ML20236L909
ML20236L909 | |
Person / Time | |
---|---|
Site: | Comanche Peak ![]() |
Issue date: | 02/19/1987 |
From: | Dalal N, Matta G STONE & WEBSTER, INC. |
To: | |
Shared Package | |
ML20236L742 | List: |
References | |
FOIA-87-684 NUDOCS 8711110114 | |
Download: ML20236L909 (66) | |
Text
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CALCULATION TITLE PAGE
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CLIENT & PROJECT Texas Utilities Generating Co./ Comanche PAGEi0Fjsl ;
Peak SES - Unit No. 1 Total No. of Pages. /r ,
f C A L CUL ATION TITLE (tanicesive of the Objective)6 l
PIPE SUPPORT CALCULATION Support Marx No. : cT -t -IM -701 -52 G R Function h<rA/ Q - {U C L,E p A Pipe Stress Problem No.:. 1- c :2, 4. No d e P t . J,3,of,,
CCNT An! ME.tJT' Mt2 AN O - NO N - N u C L E A a l System:
c /.rr c u M O $AFETY REL ATED Buildinct C A LC U L AT ION 10EN TI FIC ATION NO.d 5ER CURRENT OmON AL WOm J . O. O R w. O . N O. Olvl510N & CROUP CALC.NO. TASK CODE wC R K P ACK AG E NO.
15454 ZB N/A NZ(H)- ;T-1.@7 1ol. s2fR A pp ROVA L S - SIGN ATUR E L O ATE SUPERSEDES CON FIR M ATION 3
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- ' CALCULATION IDENTIFICATION NUMSER i I' .
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15454' -NZ(H)- g.p y w _qq. p 1
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1 TABLE OF CONTENTS l l
' PAGE NO.
TITLE PAGE ........................................ 1 l
TABLE OF CONTENT 3 ................................. 2
- \
REVISION STATUS TABLE ............................. 3
.......................................'. 4 OBJECTIVE ASSUMPTIONS ..................................... S- 1 MITHOD .......................................... 4'
.................................:.. 4 SOURCE OF DATA
..................................... 4 CONCLUSIONS DESIGN INPUT .................................... 6 ik. ~
~ ,
FORMATION OF LCAD CONDITICNS 2 . . . ...........'..... 7 SUPPCRT DRAWING ............................... 8 REFERENCES ...................................... 9 .
RESULTS
SUMMARY
................................... 10 COMPUI'IR LOG ...................................... 11 R
ANALYSIS ........................................ 12 - i f
~1 STRUC"' URAL ATTACHMENT LOADING SCHEDULE ........... ,
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ATTACHMENTS 1. A%LTG1G COECKUGT l.1
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,15454 NZ (li) (T l 1M 1W.f2GE. ZB REVISION STATUS TABLE 3
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CALCULATION IDENTIFICATION NUMBER
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l 15454 -NZ(k)- g_g g y A g l
- - I OBJEC*IVI OF CALCULATION 1 To substantiate the acceptance of design change (s) noted in change docu=ent...
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k 10C - Fko + c 90 CALCULATION MI""40D This suppcrt will be designed in acecrdance with ASMI III, SUBSIC"'ICH N?
and is based en LINEAR ELASTIC THICRY. Loads on the support will be cbtained frc= the supper: su==ary and used to for= the appropriate lead cc=binatiens. Me=ber stress levels will be deter =.:.ned and cc= pared to the allewable stresses. If applicable, cc=penent part 1 cads will be '
n deter =ined and cc= pared to the allowable leads. All welds associated with the support will be siced based en strength require =ents and g'd' =ini=u= weld sice require =ents based en thickness of parts joined.
If applicable, local stresses en the run pipe will be deter =ined and cc= pared to the allowable stresses. Pipe support structural attach =ent loads (reactions) will be deter =ined.
SCURCIS OF DATA Pipe Stress Calculation No.15454-NP(-) -(J- f- o0 '2 Rev.1 .
Pipe suppcet detail Drawing No. GT tv -bl - $ M'R Rev. 1 _.
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- G(,-3-2M . o (fb 6 i-y -i)lation. roc - grco y og Fcr ref erences see page 9 cf this calcu sad e.mmes som C.O. NCLUSICNS The design change (s) as noted in the change docu=ent have been evaluated i and have been determined to be acceptable.
FIPE SUPPCET DET AIL. DWG WILL F.E REvlSE"D AS SWcVN CN P AGp. c .
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! - confir=ation ASSLHP"' IONS USED IN THIS CALCULATION . - required YES NO 1h-_ ADE00fM D /
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p) TT \6 hSSUM89 TilAT 'fl!E i)D) STRVT fmriod ( MCCDoiJ C o S m C s
- 3 co.sx = 0. M w os y = -0 7h y s y cs s e = -0.c 18 i) a kcet71Cc E Fre s7tESS Augs.y s t.5 y e"tiI,/
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15454 CT 13'4 -b i -526 ? .
