT APPLICA8LE) MECHANICAL LOADS (NOT APPLICABLE) i 1 V A

^ ~ F08 M2'1' 4391 00 8/8 1 1FW.04 REV 4 AJP MAXIMUM OF COMBINfD ANCHOR REACTIONS 17 JUL 80 IN LOCAL COORDINATES i (RESULTS A4E IN FT.LB UNITS) l LOCATION WEIGHT THERMAL ANC/ NYORAULIC TRANS SEISMIC MECHANICAL 1 MECHANICAL 2 COPSINED DISP UPSET ENERNCY UPSET EMERNCY UPSET EMERNCY UPSET EMEAMCY UPSET EMEANCY r 5 FA -6. 4682. O. 4176. 4176. 620. 1240. O. O. O. O, 9471. 10091. F8 2311. 657. O. - 86' 866. 434. 868. C. c. O. O. 3611. 4045. l l FC -13. 903. O. 12570. 12570. 971. 1943. O. O. O. O. 14458. 15429. l MA 1906. 15964. O. 1449. 1449. 3187. 6374. O. C. O. O. 22506. 25692. MB 513. -20702. O. 67590. 67590. 5140. 10281. O. C. O. O. '92920. 98060. MC 8148. 4138. C. 3782. 3782. 2299. 4599. O. O. O. O. 14230. 16529. l j 115 FA 13. 1027. O. 5384. 5384. 3307. 6414. 0. O. O. O. 9731. 13034.. FB -2213. 1275. O. 12260. 122(0 2413. 4826. 0. O. C. C. 16887. 19299 i '15304. 18150. FC 7. 4673. O. 7792. 7792. 2846. 5692. O. O. C. O. KA 3993. -21391. 0. 28'28. 26128. 20064. 40128. C. O. O. O. 65591. 45655. PS -328, 38177. C. 16344. 16344. 10571. 21143. O. O. O. 0. 64764. 75336. MC 2173. 7154. O. 17640. 17640. 10506. 21013. O. 0. O. C. 37473. 47980. I l h

l G08 EP"1' 4391-00 8/8 1 1FW-04 REV 4 AJP MAXIMUM 0F ColWDCD ANCHOR REACTIONS 17 JLA. 40 (REstA.TS AAC IN FT-L8 UNITS) LOCATION WEIGHT TERMAL ANC/ NYDRALA.IC TRANS' SEISMIC MECHANICAL 1 MECHANICAL 2 COPSINED l DISP wsET EMEaNCY WSET EMERNCY WSET EMUNICY WSET EMEANCY UPSET EMEANCY L 5 FX 7. 3335. O. 11085. 11085. 836. 1672. O._ , O. O. O. 15 63. 16099. ELS84L FY 2311. 657. O. 466. 466. 434. 868. c.,. o. c. O. 3611. 4045. FZ 12. 3404. O. 4154. 8154. 793. 1584. c. O. O. O. 12342.~~13135. MX -3744. 12253. O. 3369. 3369. 2552. 5105. O. O. O. O. 12427.1 14979. MY 513. 20702. O. 67590. 67590. 5140. 10281. O. O. O. O. 92920. 94060. MZ 6082. 11037. C. 2250. 2250. 2984. 5976. O. O. O. O. 22358." 25346. 115 FX 7. -3316. O. 4498. 4694. 1680. 3360. O. O. O. O. 9701. 11300. GLOBAL F1 2213. -1275. O. 12260. 12260. 2413. 4426. O. O. O. O. 16887. 19299. FZ 12. 3449. O. 9034. 9038. 4026. 8052. O. C. O. O. 16501. 20527. MX -2271. 21979. O. 18741. 18741. 21869. 43737. O. O. O. O. 60317.- 82186. MY 328. 38177. c. 16344. 16344. 10571. 21143. O. O. O. O. 64764. 75336. MZ 3938. 5066. O. 25079. 25079. 5892. 11784. O. c. O. O. 34910. 40802. l 1 <L~ L 4

H08 gig S f 4391-00 B/8-1 1FW-04 REV 4 AJP EQUIPMENT N0ZZLE REACTION SUPMARY (LOCAL) 17 JUL 80 LOCATION : 5 PENETRATION P.87 i LOAD FORCES IN LOS HOMENTS IN FT-LOS CASE FA FB FC MA MS MC j I WEIGHT -6. 2311. 13.

