ML20062N047
| ML20062N047 | |
| Person / Time | |
|---|---|
| Site: | LaSalle |
| Issue date: | 03/31/1981 |
| From: | SARGENT & LUNDY, INC. |
| To: | |
| Shared Package | |
| ML20062N026 | List: |
| References | |
| NUDOCS 8112180357 | |
| Download: ML20062N047 (194) | |
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8112180337 811215 PDR ADOCK 05000373 A
P R O J E C T:
LaSalle County - 1 EMD FILE NO.:
029197 Y M*8[
DA 0 2 /0 2/R '
PROJECT NO.:
REVIEWER:
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RUN ID LIST:
.ee to i
902 ITK 12/01/80 W_o 322 ITK 12/02/80
" 'Y 317 ITK 12/02/80 a
1m 319 ITK 12/02/80 7A 32? ITK 12/02/80 I
320 ITK 12/02/80 i4 310 ITK 12/02/80 y "d 270 ITK 12/02/80
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SAFETY-RELATED 071 ITK 12/02/80 0 ::
068 ITK 12/01/30 h-MNHe"' CAL DEE N "FNT NDARD
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Safety-Related @ Active l
O sassive ll COMMONWEALTH EDIS0N COMPANY lA SALLE COUNTY NUCLEAR STATIONS 6093-00 l
NSSS EQUIPMENT QU l.IFICATION l
Equipment Name:
LPCS Pump Equipment Number: E21-C001 l
Manufacturer: It.;ersol Rand Cornpany Model Number:
29-APKD-5 This folder contains the following Qualification 1
-Documents for the above equipment, l
1.
SQRT Form 2.
Qua* ;fication Report for LPCS, EMD File # C28197 3.
4.
5.
t 6.
7.
8.
9.
10.
i Iteviewed by:
g,ovg#m Date 2-02-81 EMD File #
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Date:
Approved by:
g, [,gQ Date 2-03-81 Page 1 of _
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LA SALLE NUCLEAR STATIONS' j
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l UNIT 18 2 L
I NSSS EQUIPMENT QUALIFICATION
SUMMARY
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if IEQUIPMENTf1AME:
LPCS Pump i
i EQUIPMENT tio: E21-Cool 5
LOCATION:
Reactor Building El. 674'0" j
EQUIPMENT CLASSIFICATION:
E] ACTIVE
] PASSIVE r
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QUALIFICATION METHOD: Analysis j
J'l QUALIFICATION DOCUMENT
REFERENCES:
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1.See Page 4 & 5 of EMD # 028197 (Contained in this folder )
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LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:
1 1.
Normal Operating Loads + OBE +
SRVASY-TQ +
ALL-TC, ENVELOP h
4 ENVELOPE f
2.
Normal Operating !;oads + SSE + COLEVY-2+
E ASY-TQ*
ALL-TQ_
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3.
Norma 1 Operating [oads + SSE+ Chugging + SRV337_7g + SRVggL,7g ENVELOP [
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]
4.
Normal Operating Loads + SSE + AP f
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'5.
Normal Operating Loads &SSE + CO gyy,y h
GUALIFICATION:,
EREPARED BY:
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/k Date 1-0,7-81 REVIEUED BY:
/d5f h"MM7 Date 2-d1-S1 gg.g
{ AP.90VED BY-
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1 OUALIFICATION SUIStARY I
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QUALIFICATION METHOD:
(
)
The analysis is performed to assess the adequacy of the pump / motor assembly I
z design when subjected to static, seismic and as sell as various hydrodynamic loads per project specification.
A three dimensional lumped mass beam finite element model of the pump / motor assembly and its support is developed and dynamically analysed using the l
response spectrum analysis method. The same modet is ana1ysed due to static nozzle loads, pump thrust loads, and dead weight. Critical location stresses are evaluated and compred with the allowable stress criteria and critica1 O
1ecetien deftectiens end ecceteratiene ere cheched te evateete egeres111tr.
l Response spectra curves for this analysis are conservatively developed by j
enveloping the EW and NS curves for horizontal spectra and wall and slab
[
curves for vertica1 spectra at elevation 673'-4"-of reactor building. This 1
enveloping process is performed for all scunic and hydrodynamic spectra
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curves. Same horizontat spectra (enveloped) is applied in both horizontal directions during the analysis. Modal analysis was performed using the
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Subspace Iteration Technique and alt eigenvectors N saved on a ' permanent j
file for subsequent analysis with various dynamic loading conditions.
Twenty-five modes were considered in the analysis, with the frequency range of 7.82-140.5 cycles /second.
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Ref: EMD File No. 028197 a
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Qualification kmunty of Equignent O
LASALLE COUNTY l f
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Plant Name:
.pype.
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1.
Utility:
CECO PWR 2.
?
5 3,.
A-E-S&L' i
k II.
Couponent ! tine LPCS Pump f
1.
bbdel Nu::ber 29-APKD-5 Quantity:
1 2.
Ven$or Ingersol Rand Company
{
3.
If the conponent is a cabinet or panel, narre and 'model No. of the devices included; NA
[
Multistage, vertical mounted, motor / y AppearancchPump assembly -
4.
Physical Description a,
38'-9h" Total he., 36" casing 0.D.
b.
Dinensions I
Tota) floor load 37050 lbs.
c.
Weight l
l 5,
location: Building:
Reactor Building l
i Elevation; 674'0"
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-6.
Field } bunting Conditions [ 20 Bolt (No.10, Size 1 /4 )
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Weld (Inngth
)
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7.
Natural Frequencies in Each Direction: Frequency table is
_ h given on p.12 of EMD # 028197 3
hl:
h2:
V:-
l 8.
a.
Functional
Description:
The fuction is to prevent fuci l
clad damage in the evenc the core is uncovered by the loss I
of coolant.
f b.
Is the equiptent required for[bt Standby [ } Cold Shutdcre [X]Both 9. Pertinent Feference Design SIrcifications: CE VPF No 2891-48-3 j s L j Fcferer.ce: 90 Filc No. 02g /y 7 SARGEffT MUNDY j' -,~...L i -m-cu.a,mw_ t_gr;%); s 7 . _., _ _ ~ ~,
n D w m::mamm-. - - N LN 7 (~ III. Is Equipmnt.3vailable for Inspection in the Plant: [X] Yes []tb v.; y b h Conrients: il r L 1i a I [I IV. Equipmnt Qualification Method: Test: 1 L Analysis: X Chination of Test and Analysis: P d;8 Test and/or Analysis by (name of Cognny or Laboratory & Rc: port tb.) V. Vibration Input: h 1. Ioads considered 1.[ ] Seismic cnly 2.[ ] Hydmlyna.aic only 3.[] Explosive ') only 4 _ [L 4.[ ] Other (Specify) 5.[X] Cor:bination of 1&2 i, 2. Pequired Pesponse Spectra (attach the graphs): 11 f) [ Craphs are attached ,, [ ) 3. Patuircd Acceleration in Each Direction: ( a4 t hl = h2 = V= t VI. If Qualification by Test, then Conplete: j r 1. [ ] Single Prequency [ ] Multi-Prequency. y 7 j 2. [ ] Single Axis [ ] Multi-Axis j
- l. -
1 3. Prcwy Par.y: ] f j L 4. TRS cnveloping RRS using Multi-Frequency Test [ ] Yes (Attach TRS gra t.1 [ ] tb fj I( 5. q-level 'Ibst at Jlt n hl = h2 = V= 9 i 6. Iaboratory tbunting: lj .) ) 1. I J lb1t (tb. Size ) [ ] Weld (Inngth )[ ] f f-a s [ ] tb [ ] tbt Applicable f' I 7. Functional cperability verified: [ ] Ye' f e 8. Otner tcsts. performx1 (cuch as fragility test, including results) f,1 t ijt <j
- j.