- ' REF .
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' DESIGN INPUT Stress Problem No.- 6 - l-OW2 le t>. I
.Line Designa' tion: 10"- GX - l'6 J -3elit - 5 Run Pipe Material: 6A'M1 Y EO
. Pipe O.D.: IO.r5 zN.
Wall Thickness: O .% 6 IN.
Pipe Insulation: nod b- IN..
Ib . . .
The following should be ce=pleted only for supports which involve an integral attachment or run pipe bearing line load.
- I Operating Presstrre: '2IO p s14.
Design Pressure: 3 '2 I psig.
Operating Temperature: [N *F Design Temperature: 3N *F Sc = / psi.
Sh = [ psi.
G SECT.- Pipe'suceert Mee er Desien Temperature 4.22.1 7
V 125'F (Support located outside of reacter contaL'u: lent) 300*F (Support located inside of reactor containment)
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' i 6 !. 3 LOAD FORMATION:
SUPPORT HAAK
- NO. CT I-\M ~461 -6DR
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- SUPPORT FUNCTION 75KN .NORTE DIRECTION = blOMb j 1
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e STRESS PROBLEM NO.- /~I- \ - 61'2. DJ . k NODE PT. IhO b BASED ON CCMPUTER RUN NO. 2 6M OOD2 ' DATED Y f Il ^L- c io-8' JOB NO. ~L36 9 et 4 13 l I LCAD TTPE MNS(PSI) FI (LB) k FY (L3) FZ (LB)' 1 is g 88 DL' 96/ 24,% l\ l /
j 87 THER (NCRM OPER) l f fq 4 l - M 2 (- l \ l e' to TER MAI. f fg g l74/ l \ l j f N TER MIN. tr44 A)Sl l oN 1 :/
n:)
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2' SRSS(OBET,0CCU) l 712. 0 1 4 05 l- N
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2$ SRSS(OBEI,0CCU) l / p / c. l p ;h2, l / -l N ]
85 SRSS(SSEI,0CC7) l 4.y 6 l 147_ [/ l \ f)
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LOAD CONDITION MNS (PSI) FX (L3h FT (LB) FZ (L3) ~!
3, 1 L / 9 3( p / .)
35 ., (
3: 176' E 1. DL + THER \- / 4te; /- 1 33 3*
4' W 2. DL + TER + SESs (OBET,0CCUI . /
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se 4-. DL + TER + OCCE , ,j, 3'
$. DL + TER + SESS (SSET,0CCF)
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DYi 14 lh
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{:;};9 en THEREFORE e
- LOAD CONDITION 1 IS ALWAYS ENVELOPED BY LOAD CONDITION 2.
3 LOAD CONDITION 1 NEED NOT BE CONSIDERED IN TE ANALYSIS.
,, (FOR 'SANDUL' COMPUTER RUN ONLY) en
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- i. 'a l REFERDICES .
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. @' Division 1, J974. Edition vith Winter 1974 Addendum.ASM e 2. ITT Crinnell Corporation - Catalog PH79. '
3.
ITT Crinnell Corporation " Design Report Summaries (DRS) and Load I
, Capacity Data Sheets (LCDS) " Rev. 12, dated May 5, 1984.
'O h CP-NPS Catalog-NPSI component Catalog for Comsache Peak Project.
in h NPS Industries, Inc. " Component Support Certified Design Report Summary" LCDS/CDRS. ,
@ Design Criteria for Pipe Stress and Pipe Supports CPPP-7, Rev.'2,
- dated 4/25L8cu, tac.L2Da.t1 M.t 2xo.1EC2 MfMQAdHB4 M PSD WDSM
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67 /*d4'.PcAJ6CT P4eCeDOR&f ' $ZMU$. DMdD. '/> 412 'I l
, h Pipe Stress / Support Requalification Procedure CPPP-6, Rev. 2 ..
,, dated 4/18/86. )
(
, " Manual of Steel Construction," 7th Ed., AISC 1970.
8'
- 9. " Manual of Steel Construction," 8th Ed., AISC 1980.
(For Tube Steel Properties Only) '
is
- 10. Blodgett, 0.W.:
,, " Design of Welded Structures,"
'ss The James F. Lincoln Arc Welding Foundation,'1976. i
}
to
- 11. Roark, R.J. and Young W.C.:
at " Formulas for Stress and Strain "
5th Ed. , McGraw-Hill Book Company,,1975.
i l
, h'(a) Gibbs & Bill Specification 2323-MS-46A, dated June 26, 1984.