1906, 513.

8148. THERMAL EXPANSION 4682. -657. -903. 15964. 20702. -4138. 4 ANCHOR / DISPLACEMENT 0. O. O. O. O. O. HYDRALA.IC TRANSIENT UPSET 4176. 866. 12570. 1449. 67590. 3782. EMERGENCY 4176. 866. 12570 1449. 67590. 3782. SEISMIC UPSET

620, 434 971 3187.

5140. 2299 EMERGENCY 1240. 868. 194. 6374 10281. 4599. MECHANICAL 1 UPSET 0. O. O. O. O. O. EMERGENCY 0. O. O. O. O. O. MECHANICAL 2 UPSET 0. O. O. O. O. O. EMERGENCY 0. O. O. O. O. O. MAXIMUM CONDITION UPSET 9471. 3611

14458, 22506.

92920. 14230 EMERGENCY 10091. 404$. 15429. 25692. 98060. 16529. MAXIMUM CONDITION UPSET FA = 17657 MR = % 660. EMERGENCY 18875. 102709. 4

s I08 ME1 5 4391 00 8/8 1 1FW-04 REV 4 AJP ESUIPMENT N0ZZLE REACTION SUPW1ARY (LOCAL) 17 JUL 80 LOCATI006 : 115 STEAM GENERATOR. FW Ilt.ET (1C-1RC018C) LOAD FORCES IN L85 MOMENTS IN FT-LBS CASE FA F8 FC MA MB MC WEIGHT 13. -2213. 7. 3993. 328. 2173. TManAL EXPANSION 1027. 1275. 4673.. -21391. 34177. 7154. 0. O. 0. O. O. O. ANCHOR /DISPLACEPDIT HYDRAULIC TRANSIENT UPSET 5384. 12260. 7792. 28128. 16344. 17640. EMERGOICY 5384. 12260 7792.

20128, 16344.

17640. h. h$4k' h E Y 64 4. MECHANICAL 1 UPSET 0. O. O. O. O. O. 0. O. O. O. O. O. DERGOICY MECHANICAL 2 UPSET 0. O. O. O. O. O. DE.1GOGCY 0 O. O. O. O. O. MAXIMUM C00GITION UPSET 9731. 16887 15304. 65591. 64764. 37473. EMERGDICY 1D38. 19299. 18150. 85655. 75336. 47990. MAXIMUM C0fSITION UPSET FR = 24780. PWI = 9*503. DERGOICY 29528. 123751. i 1

l. _] _ _ J08 g S 4391 00 8/8 1 1FW.04 REV 4 AJP EOUIPMENT N0ZZLE REACTION SUPMARY (GLOOAL) 17 JUL 80 LOCATION : 5 PENETRATION P.87 LOA 0 FORCE.1 IN L85 M0MENTS IN FT.L85 CASE FX FY FZ MX MY MZ WEIGHT 7. 2311. -12.

5748, 513.

6082. TERML EXPANSION 3335. 657. 3408. 12253. 20702. 11037. ANCHOR / DISPLACEMENT 0. O. O. C. O. O. HYDRAULIC TRANSIENT UPSET .11085. 8f%. 8154. ' 3369. 67590. 2250. uiun.UsCY 11085. 866. 8154. 3369. 67590. 2250. SGSMIC UPSET 836. 434. 793. 2552. 5140. 2948. EMEAGOICr 1672. 868. 1586. 5103. 10281. 5976. . ECMNrC= 1 UPSET 0. O. O. O. O. C. EMERGOeCY 0. O. O. O. O. O. MIENCr 8: 8: 8: 8: 8: 8: "cc""2c" 2 MAXIMLM C00eITION UPSET 15263. 3611. 12342. 12427. 92920. 22358. EMERGENCY 16099. 4045. 13135. 14179. 98060. 25346. MKIMUM C00eITION UPSET FR = 19958. M= 96376. EMERGENCY 21168. 102385. 1 e e