-tI j -sal 1GE'T eLEf)Y
Reference:
D'D File tb. 028197 4
- C N OIN E;n c t] '
()t h' M c v **3t*% m r u=,,v w g m r~r m u5g y s y m ;y y 3 m y g g r y m m g x ly h .m f y 7-
D -= ~ t O{! n VII. If Cualificatica by Analysis or by the Cc:rbination of Test and Analysis,that Cocplete: 1. Euscription of Test including Results: I I i 2. 1bthod of Analysis: [ } Static Analysis [ ] Equivalent Static Analysis ~[X] Dynamic l Analysis l [ X ] Response Spectrum [ } Tim 2-liistory a l t i, 3. bbdel Type: (X) 3D [ ] 2D [ ]1D f l j IXj Finite Elenent[ JBeam [ ] Closed Form Solution SLSAP 09.7.130 - 6.6 f 4. [ X] Ccaputer Codes: t Frequency Ringe and tb. of nodes considered: 7.82-140.5 cps; 25 moder., [ ) P.and Calculations f 5. Damping: 27. for emergency.17. for upset conditions. p f Proper spring ccnstants are ) hs h 6. Sui >; ort Considerations in the mcdel: computed and applied. F f 7. Critical Structural Elements: Coverning Seismic Total Stress k i, A. Identification location Pesirnse Ombination Stress Stress Allcvabic! I l l h See a ttached table for 7-A. & 7 - B, dn a i g i i i i f Effect Upen Functional; i B. Pax. Deflection Iccation. Operability j l I ) I i 1 I. L l u)a i c I 'l 1 _{ SARGENT t LUNDY {i., F Pcference; DD File tb. 023197.,_ . c m. ;, Ame.wvxsmummenww:.=utusammsz: Tic asusrfx: TNicInumsausr:Lwsr.ams,; urn 3 w '-
~ I '~\\ (d ' a .l t .._..I_'.._ _ _ _i _,!,_ ___.'___.i_. r! .i __.!....I I. l 1 i I l_ l { l I i i-I I ! -[ I ' EVALUATION AT CRITICAL LOCATIONS .!...._. ___,l ! l i f i l. ! { e q - -- 1... ___.i.,.. _.i _ _,i ..e t I LOCATION CALCULATED ALLOUABLE 1 { I 4 i j r Motor Stand i + 4 t .t__ 5252 psi, 30 0 0_0.. ps i . i i _. '. _.. i _ 7 _ w.i._;I I j l l i i l p. 1.._. l _ _ n _.i __ !_- 2_ i I l-I l t i _____p_._._. + q'. i I 7 4 4 9 p_s_i__,.._ _ __60000..p_si i , Motor Bolting...7_ k, i, .___.t.. : _.=__., _.,e __.i _ . _. _.r: - r-- M, -- r - i l I l I l i i f i I I f + i t l l t i 4 b ....__.__'...._____.'....!__I l l -- 5000 p_si .__ - _ 0,_5 4 p.s i - n Motor Lower _E.ndshie.ld... _,' .1 l 4 i i l I i i 5 .~._,._1 I O . Suction _B_ a.rrel Shell..__:. _ _. ' _ - -' 3 1, 8 0. p s..i.._. . _3_7 8 0 0.. p s i '. _'... ..t i [! i l i t i P 1 i i L _.i _.! _. !. ! _.., s -,1.-_.._. Suction Barrell Head /P,in } I i i i j ' Interface. 5 0_2 4 ps. i.., _ 21000 psi. + _. m._ i 4 e l i i l _.. _ + _. -.-...-_-._w--. ....._ _._.i_._.i I ._ _ a -_ i 4 1 i Pumn First Stage Casing, i i 2446 psi 1500bpsi . _. __ I I i Min. Section i i i i l . __.i. _.i. : i i ' - _ _ _i i l Pump Series Casing, t Min. Section [ 3bO[ps j 15000 ps ] G s
1----.----------J--"-----------
2 d j -4 Pump Series Casing, Bolts 5617 psi 30000 psi i l-b i I .... _. _._i __.'.__ _.. l 4 .H
- Pump Top Casing, Bolts 5592 psi 30000 psi.
._.l _ q_.+ .. p _ _p ___.i ; I Stuffing Box /Disch. Elb'ow I r, Interface. U,l ~ 62900 psi 63900 psi . Discharge Head Bciting and 21676 psi 60000 psi) f F Thread Engagement 7978 psi 30000 psi I. s s t N...............
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- a. -.
= i y t l N i -.___..I I I~ !.. '.. ' (' CONTINUED)* I l l I .I I. l I a l j l l i! i 1 EVALUATION AT CRITICAL' LOCATIONS. _._.!_.. i I , y.__;-_ .m I i t' I l 't j- - _ _... _.! __.!_.'_.'.7,_ _..i.__.i._.!. LOCATION CALCULATED ALLOWABLE g 1 i _._.y. ..__..p...._.- ._r....- .m. i Foundation Bolts 12730~ psi l 35000 psi i l l Discharge Column 6101 psi .30000 psi I l --- - r $ 6----- , -- r - l 4 i _..,.f__ - __ _ ____ p _.! _.. -___..____3.__i 1. !. L ! i i i l l 2..._._ ' ~ ~r. Discharge Column Bolting a.nd_ .._11..112, psi 60000 psi 7 Thread Engagement-- - . ' _.. _ _..4 2 2 9 p s i,...... . 3,0000.. psi O e i i i t l i I l -__.__._____l'.__. I i I; al Pump Shaft at Min. Section 5838 psi _.r 17500 psi i i 6 w _..!__ i .t _ _, i _$.. __i i ,._ _....- L_, -11 ps,i, '20 psi i i l_,_ ' Pump Shaft Bearings _ _, 1 e .__..t_._.._._.. '__r__. i i i i m. l I r, l 2287. lbs.. ; __ s _ Motor Upthrust Load. _0.; _7__... i I ..I _. I I .._._._~i___..I_..._' e. . _. _. _ Motor Continuous Downthrust. 8 .. _ _ _}'_ _. _ - l l i i . 1 t
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i i } i t i 9 ,i Load ..a_,__..._._.
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4380.lbs__ 22500 lbs._____- t + 1 g .t y ( _.. Pump Pin to Support Reaction ..9789.lbs.. __.14650 lbs i 1 ) u j s E 5 f. Relative Displacement Between _ _. _. i. ;_ . l, _d._i.1__.j .a ) Shaft-& Throttle Bushing 0.008 in _ 0.009 in ... _j . j. -' .. _ ; __. __i- . ~ _L _. + y.. I I' Relative Displacement Between 4 I Shaft & Mechanical Seal 0.0006 in-0.03 in I-Oi i -ew-h.-e ..-.u.. ___...-e.e_ ......<S..u. ..-.4a .e.._m e .-.O.._. . - -.=..*- = ' ++= g ...u y._..._._...__. .__1.._y.-___...- i ~ e - jj I 1 m
CLf"j {!* CO..MO!!I."CALT!! EDISTI CO".PA!!Y Fr.OJ.7 LA SSILF m"'rY - 1 n 1J00t'O. 85K}l j Q ".awa J &-u u y' e. r.f,T"'7?{ {""PT."? cgg;;m gy y..im,,.,. g.;g,,g w o C"aXC'.~- ~ ~ CYZ 3 C';*2? 'M - CR'dn'k-4-:':~D' I C7 m p's E Calc. No. E M D-O.2pN I I O Rev: 40 Date: 0.2/o /
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# M I I ~ Proj. No: File No: EMD- ' *'^" I ' d I I s Page 750t /6f J'~mf ddfA'Cf lH 0El of ~ 200 100 50 33 20 10 2.0 1.0 20.0 i)iii siirou aqini - 20.0 1.ii un na i i i ein u n ai-gi n i ni i.a i i 15.0 l 15.0 ~ 10.0 10.0 8.0 ~ 8.0 i i I i i 6.0 1 I ~ 6.0 4.0 4.0 3.0 ~ ~
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c',3 ~ 0.3 o,2 0.2 0,1 s g 0.15 O.10 h.---.. 0.10 ' i l-0.08, 0.08 ~ I t. i I 1 i Ii i i l I i-b 'l> i I > > l > l ' l ' ' ' 'l 'l Ll" ".4 _ _ _.'_I ~ } Il 1 I i 1 0.05 n 0.0s 1 .02 .04 .06 .1 .2 .3 .o .8 1 V .005 01 t rwtA, 5*. REACTOR BUILDINC-ELEVATIOli : 6 73 ' 4 " 2% D'amping Itorizontal Slab NS-Eif ~ Enveloo of a) SSE + CO g LEVY-1 b) SSE + COLEVY-2 + Envelop of -(SRVm + SRV3gy) 7 b[ c) SSE + CHUG. + Envelop of (SRVy n + SRVggy)
[ ~ CL'.'l!T COM".Om.I'.ALTi! nDIson company 9, t-~ g.e W-a';"li LZ m] It *'"N] u," F.7?f.'T_r.A s,,r u g y Lg.j-,gg,sjij93j QT O i 3A l D._~.,2.1 DY .Y v'o a c.- c,;;g /n. 0/iw 2 i -. -. s.,_-m
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SARGENT & LUNDY ENGINEERS CHICAGO O QUALIFICATION REPORT FOR LOW PRESSURE CORE SPRAY PUMP Date: 01/07/81 Prepared by: Ismail T. Kisisel Reviewed by: Date: 02/02/81 l 7 'F. L. Cho Approved by: h#M b hM Date: 02/03/81 ( Yakub A. Patel i COMMONWEALTH EDISON COMPANY LA SALLE COUNTY - UNIT 1 PROJECT NO: 6093-00 EQUIPMENT NO: E21-C001 i REVISION - 00 / EMD FILE NO: 028197
' CalcsJcr LPCS., PUMP QUALIFICATION cafe. No. EMD-0 2 819 7 I ~ SARGENTt LUNDY-agpog7 g,,, o o g,,,0 2/ 0 3/ al
- NGIN3~,n 2
) g C " 'C ^ X Safety-Related Non-Safety-Related Page 1 of 165 Client COMMONWEALTH EDISON COMPANY Prepared by f/Jf(/ h_b[ Date 01/07/81 .g\\ \\J ~ Project LA-SALLE COUNTY - I Reviewed by 'b */M Date 02/02/81 Proj.Ne. 6093-00 Equip. N o. E21-C001 Approved by hi> k - [ald Date 02/03/81 k---- q j i i i a i i i 1 f INDEX I i i PAGE I i i I. Objective _._2_ ___.y II. Summary and Concluding. Remarks 2 j l __ _, _ III. References 4 __l IV. Introductior. 6 i V. Method of Analysis 6 VI. Load Combinations and Stresses 20 i Appendix - A 25 - 73 i l _. (_) . Basic Data 26 Physical Description 29 I Sectional Properties 39 Spring Coefficients 66 l Appendix - B 74 - 99 _3 j Response Spectra Curves 75 Nozzle Loads 91 8 Shaft Loads C 97 m o 2 Appendix - C 101 - 165 Stress Calculation Details 102 v
Calc 2. For LPCS PUMP QUALIFICATION Calc. No.EMD_-0_2 8 y 4 SARGENTt LU!JDY l 00,j nare 02/03/81 i c,,Q REPORT n ev. t_ C " ^ " X Sitety-Related Non-Safety-Related Page 2 cf 165 [ O U. O7/8 ,[g4[.. .((([7_ Client COMMONWEALTH EDI.. SON COMPANY Prepared by Date (,- Project LA-SALLE COUNTY I Beviewed by YdN W C Date 02/02/3f 7 -y - - - ~ Proj. No. 6093-00 Equis. No. E21-C001 Approved by % bb 4 hb.1 Date 02/03/81 lfu _LJ l I .j y L.J _ 1 I i I.- OBJECTIVE l __j i The objective of-this study is.to verify.the structural._.,_, i r integrity and operability of the LPCS pump / motor i assembly when subjected to various static and dynam.'c [ loads, and compare the resulting stresses and j i_ displacements to the applicable ASME Code allowables. l II.