3' 3' (b) Gibbs & Hill Specification 2323-MS-46B, dated April 15, 1983. '
se (A h Pipe Stress Calculation No.15454-NP(g)-Cr O?? Tev.1 h For computer programs used see ' Computer Log.'
ss .
l se CPSES Pipeline Designation list (Unit 1 and common) Rey (D Date N9 S5 37 16\ 'i se Ceneric C41c.15454-NZ(C)-Genx-073 Rev. 0 (6-3-86) Evaluation of NPSI Rear Bracket dimensions for Design Calculations filed in Job Book No. 14.5.1 h Generic Calc. NO. 15454-NZ(T)-GENX-087. Rev.0, dated July 2,1986.
" Calculator Programs to determine weld sizes for use On the Tektronix m ei Model 31 Progranr.able Calculator",
s $$ st df% 42d MP k)vWEL h${CM6L cpIFfu gS$ y p y y ; , 9 ;,
n Lw. 5 on 6-o s-E n 19x 2 (1 - rcy)
NOTE:
..** Reference numbers circled are used in this calculation.
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CALCULATION IDENTIFICATION NUMBER JO. OR Wo. NO. OlVISION & GROUP CALCULATION NO. PAGE l o O'. 15454 -NZ(R)- 6T-t N - h - M c A RESULTS SinfMARY The results of this calculation as shown below are a comparison of the calculated loads, $ tresses, weld sizes, and interactions to the appropriate allowables. The maximum ratio shown is the worst case for all occurences in the calculation of each item listed below.
MAXIMUM RATIO
- 1. C:cponent part Actual Load to Allowable Load ,
8 70
- 2. Component part Required Weld Size to Actual Weld Size Used
- d.fh ,
- 3. Run pipe Actual Stress / Load to Allowable Stress / Load; due 'N I k to Bear:.ng Line Load
- 4. Run pipe Actual Stress / Load to A11cwable Stress / Load; due Ohf 4
to Integral Attach =ent
- 5. Integral Attachment Required Weld Size to Actual Weld Size 8Nf ad^ Used 40 ' '
- 6. Non-integral Me$.ber Actual Stress to Allowabis Stress:
fLA fG (lftM v 7 ) y' c C N O %c tuts,S fp $crug %u coxSJ Load -Cond.
- 9I Normal Stress: Member est Shear Stress : Hecber,yevuumu Load Cond. n a2f
- 7. Non-integral Member Required Weld Size to Actual Wald Size Member %'//N N A/ Joint 70 ///< (ifE71a '))
Used; f/6
- 8. Base Plate Actual Stress to Allowable Stress 6O
/>f36
- 9. Anchor Bolt Interaction
- 10. Richmond Inserts
" N Insert Interaction N 4' Bolt Interaction 4
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- NOS: Under Maximum Ratio, write "N/A" where not applicable.
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..
- 22
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ~ . . . i Ft -F . d- .L25. m1 'a w 3= yfo[IN.-LB5. 1 F2 . Fj = [ g } La5. m2 e u
- g IN..LSS.
,, F3 = F %. p y g La5. ua = M g= p IN.-Las.
26 . 2 & L . I F* * ( F1 + F3 )* ( 7vt/g
- o )
- 7 0[oL85.
. 2 A a
( 02*g) aj Jf sf IN..LB5.
-se m* ( m1
- wa ) * .
so
. .C.AS.C.l .* co ? f3 j 3i Applicable La ell pape, pad, or piste connections i j 73 .y g ,gg. WILD PRO 8tRT215.. (TREATED AS 1.!NE) l . ..... ... gl g3 .A .
uda.;rffyG*golfsN. M. T
.. z .
Il
...d.o. klU) . ....... . g g 1N.
2 r ._ . - V M2
\ ge 37 3s J/C
- 22 e 2 x h . f [,h IN, _
38 80RCf h wfLD PER UNIT L1NGiu ! 4: F: ** 2 ** u: ; . r.. .... . ... 3 . c.... . .... 3
'8 A '2 . a s/C s
" Y,jaNk
. pI ff.2.I. : l
(. .. F 3..H..o.f.37 c .2. .M.. ..o... ......, p :
. .s .
Nl 17 // J 10p j
.s F = . r w as.:xN. t e ..____.__m_ _ _ . . _
g.j.e ,[,lEg . . t
't ' f,~=: c o n... ,s 1 CALC'JLATION SHEET FSo (li 25 8 6)-PG. z e,p +
- . f\- .,,,,,,
C ALCUL AT10N IDENTIFICATION NUWtlER , I, OPTIONAL TASK CODE PAGE - .. f, '.i. 0. O R w.0. N o. DIVISION C. GROUP J CALCUL ATION No. ~ i c& suu uz& . wlIG.7p%rl .>f> av. CASE l'
- MO/Oc 2/3 - (,C O NT'D ) .
.. ....s. ..