K08 /; 4391 00 8/8-1 1FW.04 REV 4 AJP s EOUIPMENT N0ZZLE REACTION S M Y (GLOSAL) 17 JUL 80 ) LOCATION : 115 STEAM GEERATOR - FW IILET (1C-1RC01SC) i LOAD FORCES IN L85 MOMENTS IN FT-LO$ i CASE FX FY FZ MX NY MZ q WEIGHT, -7. 2213. 12. -2271. 328. 393C. l TW" MAL EXPANSION -3316. -1275. -3449. 21979. -38177. -5064. ) ANCHOR /DISPLACEMDIT 0. O. O. C. O. O. NYDIIAULIC TRANSIENT UPSET 4698. 12260. 9034. '18741. 16344. 25079. EERGDICY 4698. 12260. 9038. 18741. 15344. 25079. SEISMIC UPSET 1640. 2413. 4026.

21869, 10571 5892.

i r.numUsCY 3360. 4826. 8032. 43737. 21143 11784. 4 MECR4NICAL 1 0. O. O. O. O. C. GDICY 0. O. O. O. O. O. MECMANICAL 2 UPSET 0 C. c. O. O. O. EERGDICY 0. O. O. C. O. O. MAXIMUM ColeITION UPSET-9701. 16887. 16501. 60317 64764. 34910. l EMERGDICY 11380. 19299. 20527. 82166. 75336. 40442. MAXIMUM C0feITION UPSET FR = 25525. PWI = 95138. EMERGDICY 30387. 118721. J l l l 0

LO8 MEP"1 ' 4391 00 B/8 1 IFW.04 REV 4 AJP MAX RI RJ, Og5 IN L85 17 JUL 80 N00E WEIpfT THERMAL ANC/ NYORAULIC TRANS SEISMIC MECHANICAL 1 MECHANICAL 2 CorSINED DIRECTION DISP UPSET EMERNCY UPSET EMERNLY UPSET EMERNCY UPSET thatNCY UPSET EMEANCY 15 4543. 2946. O. 1439. 1439. 1459. 2917. O. O. O. O. 10347. 11845. Y 0 1H5. 186. 658 6566. O. O. 8275. 8275. 2558. 5117. C. O. O. O. 17399. 19957.. Y -1008. 5275. 7834. I f I e

O e e m i t I CO o E .#b M O x. G W. ( .#1 I W:

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m8 8* R m. l ga : 2=;E-9 x i. $.$. a.s. ,e. >a m W e-- M l w l

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Og "-g ~G 2 " 'W'* : -= - g " l. e, l "E E 8Ia~: a W P: W >= .J e

e l'P F.M ~ 8 0 C I N M S). I" E! S( LT. 0 0 8 AN.. 1 5 4 CE. 0 2 3 IM TE RV EO. VM. 0 8 ) N L I 08 03 05 U (Z. 05 00 05 J S 09 04 02 T 7 N 1 1 E M E P V J ) O 4M A 2 M . 08 50 1 . 02 00 A Y. 06 30 50 TE L 4P A 0Y M T R R E ET H. 4 GN T NI V AA E 50 80 00 E MR GX. 30 10 70 N 20 80 50 R TS A EE R 1 1 40 IR R( W P 0 F S A 1 O L). 7 4 4 S 3 0 3 TS. 1 2 9 6 HL. 5 2 3 G( 8 / I 8 E W 0 0 . 5 3 0 1 E . 3 7 9 9 0 3 0 4 N a