SUMMARY
AND CONCLUDING REMARKS i .. } This report presents the results of analytical assess-- l i ment and design qualification for the LPCS Pump. r In order to assure the functional reliability and operabili ty as zell as the structural integrity, the following analytical efforts and considerations were undertaken: ? i 1. Perform a detailed dynamic / static analysis on a three dimensional finite element model which e. i represents the mass, stiffness and boundary z conditions of the Pump-Motor Assembly. 2 2. Meet with the loading combinations that are f stipulated in the design environment as stated in section VI of this report. 3. Comply with the design requirements of the ASME B&PV, Section III Code (NB-3200) per service levels B_ and C, wherever are applicable; and also 3 ( ! use other conservative methods of mechanics and stress analysis when nceded. d
I Caks. ror Lpcsggyp OUlillELCAT. ION Ca'c. No.EMD- 0 2 819 7 SARGENT a LL'JDY{ Ju gu, REEOItT Rev. 00 Date 02/03/R " 'c ^ o X Safety-Related Non-Safety-Re4ated Page 3 of 165 Client COM'JQ1MEALTillDISON COMPANY Pre,:ared by Date 01/07/81 / Project LA-SALLE COUNTY I Reviewed by Date Proi. No. 6093-00 Equip. No. E21-C001 Approved by Date f I i F! i i e .L ! 1 !. i!- 1 i j i 1 _.._.._ L L_2. -_ i-4 q 4. Verify the operability of.this pump by. checking relative displacement at the critical locations._ -..-_ y Based on the results of analysis as presented in this _ f report, this LPCS Pump can be, qualified as a reliable { and functional pump for_the Residual Heat Removal . ] i___. _. System in the ECCS. Final results of calculations are presented in Table 4 on Paces 23 and 24 of this report. Complete details of l analysis are included in Appendices A,B.& C given at the end of this report. _ l t a n / ) x; j i L-i ^ t i z 8 O ? s 2 ,s -__.r'
Caks. Fer r_pcg__pygg OUALIEJCAT.ICM Cak. No.EMD-0 2 R 14 ~1 SARGENT c LUNDY REPORT R ev. 00 o r,ta 02/03/8)_ GNECC n! C ""C ^ X Setety-Related Non-Safety-Related Page 4 of 165 l client COMMONWEALTH EDISON COMPANY Prept. red by Dat:01/07/31 Project LA-SALLE COUNTY I Reviewed by Date Proi. No. 6093-00 Equip. N o. E21-C001 Approved by Date III. REFERENCES I I - [l l l l l I l I h j 1 } l I I I 1 I f i ,. _. 3 . _.r _. _ _ 4 i j i i ___ _.. [ _ ) _. _. 1) ASME B&PV Code, Section III, Division 1, ,3 i . _ _ _ _.. Subsection NB, Class 1 Components,.1980 Edition. \\ 4 u_.. _y 2) Data Validation Statement l b__ _ _.. .Ingersol-Rand, G.E. P.O. # AC-765 _.. _ _. l t IR Ref. # 006-36026.- 4/21/1980. [ 3) Ingersol-Rand Drg. # D-29-5APKD86XI-K, Rev. 8, 4/4/1974. i .a f g i 4) Ingersol-Rand Drg. # F.29-APKD500X2C. .] l. .b 5) LPCS Pump Purchase Specification, G.E. S-2'45 _ _ _. h Document No. 21A9243CM-Rev. 2, 10/25/1973. ..i 6) SAP IV, Sargent & Lundy Structural Analysis t
- Proaram, i
.-j 7) Response Spectra File, LaSalle County-l&2, i x Project # 4266,4267-10, 1/22/80, EMD File No. f 027521. o g 0 8) G.E. Drg. # 234C735EB, Rev. 10, 8/28/73. 9) G.E. Drg. # 175R685 - Assembly,Rev. 1, 10/6/1965. 10) Parts and Drg. No. List, G.E. Model #5K6347XC59A. ) 11) G.E. Drg. No. 211D549AYG001, 211D803G001, 2:34C532AX002, 234C645P001, 152B6882G001.
Cates. For T.DCS pt!?in OIIAfirrTcATTOM Cdc. Na.EMD- 0 2 9147 [ SARGENT kLUNDV- ~~ c ~ ~ ~ ~~ REPORT 7 ~ Rev. nn Otte Q2/03/91 GNGINE1RE C " 'C ^ " X Safety-Related Non-Sattty-Related Page 5 of '165 Client COMMONWEALTH EDISON COMPANY Prepared by Date 01/07/81 Project LA-SALLE COUNTY I Reviewed by Date Proi. No. 6093-00 Equip. No. C21-C001 Approved by Date k1 ._. i _ _ _ _. _ h _. _.. f_ _.
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_. I ___u __ J __[ a _ ;-. _ j__III., REFERENCES. _(Cont.inued) _, e i i . _.__. _..__,_ r. l .__. ]
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s _ _ i d. _ 12). LPCS Pump Manual,. Spec..No. J-2500,. Project No.... _ i ___. E j _ L. _. _ _ . 4266,4267,.VPF # 2981-192-2, 3/23/1976... I i j 4 . _ 7._ 4 -___..__.u.! 13)_ The. Design Report,,Ingersol_ Rand Model 29APKD5, ,,_..l ___j .__G.E. P.O.,i AC765, I.R. Order #.006 36026, VPF _i___._.... _J~ ..-._9.2981-48-3,.2/19/1973. 1 1 ..__._.._______n... ..1. _l 14). Formulas for Stress and Strain, 1 .R. J..Roark & W. C. Young,_5th Edition ._.h__._. .._ _ McGraw Hill, 1975. ..... _ _ _ L,_ __ _. 2 _ t .4 O 15) Handbook of' Engineering Mechanics _, f. i i W. Flugge, McGraw Hill.. ___j i
- 16) _
Microfiche Copics of SLSAPIV Computer Output's. . _ Given at the end of.this report - Original Copy). j ( } ._._.._) h e 00 l j e ( i I J j i p t 5 .e_- y
--PUMP QUALIFICATION Calc. rio.EMD- 0 2 819 7 l Ca:cs. For LPCS ~ ~~~l SARGENT l. UNDY RWORT Rev. gg Date 02/03L81_ ,,,m C"'C^ X Safety-Related Non-Sifety-Rebted ,Page 6 of 165 Clent COMMONWEALTH EDISON COMPANY Prepared by Date 01/07/81 kj Project LA-SALLE COUNTY I Revieweri by Date Proi. No. 6093-00 Eauio. No. E21-C001 Appr wed by Date l !l l j i l t -i f IV. INTRODUCTION l l i l t i i j r [_ This report identifies the analysis method and results [ associated with the evaluation of the LPCS pump / motor assembly when subjected to static and dynamic loads. j [ The analysis is perfctmed to assess the adequacy of [.__ the pump / motor assembly design when subjected to ___j i [ static, seismic and as well as various hydrodyna:'ic I loads per project specification. A three dimensional lumped mass beam finite element _l i 1 ,I model of the pump /mo tor assembly and its support is j E_ developed and dynamically analysed using the response ) spectrum analysis method. The same model is analyced due to static nozzle loads, pump thrust loads, and dead weight. Critical location stresses are evaluated and compared with the allowable stress criteria and i critical location deflections and accelerations are j l checked to evaluate operability. This report i [ summarizes the analysis method and presents the details j of the finite element modelling and' the associated _j results. ,O 8 g V. METHOD OF ANALYSIS 1 4 As stated in the previous section, a three dimensional finite element model is developed for the pump-motor assembly and used in the analysis. The merits of using this approach are three fold: (1) it represents the correct distribution of mass and stiffness for the ,'j determination of natural frequencies, including higher modes, (2) a complete dynamic analysis may be performed to determine the loads using this model, and (3) it
7... Z LPCSiPUMP OUALIFICATION cmc. No.EMD O 2 819 7 ,3.. Cates. For : 3 SARGENT&LUNDY-REPORT Rev. 00 Date02/03/81 ~ CN3tN231. C"C^ X Safety-Re:ated Non-Safety-Related Page 7 of 165 Chent COMMONWEALTH EDISON COMPANY Prepared by Date 01/07/81 Project LA-SALLE COUNTY I Review?J by Date Proi. No. 6093-00 Equip. No. E21-C0 01 Approved by Date i l i p L.. L_.l Q ;_.__' #. {. e ; _ p -l 1 l l l l l l j i l _ L pl. 7..-. __ -.L 1 1_d' _. I a 4 4 i