O f 3' 4 ATTACM, . . 73 F.: fist ptsu et 0 ,1,0 90: ' l 3 .d.2- > m trumatema attacasd with 0.1 1 03 95' ! 6
% ,.netista u ==14a. *** . s.n. w o.2 o.6 1, . s,o, I,9, ,0 3.18 ii g - ~ . . .
0.3 1.23 124' s e.6 1.27 f3) -j ng 0.67 1.31 ggg 9 _q /* l
'l d ~ P1 Pee ,*de.*f , lata ] ' o, n2 I4 ' # 0, 5 f . **
e4 eg is e.ed ter calculattag W,g ia lies of matag Table 2.6.1. U . _ h _ 1 9 FORCE ON WELD PER UNIT L(NCTH ,3 l] g
......... .....,. 4.. .......- F = /Q-O O LBS./IN. g3 " ' f
{"} CASE 1 d n/De > 2/3 / .m,>- ,
..sg a t 1 i-i. .ttu .,,io,,,.,,,,,, , '
_ o / t m% . , attles =14 al ar=.4, Do= diameter of rtta pipe or pad, ___,
*' Yi */ d /'
1 + ,;,,
'wELc peoprnT1ts : (TarATED A$ LINE) i g .s1 ..... .... '83 ,t<
c1
.dd . . IN. =" - = " "a - o "a-m VN L
w 3 x f u
. e : cosa(24/.3do) l IN. I ,s A = ATde 2d,g *
- s J
" (U - 20 + Sin 29) . 3 ' 23 g,.. 4.. 1N.
s a 2, 30 3 3 l 3, 2 3 . d. .o. . . .(.n. .. 2.e . s.i.n. 2 9.). . . . . 4. . . . . .. . . . . . . . . . 1s. . . .. . . . . .
)
8 32 l
~ ** J/C=dj[Q-Oh : 'd-3' 2 / ' " C3i:: E(C%.S ,
a-
=
2. g N, ,
',l 'f u
34 eCROE ON w(LO PER UNIT L(NCTH ; -
]
p ...............................
-fir,i . ir/ in.i 38 2 2 2 ; >~ F = i.n ir,i e, in,i *3 c in,i r* 1, 2, . * ~
- TTi-l 40
.i.ng/n.......................>: . i....... . .......,
i M,
;\ . . , , , , ,,
F . .81.,.h. . 1 e$ 46 , l
~ - _ _ _ _ _ _ _ _ _ _ _ _ _ __ __ .%! 'l' -- \
l j p_, . .1 ' ., S ' r J .t : - ms - l _I. . ?[I ! n
@0E ;' , k~124 f; .. , f, , . ' . .+
s .i H 4. '., l .. z j. C%a Q ' ' 2 n,o u P so ( ff25% Y-PG 4 4 F ' '.A
. f . . , ! CALC UL ATIONE S HE ET- '
1' l E C ALCUL ATION 10ENTIFICATION NUMBER - .
.. i~
a*i
' - J. O. O R W.O. NO. - - DIVISION E, GROUP CALCUL ATION NO. OPTIONAL TASK CODE .PAGE 'g -)
f k 15454" N2tf (T e j ,'l') },,)o f, [d , _p bI* ALLOwASLE'.$Mt AR STRESS r
$$ = 0.6 5H ap P11. FOR ASME 111,CL.2 4 3 FIPING. ,
g ,; , , 1 i t
'm- '
3 . OSg
- C.8 SM * ,
LPSI. FOR 531.1 . GM.!CL.5' p! PING. 1 2[' 3 s
~ - O 'sg ' = 1.f_,5ylCo.(t/2)'.
0 ' p3T isf yjggy ,ygif .] L* af1ACN.. (21 kai nas) l 42 - Sy - Yield stress of base metal at design temperature l h g -Sh . Allowable stress at e*saw, temperature for weaker of metals N.*'
- l
,jetaed . 1 i? , , REFERENCE FILLET.wtLD : - - -- I e F l" \
u,
.. &.. '.?o' 9~ ,, waREr.) . u........... -(0.707 X: 5) $
0.707 Xg g
.gpg:N. ' .j q
REQUIRED wtLD $12E r > 4 - ji 'si , . . . . _ . : .
,3 FILLIT. WELD 4 *. . FOR Cast 1.' 'l r
- .g .
-9 is 'We'e w(REF.)'X K . x . pf!N. WMERE X 1 '- . . . i.o ' ,oAeastz.4 -
j j - w MIN s' .IN. f . WP (WELD PRCVIDED)
- IN . ' )f WR og N CPARTIAL ENETRATION wtLD 1 ,
- t. ]
ig , 88 - 47 W4p q ' < 1 JM 2. Ss = 04 Sv : (21 lai.* mas) Psi y
- d. q 2:
t / q s *Il '
.ss ,7 Ty ' :l h ~
lss-1 l te
. ER - .0.70T X w(REF.) =- 'IN. .1 l ' 38 ' ~ >p ER
- IN.
to E MIN . IN ,' .E ACTUAL . 3 . g/qg * .- !N. tr 20 # LD sKTWtIH - THICX RE!NFCRCING D40 ANC THE RUN 919t t
.q.