809 1 SECTION 8 PAGE 6 I 4391 00 8/8 1 1FW.04 REV 4 AJP HYDRAULIC SNUBBER DATA 17 JUL 80 (RESTRAINT TYPE 3) RANGE OF THERMAL DYNAMIC LOADS LOS) MOVEMENTS (INCHES) FNC/ HYORAULIC TRANS MECHANICAL 1 SE SMIC MECHANICAL 2 COMBINED DIRECTION N00E X Y Z DISP UPSET EMERNCY. UPSET EMERNCY UPSET EMERNCY UPSET EMERNCY UPSE7 EMERNCY 20A .911 000 000 0. 17888. 17888. 0. O. 2592. 5184 C. O. 20480. 23072. Z SKEV. .000 .004 .332 40A 1.2% .000 .000 0. 2122. 2122. O. O. 1861. 3721. O. C. 3982. 5843. Y .000. 654 -1.029 400 1.383 .000 .000 C. 20148. 20148. O. O. 2686. 5372. O. O. 22634 25520.

  • X

.000 .661 -1.018 1 45A 1.361 .000 .000 0. 4752. 4752. O. O. 2548. 5096. O. O. 7300. 9847.. Z 4 .000. 605 .595 l 508 .977 .000 .000 0. 3094. 3094. O. O. 1633. 3266. O. O. 4727. 6360. X t .000. 589. 475 60 .592 .000 000 C. 8173. 8173. O. O. 4325. 8649 O. O. 12497. 16822. Z .000 .230 .753 75 .830 .315 .000 0. 15200. 15200. O. O. 3763. 7526. O. O. 18M3. 22726. X l .000 .000 .382 ( I e g l

e i LONGITUDINAL LUG CALC SHEET' l,! PETRAINT NO. lN o 4o145 ati.: ar. 59th ca.es,c5 rn. e .vetD TrrEi '.c -1 LONGITUDINAL LUGS U " " ' WWO4 EI. P&E 0I22: /b S N D: M '"t*= O/4 D= /6 3 444 . v-t ( neDE rerrT: 46P' rIrz ctAss o n i -- - f '" OSINGLE LUG LF=1.0 ..l,e"h (s91u n,. 2,2A,353^) O DOUBLE LUGS -tz ,. ~s v ESHEAR LUGS LPO.5-( ~ 9 n. r s 4.>. = > C3 q ( 591h rig. b) 7 1SA "f6 UN O/U 9 8 Q v 591h Det. Luc In::Ta Luc THICCEOS PAD THICEES3 591h Fig. LUG LENCTH A

  • I
  • T=

'S.O.0 SINCIE LUG (rig. 2,2A,3.)Ah) (gf,,, E

  • b
  • T=
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  • D/c os *

= D 'I* 'T" 'U* 2A

  1. L.

CA E 'N

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) 'D _g ra 3A .D. p asumm.

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O MOMENT ARM-h LOAD FACTOR -LF u r-7,,dy) L~hr

g s m n,.

tm Turcatos j m .T. 2u

e.,

., 7 ' MOMENT kkM-h

  • c-

'^~ Eat =' - Det. B6E; A = 0.0 in if app. it D, n, me e= u- ......t o., .E in " 37f N ' ^5Di 8^ - 5" IN h

  • C+A-S-Do/2 Det. A or 5: a6E-in SHEAR LUGS h=

(# I' APE ** A. EMD-020697) Ictmz tres (Det. A or D) h t. D or E: M= in SINGLE LUG:

  • C.
  • s.

h=- IN is *E h / Ti (or_) y,c I ? I h.*C *S-Do/2 YES-L F= 0.5 f~ T E too i _.__gra f . 4 (in) N O - L F = 1.0 5 h s. in } ~? Ds " /* I ~T MDDELING s-, + ' Indicates dimension from 591! dwg. 4 t! Pear Pnd Bracket "A" dimension fres l 1/4(Do+2x*S)= 4 Appx. A, L'M.D-02697.