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__ Lcorrectly determines how the: loads are distributed l through each load path _.in the statically _ indeterminate __ _J 1 J~_i_ __.. Portions of the strueture. p__._ j __.,_i i I i j ! __ I i..i i i t ?- i_ l _.L_.__* ._ i. .d.. To qualify structural integrity _and. operability of_ L! L i this Seismic Class I essential, equipment,.i.t was decided that a detailed finite element.model.as indica-i g ted above is both justified and required. The model.'is detailed enough to represent the actual mass and stiff-i ...____. _ ness distribution resulting in,the three advantages I i _, _ L;,_ m_._.. discussed before.. _ _,_,j i =. = _._.- L-.. _ _ rhe pump / motor -assembly and some _ details of the pump
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re shown in Figures 1 and 2. The schematic representa-tion of the model is provided in Figure:3. Essentially, I .the model is a_three dimensional lumped mass beam ,,_j. element model, capable if accepting loads from the _ _] vertical and two horizontal directions simultaneously. j [ _; _ The three parallel beams of the lower portion represent [_, the centerlines of the pump shaft, bow 1 casings, and a i ~ ,i i. suction barrel shell, and actually are superimposed on top of each other. In other words, the nodal points i c indicated by dark circles have all the same X & Z j [. coordinate values. This technique results in-a model 2 that is symmetrical in the two horizontal directions and i may be used in a three dimensional analysis. The discharge head, discharge nozzle, motor stator and rotor g , are also modelled with equivalent beams and lumped' masses as defined and located on the appropriate outline draw-ings and other references. Pertinent drawings and. O, ceicutetions reserdine modet eroverties are eiven in Appendix A. Model has a total number of 105 nodes, 97 beam elements and 16 boundary elements. S&L SAPIV
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Cates. Fct T of g pmMID TlT F TCIMOy Cale. Ma.FEDd 7 H I 91_ ' SARGENTmLUNDY' R:v. 00 Date 02/03,,31 nEpopm anwne x. _f Safety-Related l Non-Saf ety-Related Page 11 of 165 C ~C ^ " Client CnMMON E ETF EDT90N C O?.fp A N Y Prepared by Date 01/07/81-- 1; Project T.W T.T.E COUNTY T Reviewed by Date Proj. No. 6093-00 Equip. No. E 21-C0 01 Aaproved by Date l l l l i i i { l l computer program is utilized for.both dynamic and f static analysis of the model. l' __ l The analysis is performed in two distinct steps. First, a modal analysis is performed using the I Subspace. Iteration Technique and all eigenvectors _l are saved on a permanent file for subsequent analysis 'with various dynamic loading conditions. Twenty-five modes were considered in the analysis, with the highest { j frequency of 140.5 cycles /second. This frequency is _j f high enough to cover the ZPA of all applicable response i spectra (both seismic and hydrodynamic series). Table l _ on Page 12, gives the frequencies of the model. As I\\ can be seen from this table, the fundamental frequency V ~ of the equipment is 7.82 cycles /second, justifying the need for detailed dynamic analysis for this flexible equipment. l l 4 Second step of the analysis consists of applying various dynamic and static loads to the model and investigating the structural behavior of the pump / motor assembly. 5 Response Spectra Analysis method was selected for the m dynamic analysis of the assembly. Response spectra I curves for this analysis are conservatively developed by enveloping the EW and NS curves for horizontal spectra and wall and slab curves for vertical spectra at elevation 673'-4" of reactor building. This enveloping process is performed for all seismic and hydrodynamic spectra curves. Sane horizontal spectra (enveloped) is ) applied in both horizontal directions during the analysis. As an added conservatism, for the emergency load combina-tion, envelope of the following three load combinationr is used:
l a' Muac# Cafe. No.EFD-028197 $O~ Catet For 4 T' SARGENTA LUNDY- " ~ - * - ' ' " ~ C~ ~ n, 00~ Da,e 02/03/81 IENGINMRL Safety-Related Non-Sifety-Rchted Page 12 of 165 "'C^" Client Prepared by Date -. _. d Project Reviewed by Date .~ Proj. No. Equip. No. Approved by Date l l t i i I. i._ L. I i__ i J.. i. _ i. _T~ L _ i i. i.. i _i .l. ! -. _ y_j.. _ j.-_ j L_.L_--[ l i I TABLE 1 - EIGENFREQU.ENCIES --_,i.J-I t l 6 6 P I il 6 .i +_ " ~ ~ l i I I PRINT OF FREOUENCIES ~ ---- { { - - "--"l MODE CIRCULAR NUMSER FREOULNCY FREQUENCY PERIOD Tot.ER ANC E I = "-'~~5 (RAO/SEC) (CYOLES/SEC) (SEC) 'j - r - l L I l l k ^ -1 1 .4912+02 .7818+01 1279+00 .6705-08 '- r - -- l-L- ~
- l I
j 2 .5352+02 .8518+01 .1174+00 .2559-00 i
- --+
3 .7308+02 .t163+02 .8598-01 .3421-07 .i- { 1 .I 1 4 .7600+02 .1211+02 .S260-01 .2253-07 l-.L-p r-.--J i j 5 .2167+03 .3450-02 .2899-01 .1594-07 L -- 4 L 1 i .i i l --- -- - p -- i 6 .2173+03 .3458+02 .2892-01 .1240-07 . ---pJ i u l { 7 .233S+03 .3717+02 .2691-01 .1848-07 .l- _ -. L r I -~ ~ 1 8 .2590+03 4122+02 .2426-01 .2935-07 j. ;_ __..___. b/ 9 .3729+03 .5935+02 .1685-01 4124-07 6.u a. .7 - -+ 10 4034+03 .6421402- .1558-01 .8730-08--
- J
_____.!--,.___i__ml ~5 l l l l ---L-'- 11 4605+03 .733O+02 .1364-01 .8963-08 ,.] 12 4825+03 .7679+02 .1302-01 .2232-07 . _4.____-__- i -- + - i - - - - 13 .4923+03 .7835+02 1276-01 .1750-07 L _ 2_. i 14 .5284+03 .8409+02 .l189-01 .1954-07 _. -__, __. L_ ) _ _ J-n 15 .5918+03 .9259+02 1080-01 .3988-07 16 .5910+03 .9406+02 .1063-01 .3304-07 p-- - -. - - as t 17 .5957+03 .9481+02 .1055-01 1984-08 - - 4, O ^ h E 'f- -- 18 .5962+03 .9489+02 .1054-01 .2878-07 o 19 .6201+03 .9869+02 .1013-01 .1167-08 g F - -.- 2 20 .6219+03 .9898+02 .1010-01 .3537-08 } i l 21 .626G+03 .9973+02 .1003-01 .2506-07 22 .6269+03 .9978+02 .f002-01 .1471-07 _1, i 23 .643O+03 .1023+03 .9772-02 '.3082-07 l s .-..__3 l 24 .6845+03 .1089+03 .9179-02 4870-05 j 25 .8828+03 .1405+03 .7117-02 .1305-07 l r o .~.._ l
Calct Fo< r'~;LPCS; PUMP QUALIFICATION Calc. No.EMD-0 2 319 7, ' SARGENTRLUNDY-rx:w:t. Hev. 00 Dat, 02/03/81-REPORT c " *C ^ " X Safety-Related Non-Safety-Re!ated Page 13 of 165 Client COMMO1MEALTH EDlSON COMPANY Prepared by Date 01/07/81 ( Project LA-SAL _LE COUNTY I Reviewed by Date Proi. N o. 6093-00 Equip. No. E21-C001 Approsed by Date I I i l I l l i l l I i i _ -. b. . a) SSE + CO J LEVY-1 LEVY-2 + ENVELOPE OF (SRVALL + SRVggy) l b) SSE + CO c) SSE + CHUG + ENVELOPE OF (SRV + SRV.SY) i ALr a ..j u l . _.J Damping values of 2% for emergency conditions and 1% for _ upset conditions were adopted. Response spectra curves .l for emergency loading conditions (envelope of a,b,and c L__ mentioned above) and the tabulated values are given on i i t. Pages 14-16 and Tables 2 & 3 respectively as an example. All of the response spectra curves are included in 7 Appendix B. _ _j j. .y v For the static analysis of the pump / motor assembly, [ action of thc following loads are investigated: t J (1) Nozzle loads, obtained from the analysis of the [ piping sub-systems attached to the Euction and 4 [ discharge nozzles, i i z j (2) Weight of all the metal components and the water inside the pump, c O (3) Internal design pressure acting on pressure boundary components, i (4) Pump thrust load, resultant acting on 90 elbow of discharge head. i / Nozzle loads obtained from PIPSYS outputs for i subsystems LP-02 (discharge nozzle) and RH-07Z (suction nozzle) with appropriate piping diagrams are* included in Appendix B.