- 3, . REQUIRED FILLIT wtLD .
l 30 wa(pac) . IN. C s!! CALC cN'escg; I l 31 C CONSERVAT VELY TAKEN 5AME AS A50VE WR, SINCE:THE j wtLD DeCP ERT115 CF ,,,,,,' I
- RfC*A W LAR pac l 32 _
t ARE uuCM MfGMta Twth .tLa pacptaT !$ OF ~
- I 1
33 O!AMETra TeUNN!CN. MULTIPLY wetpAC) w Tw aa? Sg(NF) /56(NC/NO) 3 t 8CR 'C = 3* Casts. l D-' , ' g , 33
'wa(Pao) = IN. . tN.
3, ( wa(Pac)(wtLD *Rev!:tD) ! 3, t eso - i/is . . :N. >,weieie) . :N. l
. l 3.
3, 7..................,.............................y Twt weLo 6...............g....C.1sNotACCEPTAaLt :s .. l l
........................e , .e.
jfM d' i
' h,1, f ' at i i .l
.,.e
.y .
e3 I 4. l t t'
,g i ; '! . [*6 I S,G , =L _a__
.O STONE & WEBSTER ENGINEERING CORPORATION * .,1 ,. .
CALCULATION SHEET 4- A 5010 65 CALCULATION IDENTIFICATION NUMBER
- FN J. O. O R W. O. N O. DIVISION & GROUP CALCUL ATION NO. OPTIONAL ASK CODE PAGE M i
15454~ __ NZ (ti) ' 6+1N-7'ldidI i. ( AEr,
- SW-2 WELDED CONNECTION - RECTANGULAR OR . -
l' I? SW-2 l PARALLEL [(, (4 sides WELD.C0 tit 1ECT1011 s
' all around) RECTRNG/PRRRLLEL . SIZE A = $ $ 1n.B= 3 in. (4 SIDES) ,
allowabic.Jeld stress S 3= 3f M '## psi REU.0 11/25/85 ! s /ZAC member BOWET ToPfkTEF(;&f, joint W = (HI2 Al UNITS LBrINCH t MEMBER FORCES & M0MENTS RLW.UELD STRESS
.,, (maximum absolute values, joint similar 1aa19 " pu n 1% if RECTANG.S15k R.iB
- 1. axial .,e
'2
- 2. shear F2= /4617(03[//v-/gt @ < /4 2 3 3 $ #*%
F3= o ** is 3. shear MEhce?" FORC:<'
- i. , 4. torsion M2= Fl= /44 o
2 7 54 M,ggnj" 3 3 7a cf> FWIRL F2 is 5. moment- 14233. i6
- 6. moment M3=
Ml= o 3 7'/ 2_ x 3y6 : //fq/ w,M SHERE Y F3
. l.'..
i, j SHERR 2 F1 - 3372. ; is MOMENTS: ' TORcIGH M2 20 iff 6 6 I si MOMENT Y M3 11591.
,, f) , __F2 - , 3H1 + 3M3 - (10 MENT Z h! ,, 2(A+B) 2 2 D' 4
A +3AB B +3AB '
,, f2 = 'F1/2(A+B) + 3M2A/(A+B)3 FORCE r'. f3 = F3/2(A+B) + 3M2B/(A+B)3 , ,y 2
2, f = f 1 + f22 + f32' 30 e.
/
6 UECTOP CUh W'2' WEL D REQUIREMENT (Min. j fl6 ") W=f/ 707S3 f,Q5.C Jun =- Q " 7 Ju.s. : qf " -
-.x ________________ -3 ,
55 REQ. FILLET UELD r3Jy .146 35
.37 % / MS '
L 39 "O M1 L h A
'.,/a. ' "#.3 y d4 X MZ ' ~F2 _ *B
~
- f
=
c.. .,1 < STONE 2.T!EBSTER ENGINEERING CORPOR ATION m CALCULATION SHEET . CALCUL ATION IDENTIFICATION NUMBER
/ )g . J. O. O R W,0. N O.