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is E < 1/4(Do+2x*S)? o n la + Ave radius of model from Appx. B, (#'..) ,,T. ' 26... M::; b O Y ES "" 8t"82 '"* "od-i a - l (tw.1 aa Storia inal ] '. NO Use Dobule Ing Mode LUGS P i i, SHEAR ] IOl'BLE LUCS (Det. B or E) Cocconwealth Edinon Compg m,p.,es h, [/ h h[u4dd. Doin g(( C*d w Le gituM nal lugs ca n. gi, l0e Dyren/Praidwood Unita 1 & 2 n,. =,d., [ j M

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) n o i t aa 2 s i r d rt l l ee d i ,e e nt n l a ) w oie e e F 1 rp o t V ,o 4 6 l o ) c N i 1 8 n 4 s 1 / / o l S t / / / / et .re el 1 3 1 5 3 s r*Dc gh 2 i ol e .e h u t' uS tf nfl a a l i i P s

i. n t M F n

re a t e2 i o a c a n dhn 1 eo e-2t t 1 ) h. p" sif k t f 2 st ewI c r ( i a i 3 o e l' 5 a t o l 2 0 o 0 r . eI s h p o o t be l-0 o 0 on 4 u e h ? e T e t e ) a s f r tt w T .fr A o n f 1 w e o. o. 0, 5, f w p o / sh i i 6 3 I ( o r eo 8 7 7 7 oh lt s, e eel 1 r" D ASb 1 2 2 3 r. rhe t' e Ig t r r r r lS e( ~ A.,_ e e e A a" a cj o v v v 4 4 z M n) t c dS s. o e o i t9 o1 l oW l ln i a V um F~ - l )g~ qo erf /P )h ( Pir + H s o () f yn N - ao nN n ( o wi i t i l s F T. an i _e 9 e a ei r n 8 e ) ) li t S. v l 9 6*& Y d e g e e la S d. R w a P V P D I oe 0y L 6 e P lt r t n e n p ) s gm t e F E i i P ( o si t a X r ud c r t n F rn i. D C 3I hI s 0 i t [ e O R e._ ) ) m M l L5 e P o / l r t a ( / / F V + g ) ( a )d S 5 7. J p f( G e a e te ( + i P ) D o o U d c a 3 n ( o h R 7 i L L kn 7 e L 4 r p 4 4 E 7 ) j s 0 o 1 a L e o , b ) c 9 G 3 F ex c 2 7 g 1 ( (Q 5 j N 1, t S t t x .d Bu b l IS ., p = _h s .n r 3 o o s C b. 4 i c t ) o t c 6 t n h 9 z 0 c e )x 1 f m dL i m n (S 6 . A n P x 4 st o s .!i ( ) 2 b l v ( l o i i n&. a L f n n 1 e ) i t 0 ar

r. f y

s n 1 li rt n , u i a e a 2 n rh u r S i 0 O , h )x p u t e q T cT a,M e Et ( (S c C s x ) f mt e t o k (e b i h r n i ( fg o n yiil s U l ea i i nswn d d l t 5 R_O M"2 i E o o s n o r c P l drar h w e O e a ) S eth e t d 0 r. qle v w P o /a 3O x)O E e I E S v n D rSt r l i 6 s ) D S o F / o b i e a a Y L 0 uerr e r R L (I C z Q. S W M A / I C bh n/ o. P n P e / C S S n n H . i m 6 z r at r o m = I C U r C 3 m a woe n e F I I I o ( f u r 9 i N 1 o o t I E E E S = u. P M A N tls o y 3 S Ot V T S S T s P I h d2 C B L l R 1 Aa-9 F 1 op rN C ,a., ( 3 ie lT 0 O m C NC L. D 0 4 .k R c S DN n a EO E G gh D O a'

m. 0 o

4 I T = =m, = I F s 'E CF )nT C + 1 m h 95 S k + T A C H E G T w3 L (BC T F = S MA +q N I + + h O 7 7 CE 123 O-W7 T D W N m H W I S/ 4 W N CE A N T 4 t O 0 I U L A =' lvR O E t L T S u s = DN. 8 9 9 O I O N T T 2 ER E N E I l CO G me E P CE o H E U m M A 1 F~ W r2 'A r T S tc S m h 8 @2'g,r '.I.

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