Page 14 9 Q,fyi*1_' ' CO?'".ON.W-ai.TH EDi.~O'I CO:1PM;Y
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.Li.2.J'.3C.12M{! nfv 7? 6 q FI" t U p.,.: c 1 c..w .c, e e,,... n.,.... f . h'_ n= -, _, - ~ ..a C ' C .'- W i' J Q{IC' TID Oy7'(77-).1-,, ~_ t,7,z.y;6C-MT 2 / C7.2 7 alc. No. EMD-e>N& u.,. m o l Rey: su Date' f 5lo */U w ,. ; ma l l Proj' No %^.'s -Jo File No: EMD-02 W I [- l I I = Page d of # # rrc:m. crs 200 100 50 33 20 10' 2.0 1.0 20.0 iiTT iiis n i imm ou E m. i i i J > > i i i o m .u. o u o 4.- i i_ 20.0 15.0 - 15.0 10.0 ~ 10.0 1._. L.L. ! '--._. 8.0 8.0 ~ L ! I ' l J. 1 i i R 6.0 I--.J-.-- . 6.0 '~ 4.0 , 4.0 I 1 i 3.0 3,0 a 4 J ~ 2.0 2.0 /.]g t .I 1.5 i r r__ \\l 1,; N N 'y /' i 1_.___-_---{. 1.0 1.0- / i q_ j n.a _,_ 7 .p ,/ { l L.. , ;. _L; ,3 o.3 9 h 0.6 2-h--NM l3-M I 0.6 ) t -{_ 4 W4 ,l \\ s 1 u ,N 0.4 n a,4 g,3,. .- _.E O.3 5 t l. o,y. 0.2 0.15 o, y r, ) 0.10 O.10 - - - -t-2 4e 0,08 __i. L._p j _ j. .L-j _ _._1 H _. e 0.08 CT-ZI~~~l~~~ -~ I-i f~iTI L' I. ! i I .i o,o;Iu.l.1a.L: 2mh4iw.:.duid 1 ! : ! 1 b,I.tu. d.u.ukdda.m bug _.!.E O. 0 5 i'> . C O '> 01 02 . G.1 .G6 .1 .2 4 .b .8 1. / inh, se REACTOR IlUI LDING-ELEVATION : 6 7 3 ' 4 " 2% ~Dr.jizig !!cri~ ontal Slab NS-C.' z Envelop of a) SSC + COLEV,-l p,pg b) SSE +.COLEV.. 2. + EnvolOP of (SRV
- SilVLSY) 1-ALL g7g c)
SSE + CI!US. + Entelop of ( S RV,.,;,n + S RV3gy) m
i j.prl,4 *!edi N py.y ". .. - CLO.T_ coWfne.LTil mLsuw etmMwk ~ $;OUTTagaint.y:vcarg7y - m,,Jc3R>.4pMQ;.1 [. t.:,fs.wt.n~J d el kwJu d g :.c.g g, g,,,,.,f, g _ g..... ff,, q f f,., ~.. cg w :O c<,yf;! m,_ pqy;f,n-secgicc :>. 07__y _ 2. C CC::=': J / O Calc. No. EMD-e://97 '" '*- I # I C' Rev: 40 Date: os/o 3/h m"inSI *l"I "^" I"' Proj. No:' " 2 /l,6 - o o I I File No; EMD_nfN7 { Page M of /4f ,,, m 200 100 50 33 20 10 2.0 1.0 i i n i u n u.i o u i m% i i i. 20.0 20.0 _. iii i iiii .u i u m u. nei im on i ii i,.ii4 15.0 15.0 7 ~ 10.0 10.0 _ ~ ~ 8.0 8.0 _ I 6.0 6.0 4.0 4.0 ~ l.0 3.0 ~ J 2.0 ,a 2.0 l 5___...____.._.4._ N -t 1.5 ~'% i <; (J y [ / [u/ 1.0 l '. 0 h-- 7 j y p 0.8-- j 0.8 i dq __ --{ g g _f i NI 0.6-0.6 b ;~ (e-cf ~ I 0,t [ L 0.4 E E / =- l # 0.3 ~ 0.1 0.2 0.2 i____.. _.. 0.15 0, i r, 3 0.10 ~ 0.10 i t 0.08 0.08 [ I-I 4 !~ 1 i-r 1 " ' 'I >>'b'ikiilt i n n!"u)uu' r i o '.ilIi 0.05 d ~"1 .nu 1 iii au ii> .'01 0
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.02 .04 .06 .1 .2 .3 4 .6 8 1. . C O 's vn't se. e REACTOR BUILDING-ELEVATION : 673'4" 2% Damping Vertical Slab Envelop of a) SSE + COLEVY-1 k EMD d b) SSE,+ COLEVi. 2 + Envelop of (SRVALL + SRVliSY) _.02752. c) SSE + Cnua. + Ehvolog of (Savy,L + Sav Sy) n _T
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.(Q Calc. No. EMD-dff&f Date: s: ctv. no. o 1 l l ftM-e/e3/// Rev: so o em /. r_ al i Proj. N6: File No: EMD- 02A'f7 mmm. l c.s l I I 1 Page n of /W 0 t rrnaxy ces 200 100 50 33 20 10 2.0 1.0 .20.0"y.ii.i i i i i: u i s uu..m n o un 'a u i r1 e i i i i i i n u n n o u n tra'ra, i ,i,-*20.0 l 15.0 ~ } 15.0 10.0 - 10.0 ~ 8.0 8.0 _ 6.0 l ~ 6.0 4.0 ..--.~.- 4.0 i 10 ~ ~ 3.0 ('2', 2.0 2.0 [ 1.5 i / s /' / __f. ' t 1.0 1.0-- / t I / I 0.8 n 0.8 [l j 7 M.J ~ 0.6 O.6 j- /I \\ /1 \\__'_ e a.g -13 1 \\ . 0.4 M 3 n,3 ~ 0.3 J___ _.. _ 0.2 o,2 ~ ~ 0.15 o,is h h. _] 0.10 0.Io 0.08 0. 0'8 1 1 I l _' ' ' ' ' " 'I n" ' ' ' ' ' " ! " " !" u. i n u. " "I "."6 '. 8 1. [ 0.0S i 0.05 T (5 1 '.' 0 1 .02 .04 .06 .1 .2 .3 4 / .005 rw ,c. REACTOft 11UILDING-ELEVATION : 6 73 '4" 2% Damping Vertical Wall Envelop of a) SSE + C0ggyy_ y SSEa+ COLEVi. 2 + Envulop of (SRVALL + SRVASY) - @d b) 0 Elf ~c) SSc + Citua. + Envelop of (Sav3tt + Savnsy)
F__________ c2 ci. ro, SARGENT t LUNDY . LP. cup 2;P_20,3tttCar_I_os nEPOnT caic. No.Eno- 0 2 n 19 7 Rev. 00 Date 02 '03/JLL cumuxu C"C^' X Safety-Retared Nan-Lf tty-Reuted Fage 17 of 165 Client CO}D102MEALTH Enic;On COMPANY Prepared by Date_pl/07/81 () Proiect t.k-SAT.T F COUNTY._.I Re<iewed by Date Proi. N o. (;og1_00 Equip. No. F21-c001 Accroved ty Date II t i i l i i i i i -_a< u .1 i I L m _., TABLE - 2 ,_ l __,_ 4, _y ACCELERI~.lON SPECTRA - HORIZONTAL - i _1 l (NS - EW ENVELOPED) .,_______} i i REACTOR BLDG. ELEV. 673'-4" I .,...,._...._i 2% Did4 PING ENVELOPE OF EMERGENCY LOAD CONDITIONS .._.__._._,i Period Acceleration i f--- 1. 0.005 0.55 - - -._j .2.. 0.010 0.58 I i 3. 0.013 0.65
- 2. ___ _ _ ;
4. 0.016 0.65 .__.._.} r__ (O 5. 0.018 0.79 V j 6. 0.022 0.83 7. 0.024 1.07 8. 0.026 1.08 h .9. 0.030 1.30 10.. 0.040 1.30 1 11. 0.049 1.20 .. _ j J 12. 0.060 .0.80 i j 13. 0.072 0.70 14. 0.075 0.02 o .15. 0.085 0.86 g 16. 0.107 0.85 17. 0.123 0.74 18. 0.135 0.74 { 19. 0.140 0.69 _ _j 20. 0.170 0.69 21. 0.180 0.57 bq 22. 0.200 0.57 23. 0.230 0.C6 24. 0.250 0.70 t P
SARGENT'~ LUNDY ~ ~~ ~Cse. No. ' EMD-0 2 819 7 Catc For LPCS PUMP OUALIFICATION REPORT Rev 00 'loate 02/03/81l' unwn=uz. l X Safety-Related N o n-Saf ety-Related Page 18 cf 165 l C **'" ^ " Client COMMONWEALTH EDISON COMPANY Prewed by Date 01/07/81 Project LA-SALLE COUNTY I Rev;ewed by Date Prai. N o. 6093-00 Ecaio.N3. E21-C001 App <oved by Date i t i j i I i l i I 'l TABLE ' k i i i i i '. ;l i i Period Acceleration ._I i __[ 25. 0.350 1.41 26. .0.375 1.41. . d' ..j 27. 0.420 1.85 _ i..... _.._ _._. q 28. 0.470 1.85 ... _. _. _._ _ j 29. 0.500 1.50 i 30.. 0.700 1.17 8 31. 0.770 1.18 l i + 32. 0.800 1.30 t [ _..._ _ 33. 0.900 1.30 4 34. l.00 0.96 . _ _. ] V (__._ 7 i t. i ~ h t p C 8 e. g ... _ ~ ~ 0 E r i ) sv
~ Ca;cs. For LPCS PUMP QUAL 1 FICA'I' ION REPORT ' Cate. No.EMD-0 2819 7 $ ~ SARGEf1T LUNDY .', 00 g,,,02/03fg1 ~ g J G N Gs NOO 542, X Safety-Related N on-Saf ety-R elated Page 19 of 165 "C^" Date 01/07/81 l CIWnt COMMONWEALTH EDISON COMPANY Prepared by Project LA-SALLE COUNTY I Reviewed by Date Proj. No. 6093-00 Equip. No. E21-C001 Approsed by Date l I l I i I I l l ._. J 1 r ; - __ l I TpBLE - 3 i i i l ACCELERATION SPECTRA i + _. VERTICAL _. __, _, _ _ ' _ _[. _ _ _ g (WALL AND SLAB ENVELOPED) . REACTOR. BLDG. ELEV. 673'-4" _ _.. [. ! __l 2% DAMPING [. _.__. _... ENVELOPE OF EMERGENCY LOAD CONDITIONS ______.J, Period Acceleratioti f ~] t i 1. 0.005 0.35 __j 2. 0.022 0.40 l 3. 0.028 0.64 l O [E_ 1 .4. 0.070 1.40 5. 0.080 1.73 6. 0.110 1.80 _i - 7. 0.165 1.00 8. 0.175 1.25 9. 0.185 1.30 l N 10. 0.200 1.25 i 11. 0.220 1.15 z 12. 0.270 1.12 5 13. 0.360 1.50 n o j 14. 0.400 1.52 5 15. 0.440 1.50 16. 0.460 0.67 17. 0.520 0.66 18. 0.600 0.60 19. 0.700 0.53 20. 0.820 0.53 U 21. 1.000 0.42 e
u c ,a: cas. For acS PUMP ovALIFI_ carton c,ie.No.- Etto.028191 SARGENTELUNDY ~' ~ n wnd M ORT Rev. 00 Dat. 02/03/91 C "C " X Safety-Refated Ncn-Safety-Related i Page 20 of 165 Client CO51:10NWEALTIL_ EDISON COliDApy Prepared by Date 01/07/g1 Project q -SAT.T.E COUNTY I Reviewed by Date Proi. No. 6093-00 Equip. No. E21-C001 Approved by Date .i __. _.. L _. _. ._.a 4__1 !j__4__._The. vertical. component;ofthethrust.on.elbowis. I applied. vertically, upward at node _47. The hori-I _._._b .._ _........zontal component.of the same force is not considered _. l .1. [ for,this evaluation. I.t is assumed that.this force _ _, . _ _,. _1.. [ is_not considered for this evaluation... It is., il i assumed that this force is_ totally transmitted to ' .. the. connected piping sub-system by discharge 2 flange bolting.and absorbed.by the piping suppcrts. _- t _.i_.. _. _... .__7.. l + .V I. LOAD COMBINATIONS AND STRESSES _ p_ L_, 1 f ..p_. . L_.. _ __ _., a y The pressure boundary components of this. pump / motor ._ _j F-~~-'~ ~ ~ assembly are classified as ASME D&PV Code Section III , _ [_ ! Class 1 equipment,.and must comply with the rules of Subsection NB. Stress integrity is addressed in terms _ of these code rules wherever applicable. At locations where.ASME code does not apply, general methods of stress anal;. sis and principles of mechanics are used. l p -. - - ...a [ Following load combinations are calculated.usin.g the. i [ results of static _and dynamic analysis: e } l 8 i 1 ] Upset condition: 1 o l _.__,.a._.._. N + OBE + SRV. 3 ? N i Emergency condition:- - )>- -- L l 'SSE + CO !j _ N + Envelope of t SSE + CO + SRV ,SSE + CHUG + SRV, ~l O (n = " r= co#aitio==> I i j ~ .)