OlVISION & GROUP - CALCUL ATlON NO. OPTIONAL TASK CODE PAGE 7 15454 90 i NZ(ff) GT'l'I'll~/ol-5WA ' n
#' .. \
3 SW-2 WELDED CONNECTION - RECTANGULAR OR - 6W-2
- 17 PARALLEL WELD. CONNECTION
* (6 (4 sides - all around) RECTANG/ PARALLEL SIZE A = TVin.B= 3 _in. (.4 SIDES) ' allowable weld stress S = M N r "' psi REV.0 11/25/85 s ( W $/lu tG r TD fh1Pft M 5 '#SW' ::::l1911RI UHIT?:LBsIHCH mem5er , joint MEMBER FORCES & MOMENTS ALU. WELD STRESS (maximum absolute values, joint 19912, similar. RECTANG. SIZE A;B ,m j 1.P/2eH 96 t}F2=/4/2 / (* 7/z 7) == H&4 9 tg axia)
- 2. shear F3= o ]3 , ;
is
- 3. shear f1 EMBER FORCES:
Fl= / 44 2 7(# 21",t ##7/I')y,:- f/0 M R.'4IAL F2
- i. 4. torsion M2= 0 is 5. . moment 11449,
- 6. moment M3= f l e 3 x Fft, 5 f / 2 9 c _ ,y,g SHEAR Y F3
,, M1= 0
- 0. Il SHEAR Z F1
's 9103. J ,ie MOMENTS: . M,,ho TORSIGN Mo w ,, 0.
MOMENT Y M3 31292. . 23 F2 3M1 3M3 110 MENT 2 M! 1 fl = + +
. 2(A+B) 2 A +3 AB 2 0' k B +3AB ----------------
es FORCES 1,2,3
.,, f2 = F1/2(A+B) + 3M2A/(A+B)3 3370,19
{
- f3 = F3/2( A+B) + 3M2B/(A+B)3 728.21 2
.. f =
f f 1 + f22, f32, g, ! 30
/
0 VECTOR SUM
,5l WELD REQUIREMENT (Min. k6 ") W=f/.707S 3 3447.97 l Ss Ufbp hi pWgo. s#p "
- 3. ' ' , ----------------
3$ REQ FILLET WELD
" Fd Y .244 37 s e ns 38 31 d' N1
_L h A l$$.
.., g Fi / / i 43 p
44 N UI -
*5 f2 ~.B es _,~
l
, -.* , j, , ' STONE B. WEBSTER ENGINEERING CORPOR ATION ' ,. # .. CALCULATION SHEET . a im a CALCUL ATlON IDENTIFICAT10N NUMBER
{ J. O. O R W.O. N O DIVISION D GROUP CALCUL ATION NO. OPTIONAL TASK CODE
' 9'
- ,5454 -NZ(k) Of'l ll') /Jol- 5 d 2'B PAGE j , ;, _ . .i - - - -
A E /.' ' SW-3 CIRCULAR WELD FOR STRUCTURAL MEMBERS' > 3 Pipe outside Dia. 0. D. + dl 2C "
'~ '
4 I7 o s allowable weld stress S =/4x2//n/w' g hmember kE MdM 1) oint,14'Vdded a 1992 su-3 MEMBER FORCES & F0MENTS rg/ CIRCULAR UELD (maximum absolute values, Joint FOR STRUCT.MSR'S similar). s WM M 2 6 s 1. axial F2 = /4 23.3 L6 REV.0 .11/25/85 io 2. shear F3 = 0
- 3. shear F1= 3372, LS UHITS:LB3IHCH
- 4. torsion M2 = o ALW.UELD STRESS
1g292, o 5. . moment M3 = //f9 / /N. 6
- 6. FIFE O.D.
i. moment M1 = 0 6.625 is MEMEER FORCES S RXIRL F2 14233. ie SHERR-Y F3 1 t, O. SHEAR Z F1 h::; 2e f t= F2/ TTD + 4 9 2 2 3372 - us to M3' + M1 /n D MOMENTS: 8' TORSIGH M2 f s= 2M2/ TTD2+ F32 + F12 /Tr0 0. 22 - I. 2 MOMENT Y M3
- r. f, =
ff t2+ s 11551.
,3 MOMENT Z M1 ,, ( 0. !
2' [ WELD REQUIREMENT (Min..rj/f ) W=f/.7075 3 FORCES FT,FS Mft.z Wn * '/i' ***'" 3, vg a ptf . . sz 162.01 i
~*' FJJ VECTOR SUM 33 t>' M3 1032.88 !
3 ,, 33 RE?. FILLET WELD 3, .069 57 Sa E=
,, n)M1 "
D
.o .
42 43 x F2
- 4. j 4S I' i
44
3... g > . 1 p' ' *'
.)
STONE & WEBSTER ENCINEEKING CORPORATION g
"i' -
CALCULATION SHEET I a wo u . F2Y0/088G)/oe g -
\ '( g C ALCUL ATION IDENTIFICATION NUMBER J. 0. O R W.O. N O. ' DIVISION & GROUP CALCUL ATION .NO. OPTIONAL TASK CODE PAGE - 'l l
15454 NZ(N) -M'$0 l 4 d
- f j s REF.
i l~ 3 BASE PLATE AND ANCHOR BOLTS ANALYSIS i (Using Computer Program 'BAP', ST-383U,-V01 LOO' s plate 313,: ' ]6ff "xf f[""x l " (Haterial: O -%-515GR65, g SA-36) I
.a Anchor Bolts: C( Hilti-Kvik (Friction Type) K=.25E6 lbs/in " Nelson Studs K=2.5E6 lbs/in !
v 0( )
. OC ) "Hilti Maxi Bolts (Bearing Type) X= lbs/in , Q4 / " ft/fEk,,tilL-f > h i l K: .116 Gy/
Attachment Size: . t0
' } "g > , f ~ .ai d
lat . >- r-ra
~ " a.
m
,, ** BAP '
CO.WUTER 871 ~ p M 5, M- A PROGRAM $- - 4 a.> f d &
,3 16 h
h a' .17 , 4 i is 7 A TTA CHrEr/ T* - . ( .j.f x 2// ' ,, e'
- b b
' " T ,, bb/ E u *s 2/.$
b'"'A n n)
- s y
' ss 27 4)[' N 'l C %[
p GT A3 80 p i g 32 __ f G 3 bI26" 2
.- X D.iv, .
l f
' ^ 3S I $J16 3
2 h% P[ 37 38 C -~ 3' NJ)L~,) N.(E)
** (y 4i r ,, Notte . 1) Input loads are in local coordinates. -
' h@g. ,, 2)Meis t critical loading conditions are considered.
** (0 OR P/ /A/ 91E'S OF ATI~/iU/Myjf Q c ( );, y {t&
45
'4s
__lm_-___m_i__.1_______
- 7. . a .,:l. .
- P '
,,q , ,c, r STONE P. WE85Td R' ENGINE E RING CORPOR ATI,0N.-
A L. i , -CALCULATION ~ SHEET
- a mo u . , .. /Y . F CALCUL ATION IDENTIFICATION NUMBER 1 'PAGE' ~
J.O. O R W.O. N O.- DIVISION D GROUP C ALCUL A TION 'NO.- OPTIONAL TASK CODE IlM*lf N2 (Yi ): CGf'13'l-201-(d. 8 - 3 a' f' AN(ifdL $0L.y $1EE k(fv/tt if(cfl ) X l2,/'LoN(:r! ~ ' . I ATT4 4 , - } [y 'f MIA/. eM8ep M6^1T fp>0/4
' =
Fre!AL EM6@MeuT = Vf - l 6?/f" i*
% = l7y)' e ) Sh5Ep 6MI [3 " EM S , 4 @ p GAlcRETE
- (
'o yp s' GyJg:n ) ?sSThnc G .b " a ;
t 's: I Mlbl. Gil57*th(g fou[ tioL6 6966 96TPNLE-c 2, 7 fMWREc'D i
" . or, f>
56 Mi^l 6st-f SfActslQ KE&ut2ED = lO pj f l' MirJ GNriMr 60cT st'Actas, ==- to mio sjz p .
'a '( fa j Web,f lJC1h W O C WATIO'Y Q
wy hs Ti!E Ssevf is P!:ECTL)' m/ c t'E:
~
23 l- f
**' . CdWSt.DCK Ep ,
! tb gs
=>
L n Iht' 29 . 30 y Si
*b t l 33 I-' ' , 3..
3S
/ .. 36 3r 38 i n
[khh. . l; ,: 43 j; , j [ < 4 1x_.1 _ --- _ __ o
L cg * ,*
...i! 1. . . ' "e $,....;* ; , STONE E. WEBSTER ENGINEERING CORPOR ATION .
7 l h ( 5..' ' , CALCUL ATION SHEET' a
,. 'lA 5010 65 . C ALCUL ATION IDENTIFICATION N!JMBER j
[N" -
. J.o. O R W.O. N O. ' DIVISION 0 GROUP . CALCUL ATION NO. OPTIONAL TASK CODE ,PAGE k )
h , 1 3 , "19494
. yg c g) ci . ) . t31-1 ol. 62.9 R. Z O' l .l m .i a
l "'u.. .
- i. !
- i. L' S EF. ~ - '
g;p a ATTACK. EvAt u ATrotJ oF E ESV t j
- . :s .g 5 5
( Fod sesv 4 lls F0E su ff r. I f'H-l-oc>q. ool-62.2.R. g;, g - z .
. +.
io .__J 1!
, 4 f .- ~,, . , @1,.-__ - - 89/8"'
or9/4"$HK&. is
'5 E ("4" H K& . Q\Q,4 pac.ld C. g g [ p, . 8 3A "
s
t 0 L .E , 6 M" '7 -GuffT # CT l-l?1-101 6EGC 2 is (7419 Gurrr.) 6 X 14 TIM G GFt.c.idG .$ kg;"
0% .to FO R ' E E 6 \/ N 0 3 /1- 't 22 J: N co x"'
.24 . * {"a 4K&
ts - - -
, f,r I'*
- T-'i 'f l/c 4 X 9'/[ HK&.