i Cafg. For JPr8 PMMEL.QUALTFlCATTM . Calc.No ma g 3 L. SARGENT 3 LUNDY- , x,u x Rev. 00 Date 02/_03/91 REPORT " ^ " y Safety-Related Non-Safety-R lated Page 21 of 165 Client COMMONWEALTH EDISON COMPANY Prepared by Date 01/07/81_ k,1 Project _LA-S AI LE COUNTY __I Reviewed by Date 1 Proj. No6 0 9 3-0 0 Equip. N o. E 21-C 0 01 Approved by Date i I l t i t . -. L ; _.__ L ' i t l t 4 i i l i l l l The forces and moments obtained for each beam j element are combined according to the load _,_ j combinations mentioned above using absolute sum L method. These combined loads are then used to calculate the component stresses at critical locations. Evaluation of stresses were done according to the general criteria set by sub-l section article NB-3200 of Section III Code for i service levels B&C whenever applicable. Specialized stress analysis techniques are also i used whenever necessary. _ _. ] For all critical locations except one, namely _j (] the stuffing bax/ discharge elbow intsrface, the stresses evaluated as a result of emergency load f, combination using service level C criteria I mentioned above, were higher than stresses pro-f duced by other load r A inations. At the inter-L face of the stuffing box / discharge elbow, using upset Joad combination and considering secondary n i stresses, produced higher stress levels than any a: Other load combination. Highest stress levels at f all locations are used in comparison with the allowables. B i I w Foundation bolt stresses are calculated from forces developed in the spring elements at the foundation level assuming that all bolts nominally contact the pump to transmit shear forces. (]) Operability is assured by checking loads on pump and motor bearings against the allowables and also by checking relative displacements at critical loc;1tions.
r-Ca'u. F or rPCS R L gip Iryryping Cate._N - rP D- 0 2 819_7 _ SARGENT a LUNCY R" 00 D *'e 0 2,,o m,,,0,, me c m;,~ m Non-Saf ty-Rebred Pz;e 22 of 165 C " ' C ^ y Safety-Related t Client COMMONWEALTH EDISON COMPANY Prepared by Date 01/07/61 ( b x__j Project LA-SALLE COUNTY I Revicwed by Date Proi. N o. 6093-00 Ecuio. No. E21-C001 Approved by Date i l i l l l I I i I l l n 1 1 1, A summary of evaluation at critical locations are given __ { i in Table 4 on pages 24 and 25. Details of calculations ___,___ji 4 are given in Appendix C. l I I Microfiche copies of the pertinent computer outputs are included at the end of the original copy of this report _j and kept in EMD Library. Also a set of microfiche copies l r - - -.. -q i and Xerox copies of all computer outputs are kept at the ___ 1 1 office of preparer. l i i t__ ____4 1 .. - _. ~ -.... -. .. - -. l .______i ,s 3 q) J -- l --e I {~ b 8 0 O E 5 6
. Calcs. For. LPCS PUMP OUALIFICATION cate.no. EMD-02 8197_ _ SARGENT 5 LUNDY REPORT Rev. Q_0 Date Q2 /01/31,. I c:m ocx j c -c ^ w X Safety-Related N o a-Saf et y-R e4ted Page 23 or 165 Client COf1MONWEALTH EDISON COMPANY Prepared by Datt01/07/81 I _.,,/ Project LA-SALLE COUNTY I Reviewed by Date i Proj. No. 6093-00 Equip. No. Approved by Date l I l !l i l l l l ) i i _._4_.._ .i i 2 4 1 l TABLE - 4 l l l l l t EVALUATION AT CRITICAL. LOCATIONS l._. LOCATION CALCULATED ALLOWABLE e p __g _ _ _ _.. Motor Stand 5252 psi 30000 psi _ __j l } Motor Bolting 7449 psi 60000 psi l l _._ [ Motor Lower Endshield 1054 psi 5000 psi __ :l l } ,t j_ Suction Barrel Shell 3180 psi 37800 psi j J l^ -- i -./ Suction Barrell Head / Pin 5024 psi 21000 psi Interface { Pump First Stage Casing, I 1_ Min. Section 2446 psi 15000 psi I i i Pump Series Casing, g Min. Section 3000 psi 15000 psi ,5 Pump Series Casing, Bolts 5617 psi 30000 psi + 1 Pump Top Casing, Bolts 5592 psi 30000 psi f Stuffing Box /Disch. Elbow Interface 62900 psi 63900 psi (. Discharce Head Bolting and 21676 psi 60000 psi Thread Engagement 7978 psi) 30000 psi
~ Catet For LpC3_,pt]Mp OtW.T FTCATTO1 Caf:. No. EMD-028192' SARGENT tLUNDY CN2ifMERS n,y. 00 g,,,02/c3/al _ _x Safety-Rehted Non-Safety-Related Page 24 ' of 165 C "C ^ COMMONWEALTH EDISON COMPANY Prepared by Date 01/07/81 Client %/ Project LA-SALLE COUNTY I Reviewed by Date Froi. No. 6093-00 Equis. No. E21-C001 Approved by Date . l..._. _.,I, l I l l _... _ I.. f._.l l .._}- ..I._. I i I I l I }. l l l.. '.. TABLE - 4 i l ._-._ g....._4 _ 1._ - a! l j l { l f i._.j I .-..m...... l l l i l I ~ (CONTINUED) _.--_.-__.L..e._... l t i i EVALUATION AT CRITICAL. LOCATIONS l l l i l . _. -.. _ + _, '... _.. I-j i i i LOCATION CALCULATED ALLOWABLE .. y J l l. Foundation Bolts 12730 psi .. _.:35000 psi ._m I I i 4 ( i 4. 30000 psi 6101 psi Discharge Column -,._ _ A s i Discharge Column Bolting'and llll2 psi . 60000. psi p 4229psiJ _30000psij _ _ _j Thread Engagement j . _ _ _.. _.. j _O _ _ rume suert et_nia sectioa sa38 eet 17soo ee1
- 1 t
l-Pump Shaft Bearings' ~11~ psi . 20 psi .l e . ~, _ -. _ - ...p.. 2287 lbs t Motor Upthrust Load 0; L Motor Continuous Downthrust 1 a i ....._1 u._ _ _. _. _ _ 4380 lbs_ 22500 lbs j [ Load 8 Pump. Pin to Support Reaction 9789 lbs 14650.lbs. O E C {_ . Relative Displacement Between i Shaft & Throttle Bushing 0.008 in 0.009 in i l Relative Displacement Between _ l i-Shaft & Mechanical Seal 0.0006 in 0.03 in o: i. i. p g. --p c,.-- .-,-.-.-~..a + --,. .4---.g.g----- ---1 w
lu., SARGENT & LUNDY Page 25 E N G I N E E R' S ' ~ ~ ~ ~ ~ ' ' ' ~ ^ ' ' ~ CHicAco I O-i I i f APPENDIX - A 2s - 73 O saS1C onTa 26 PHYSICAL DESCRIPTION 29 SECTIONAL PROPERTIES 39 SPRING COEFFICIENTS 66 4 0 G
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p, m i i v > i i ..,.__L_.-_.1. .._ _J _4 2 7,_ A = $0 32 In ' ' -. g -. __ Iz,3 : /4 12 ' % L 3 2..o;J _ ! - _+_ i _ _L / _._ _p t m t M_.._.-9__ -k_1 _4. - {, 9-m. ..' _ _. g4 l 4 6 i }f It i l i. l i ) '_ai n i l 1 l i l p f i .}.. 4 2 ff,. A.- 3 0 3 7 tC_ -_. _ ..I._._.w. n I2,v7% f2;f I, = /W 25M - =. w. -._ L.J G i t ._n-, -.---g . Ay I I t i h 5 E 1'(. w i _._NN I f f -. - Q,. Q )\\ - l i a 7. . _.4 _. g,___ ._;._.__j l r i -_...._.7_.______.. y g D l i g g _.4 6 6 3 i i 0 ~ ~ ~ ~ - * - - - ~ ~ ~ ~ 'b o I ~ - - - ' '" ~ ' ^- ~ ~' ~ ~ " ~ +' ? ~~i 5 I -- -f - .--.---.4 E 4.yo, A = 17 3s,e t s . - =. C i t,n 23. s,V,1, = t ?. 91/J. .) 'n i + i 1 ~ t +y .g s 4 i t i g. e 1 m . ~.... I I A) tv [ j - t. , - + -.. - -. i 4 \\ - ~
l:.: \\.'al kW ,-o e. ca, J' f 3 DATA VA' IDAT10'l STATD'I';T Q V e f f The data centained in this request has been independently reviewed by c. responsit,le verifier.- ghc M (9 O The extent of this verification includes: q 1. P,eviewing ar,d concurring with the nacerical accuracy k, w o g. w o of each re:orded vaiue. 6 6 00 2. A:knowles;ing that the in3ividaal colle: ting the data Z O z e.. \\). is faciliar witn the equipment and its terminology. i S.g E no-n o a: a =. a., u '3. Verifying that the reported data is the r.ost currcnt and obtained frc latest revisions of drawings. Co6-36026 2gppp--E h wJk DATE: /5 / NO DATA C0'LECTED BT:- DATA VERIFIED SY: C.Aw cm ~ -2f AE 60 DATE: 1 Co:pany 19casca - P Aur _ Pu~,p Service
- 1. Pr. g Project'Ilane LA 6 A t.L E _
G.E. P.O. ( A C - 76 *3 IR EE.F =S co 6 - SG026 9 e e o e e
s. c m ~ - T Qi.; . d.. W ECCS P.T.9 DAT A P.EQUEST , '^ Pamp Service
- t. re s Date.___
Project' II3me __ L5 %t.t.F , Hame _ G.E. P.O. f Ac - vm g co G-3 60 ~:. C-Calc. No. EMD- 0.:#97 29 Ap,c p -g Rev:vv Date: V. g g / o 3 /d'/ o.2 Pro),. No: co File No: EMD-Page s'/ of /6 S~ General Ouestians Please provide the following information: a) Thread engagement length of stud (part nutber 179A) into plate (part number 359-1). l. co rairJ c) Thread cigagement length of stud (part nuriter 17PA) into discharge nozzle p' ate (part nurber 351-1). I. c o r.t, n d) Typical thread engagerent length of stud (part numb:r 178D) into ~ casing (part num2cr 15 or IC). /. 0 0 p~ e) Are all shaf t bearings shcun on data request fort'.s?, YES O f) ifeight of purp shaft coupling assembly (part number 164). GO
- lbs, g) Weight of pump / motor shaft coupling assembly.
9-3 lbs.. h) Maximum ello<able intermittent horizontal load that throttle bearing (part cumber B.) can be subjected to. .l b.7 top ( srrADY.Ju rE
- 1) Weld size and type (e.g. full penetration, fillet, etc.) of weld connecting l
motor stand (part number 351-5) to discharge nozzle plate (part number 361-1). v3 BG-Fw PT\\ I' Maximum allcwable horizontal relative displacement be% tween part numbers r.z5 j) I and to in mch seal. . o/6 O ZL',- l l k) Tolerance must be shown with dimensions when the tolerance exceeds t 1% oT I the masurocent dimension. Has this been adhered to? Yss 1 !O O 'F D-o 7.7-.__
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,. g.3.- 2- -~ ECCS PLW DATA REQ' JEST 55 ~~ Date Ptry Service LPC6 2^t APG -L fd Projc:t 'IBoe _LA II W. - 0^ttC - cm. > co m ~~ G'E. P.0, f Ac-76c Calc. No. EMD-BIf/97 L Rev: ro Date: 42/05/// Shef t Detside Dia eter Su : arv: Proj. No: VJG4-so Shaf t 0.D. between '0" - A = U 26 File No: EMD- " 8" # I # S.7 f Shaf t 0.D. at B .Shaf t 0.D. at C S.7f Motor ibunting Fler.ge g i5 k. !b j ~ ,[ f ~ .~. D- ?:p
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1[ p'. J 1, L__.;a&Q[M o r r ? ' L _Mv y ( Dirensional Date:
- Crouc Letttien D2scriotion Distence Above *0" Shaft A
Shaft Dia.eter Chtnge 27 in. $ht.ft B Throttle Cushing Centerline 30.6 _ in. Shait .C t'ech. Seci sucLM face. 37.5' in. Sh6ft D Shsit Co.:pling Centerline (> O ' in. (btor Sund E.- Yep of Fitnpe 1 25 in. Ibtor St.snd .F flat Plate Cente.rline 38 , in. T = Average uall thichrycss of :;tuffinD box pipe 63 _in.- CD': ours DF OtA or orarfirJG cox Ap7"TI tu.clit:41tJG 6.76 in, e
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ECCS PW2 DATA REQdEST s7..; Date Pur.p Service _ Lod 6 7q Apg o,g ~ i*snuF ces-sooz6 me c. me. <.eiD o e ar ""=" O erosect raoe - Rev: oo Date: 6 > 05,4/ e C. -ic, 'c Proj. No: 9'a46 - <ro. G*E* P.O. ( _ View AA (Next Pace) File No: EMD- ~~ ~ page 57 of /64' First Stage Casing Data _ w Toe ee.u. ire D p '; [w ~~s zo, e a w. AM*** J a. tied h r.i h 'i A / [ jE L oad ^~' n , ' le s -t ^b]C
- b Di oo
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G -R>J o eo [ ~;[.~;a (i j b di 1 'i y-@ ~Q; r cAsieJG c G. O li Y >I f s ouw o E Di^ or .1mpeiler 11 s p Af ~ L ij fl. r ( f nue.Tieu oc a q usu. c.L:r'OU / y ~ cocnio ta G ELL g /~ ) f J (, Taicu t s 5 AT Hitli k> +C- >,g f s c e.,i c, e j f ~ \\ t.ower Sessa Vat. Y~ C o rd i's o u S Lo*d 20' u ^ AnoW O C z.,.f tt,%i tied Lea d _ Weicht 810 lbs. (nominaluncorroded) Casing Petal Weight (nominaluncorroded) /60 _,_ _ lbs. Impeller Metal Weight Dirensional Data //.2 6 in. A = _ _l 8. R _ in. F'= 2f.8 in. B = __ll in. G= .88 in. C = _ t 23I in. t =_ Do = S.E in. Dimensions should include S26 10' .'36 Mic h effect of corrosion, and minicum DI " _ anticipated cesting dirensions. do = 5.75 in. c ^sT J es 'u
- 4. 2.G in.
(G B
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- Quantity of tubulcr ptissages
- To p Scarino 10 4.2jT in. Top Dcaring Length 4.26
_ in. H _ 5' 6 it. nt. Low er-Bc t.t.th3 L cc.-3 Lower Sc d3 T.o f 6 T 2- * -
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ECCSI.i?.?DATAP.EQUEST Date_ q Fwp Service __ LPcs f(anc __ V Project !!are LA = A t t. 5-G.E. P.O. f Ac - % F Calc. No EMD D 22M7 29AP&O-C Rev: go Date: o 2/os/H Proj. No: 9444,00 OCG - 36cf,6 File No: EMD- , l., - Page 51 of /4f Tubular Passage .. d. Suction - Hozzle 9 i ( O 4_ ,/ / YlEk' AI e 1 Orientation of First Stage Case 9 CR!Fn7ATrod MW - t CHAT %5 DEPE/JpIN(1 OM ASSEMSW'1* r^ e ae -e ** wo . uaw
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^ G.E. P.D. f A c - 76 9 M -%O2/o Stage Casc Ho. 2 ~ * ~ = n Calc. No. EfdD-d r.f(j/d/ fV Rev: to Date: os/op
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R5 Proj. No: 7164 -o,o Casine' Dita - e File No: EMD-A Page s y of /44- [ h'.M T4 noninal 3 1 b' 't ~ R "'- - Scade$, m Atcoms:.n, I l? 7 - o /,3 y 4, coux,avoo3 t.ogg go p \\\\g ~ IxTtevivrtur c:Ao ~ eg Yp T1 average from 111 to H2-h.\\ y \\ ~ T CG G' h3 g2 l -T3 average between L1 and L2 4 T H4 R2 -i c N - T2 average over H1 s h1 y +/ IN-v y y s b i of vancs, n vane thickness, tl R1 - g average width of vane 700' lbs. (noninal uncorroded) Casing lktal Weight Neight of Impeller inside this Casing 13 5 lbs. (ncclinal uncorroded) H3 14 Z6 in. H4 4 ~2. 6 in. All dimensions prov.ded sh::uld Avg. Ikcent of Inertia Ig gq in.4 include effect of corrosier.. and minimum anticipated casting in.2 dimensions. Avg. Cross Section Area a Bearing ID 4.26 in. Dearing Length 24. 2 f in. R1 11 in, f of Vanes ~1 R2 S in. Vane Thickness .Wo in. R3 2.68 in. Avg. Yane Width 1 75 in. P4 6.si dn. T1 Avg. from H1 to 112 t in. 3 2 4W. h5 ~7f in. T2 Avg. over Hi
- f. O in.
4n. T3 Avg. seteeen ti r, t2 .cg in. . :-a re.. ~. .O (iii ~23, 12 /E in. T4 liominal ~ /. 7 6 in. 3.'72 in. ~ .L1 ~ 6SB in. L2
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U-Dste V ..-.u./ Pug Service - L oc's - y. . g"- am ~ .' Projcet !bx _ L A ?^t t E W - L OZCs Stage Case 110. 3 G.E, P.D. ( Ac 7GS Calc. No. EMD-6.22H7 Rev: so Date: o c/oS/// e (~) Casing D2ta - R5 -J Proj. No: +'2 4 4 - oo s ') File No: EMD-c 4 Page 4o of ydy ' T4 noninal i i 3, i L2 5 - Se,::w g Mu AucW A%E, p^. J3 <J \\ ca m 0ueus teco '7' N Igrecomtm tcxe N / x '\\ T1 average from lli to H2 T-- CG G-N y' l- ~ T3 average between Ll and L2 iG H2 q-11 4 - R2 q T2 average over H1 s s h1 L1 g / l \\. I i Y Y { . vane thickness, ~' (d R1 - c everagc width of vane \\ k. SAME /p [ STAF Casing thtal lief ght ,(noninal uncorroded) 1bs. IIeight of Impeller
- lbs, (ncr:inal uncorroded) inside this Casing in.
IG H4 in. All dimensions provided should in,4 include effect of corrosion, and minimum anticipated casting Avg. Iknent of Inertia in.2 dimensions, Avg. Cross Se: tion Area f>etring ID in. Bearing Length in. El in. O of Yanes in. R2 in. Vane Thickness in. R3 in. Avg. Yane Wictn in. R4 in. Ti Avg. fren H1 to H2 in. R5 in. T2 Avg. over Hi [3 H1 in. T3 AYg. tietMeen ll & L2 in. 74 I;;c.inal in. U2 in. in. L1 ~ in.- L2 ', ~.~--.e ~-_y ~.. ~..-. --...- .j,_;.,;_:,0 QY ' ' ' m a e m e v_a - c.. e,..og -.. ~ -
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G'E* P*D. ( - Calc. No. EMD-42//77 P.roj. No: #1.s4 -e/o s/// (,,) Rev: 54 Date: o.2 o. R5 -
- j File No: E M D'-
- Casing'Date -
c-L Page 6) of M \\.N.. T4 noninal ^ 3 l i
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l (p - Beh9, 3 J.3 y \\ conTw u e:.a s Let-0 b MC7 It4TCr.MITTEfC CAO R.. f /A _ T1 average from 111 to H2 Y CG G'h r' l T3 average between L1 and L2 '-3 IG H4 - R2 I d T2 averace over H1 h 3 d b1 L) 3 y i/ INY b f of vanes, ,s( ) vene thickness, average wid:n of vana - R1 - c ' ~ ~ ' = L k. $N b fS ]W STACg Ibs* (noninal uncorroded) Casing Ittal Height Height of Icpeller
- lbs, (nminal uncorroded) inside this Casing in.
.H3 in. All dinensions provided shculd H4 include effect of corresien, in.4 and mnin.:n anticipated casting . Avg. I'.coent of Inertia in.2 dimensions. ... Avg. Cross Section Area Bearing ID in. Bearing Length ' in. R1 in* i of Vanes in. R2 4n* Vanc Thickness in. g3 jn' Avg. Vane t!idth T1 Avg. frm H1 to H2 in, R4 in' in-R5 s' T2 A.g. c m H1 (^) i n '. T3 /,vg. between L1 & L2 _ in. g; -
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- Casing'Dat!
R5 r, File No: EMD~ 4 Page /s2 of /ds Mk' h T4 noninal g' 'y 3 l - secep, v. u Attow At'. t. =- R4 L? g \\ [y 2 0 P5-conTm u cu s Lec.; J3d 3 7 mets T7gs7 wuc p. p. v %s T1 average from til to H2 T Cd R-- H2-I T3 average between L1 and L2 T ~. ~ 1 l H4 - R2 N +\\ T2 average over H1 m-N i h1 LL M / iN\\ ( y I I i of vanes, O 1 vane thickness. R1 ~ average width of vane c L. ~ Casin; thtal Weight lbs* (noninal.encorroded) (o60 !!elpht of Impeller I'E 5
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H4 8,'2.2 in. All diaensions provided should include effect of corrosion, /.rg. Mxent of Inertia
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N Avg. Cross Section Area Bearing Length N. 7 5 .in. Eearing ID N.2 5 in. 7 R1 Il in* i of Vanes .5 in. Vane Thickness PJ 'th 6 i ". Avg. Vane Utdth /* M R2 in n'.. gg n p4 g,n j n, T1 Avg. t.re H1 to H2 _/ OiR$ 2: U M: ?H, "le"n ti t2 'f I s'""" w x in. yunin -gg ' l.2 t,6,4 in. .. to,+F C
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J 63 ' ~~ Date .. Pep Service LFC 6 c'0 6 -360 EG Ihme ' Proje:t ilme _ La~- 5AtLE-29,:P406 Calc. No. EMD- 03867 Ac 7GC ~ Rev: /C Date: 42/o3/#/ O.E.P.O.( Proj. No:' v2 fd - 40 File No: EMD ~ .~ Page 4.t of 4f _ f - - = _M^[- g ]' y ~<v () i r .s 3 v. W _\\ Qm / ] l b ~ .A l ( ~ 'N 1[c... r i p--~ v >I w )$if / J K _-~ / Part A / i .,/ c ll ) L A s Part E _ )s ' i = s V / t,! % c W' ( / 'T I b//A#' Souto P 11 in. n- - 10 7-M~, a y 0 s b 1 O ~ <26 in. Diuttral clesrance between Part 4 rind Part C e gg g 'e .m,y g
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ga',c 2 fe"1?.~ "o'i7o'3 +c-va" e. ~ Pro}. No: /204 ~ # # Shai'T COUPLING File No: EMD,, Page 6'/ Of /#-L r.m - ~ y a a s y \\ l f x (N / ,6 t-j / ~.' N / d'if C i '!fy V . (V 3 ~!L- \\ \\ A-C s l /\\ v g N B D c y [ / \\ s N O ~ L .1, D s {- DIMENSION 82. DATA A= . 38' in. E= ,36 in. B= 2.49 in.(SWtemeMh C= ,62 in. D. ,62. in. l O I a. l 44 .. x
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~~ 006-36026 .Projcet flane L A e M_t E _ 29 Apeo.-5' flame G.E. P.O. i AC-7G E ,m, Calc. No. EMD- 02hf 7 t A Rev: 0C Date: o2/o 3/// v Pro]. No: v)64. oo File No: EMD-rtw/mTOR SE:7 COUPLING _- m ~ Page 1 5 of MS~ O A A t = n m i N E ~ N, T,9 o f, [li t 6 n -c c A rTT1 i A,A y r N I! f -~ ,n j/ )~t ' D . ~ /1 0 ~ O 4 '3i\\ N!i\\' i , 31 ) N F v DIK.NSIONAL DATA A. __Q,6 in. ~~ (Bolt circle diameter) B=_ 9,6 in. C = _ 24,69 in. (Spacer piece diameter) D=_ l 38 in. (Thread engagement length) E* _ i.00 in. (Thread length) F* _ ?). 3 (o___ in. (Minicus shaft dir.=eter) p) ~- e ahn .v ; uf 3,. w...; - - mmm. a.u.. me--m.._. -, ~ .e mee-- s-o E - -
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OF INDIVIDUAL LOADS (FT-LOS) LOAD. TITLE LOAD ID FA FB FC MA MO MC DEAD WEIGitT LOAD. WGHT 43. 1530. -205. 846. -290. -1167 .,). I CDEHAtrPERCENT 08HI 243. 353. 2tt. 138 112. 189. .V SSECtJEPERCENT $511 315. 501 202. 158. 14 9. 260. SRVEf4VCtJEPERCENT SNt! 607. 135G. 520. 202. 274 725. SRVEf4V TWUP E RC ENT SN2! 458. 995. 394 15G.
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.7,o T p N ,.:'N/ ? Ik TN<. X M8:s.N'k-g ',74]g. ~ ' Jl* l sA. ...... d 4 e v i. 4 [ I '. 8=d. v t .,,,i au a i. ..n, e.,. .6.he....s...,.. .N.- CC. SIN E r., ST R ES5 4M Timu TY, 5 I " "- "o * ". s, s L,., <; +. sfe,,, a. " - i...n.. s = i. .e < 6. <. - l <r+". l n.x r, o 5= / <<,- r.> -i e ....a.... -./'%- (' N,/(M /R.,2,3) so determine 5 by (C ) from Table u Calcutation of stresses t t 8 (sce para. 4.3). 4.3.1 STRESSES RESULTING FRO \\f RAurAL LOAD,- 4.2.2.5.2: Wher. consider:ng bending moment P. (M,): 0 = Kr.4p,3,1 where Kz. is given in Tabic 4.3.1.1 Cirewnferentici Stresses (a,): h. 8. Step 1. Using the applicable values of p and y r 10 Stresses in Shrils
a1g s T:bte 5-C2mputitiin Shut f ar Lecz! Stress:s in cylindricci Shills ~ b%g ~ Lt2. n",uJ y & /'e-" Sdg i /> i. 4,,i. a L.
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't 5 {' '36 ( 4) (N Tabic 5-Computat;on Sheet for Loc.21 stresses in Cyhmteical shetts % *N 9 %g \\ Q p -s b"l 3D k L J y \\, g M g g. '.hgy "'r-" O hN o N
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