I ;. (Uul.+T<ur - IAl674UU$UT currT.)
se . l'J ." l . M lW . 4 PAC llJG R.5G'9. . 7 Y
'[
_yL l S g ,, _j f c> A r , 7. s " l CkilN)CXt97pJG fi.P4dlMS
- 97 /f"
" ' Gu PPT.1 cr.1 15,1-101- 42.9 R (THI9 6dPPT.) '
36
.'.u+crn w xer u T m eiac cessv 6 A " 6> R c N c 710 tJ FACTmt. ' - ( ACTU AL WAC.lMG)* ** (R %'P. 6 Fact %)1- " ,& , f (5. G15]2, , (,s l 5 (c '** (1 9);
ff a) 4= 45
- 1. Tw. e.FGrt) = GiuGs74i) = es/A 'M 5 3 :. 4532 lbs. (so usucnod) 45 46
_ 2_________.
7 t sp -
~
n ,1 .'*0T ,i. 3 .,; .c ...
- STONE & WEBSTER ENGl.4EERING CORPORATION
./ 4 c. . . .
. .. CALCUL~ATION SHEET ',.
um.e FH(e/0884) ps9 f'
~ .d '"? s ~ CALCULATION IDENTIFICATION NUWBER. . .. t . '7 p ~w .
J. 0,' O R W. 0. N 0. Dividl0N C, GROUP CALCUL AY)ON NO.. OPTIONAL TASK CODE PAGE - , N 15454- WZ h'h ~ A Jl'llb 2#b $d " i arr..
.g i 3 CECK ANCHOR BOLTS: .' 'BAP-Computer.Out'ut(RunRJ0f( p jJob#:u Datei P/p/
a 'BAP' From .'BAP1 Output: i y ' COMPUTER
-* PROGRAM $ max = 9 3bQ Lb s. (MSul YS PAGM a RPfu eu 1 DEDA!c) r . ; lFROM '8AP 2'007P127 : .. ,
Lci rmax ; syjnas.('es4c7/oM ases, max @ J7. i .
)
lSmax?B' 'Tmax f3 x j,o ~ qSm.t i qTALL ^ ) ' is . .. ss
] ?3dy k: + ( 3.r3y iS4 = s' m + s. s oy = av 1.0 y Wst /: ( fJfy /
CECK PI. ATE ' EDGING STRESSIS: (/f,cc/V) . JA8 7-)
.. p.. ** + :.2.U< m ** S Y = ji yv ' P SI @ l g *F Fe2 ' Sk - } [ M4 TL. . l 23 ** Mar nam PrinciFal Stresses :((tTD psi 10.75Sy 7hr0 PS/
3.. na (Sig.1 or S432 at elem.g ) ] 4 Mari== Equi,ralent Stresses spj-1 psi 10.75Sy - dp g F.5[ 'f
'(Sise-ateles.g) 29 -30 s: ' ~
3: Base _ Plate // ff "x/4),"x [ " 0.I. 3, Anchor Bolts ( c.) ["f eg _0.K. j 34 } i 33 i
'<- 36 37 30
- 39 1
4 40
,41 7 + . , . 43' m' . '43 8 .. ~
45
>.. j z
l _-_ _ _ _ _ _ - _ - +0
l STONE & WEDSTER ENGINEERING CORPORATION
'. CALCULATION SHEET A 5010 65 ALCUL ATION 10ENTIFICATION NUMBER - J. O. O R W.O. N O. OlVISION O GROUP CALCUL ATION NO. OPTIONAL TASK CODE PAGE I 1fy9y NMH) C1 I d')-7f1. N1R TS l ~
3 a REF. friFrrK66 C M.,(. U (J6l0 rJ I
. 4 q 4($U :
Qr C Y Y K (OI L- fid , l
.. i8 _fcAL (RA ct'E'T : ' l . fe% 04 Q r .: (0. 51 x t o t Fj'ut 9&f4L : 45 = 10,1 t vio l i.1,li d i.
f fMePtinE : p t w c. 6:p(it.rtr)rinr u / Thator) : 3 I is -s.V' I
: If . g Q is %
l 6- p irl-s . '
.Q" ,2.g $
ze e i m. b , ( I [. f )/ /O 4 [ fg s M
/S.12 5
23
** [C1/1 Tint) h.?9LI'( 1 )'
es . 26 6-M ,,, /[ f 7 f - ~ { , , , g] 21 (3 -(, 3 / S./ LJ' (if 28 30 ric \ \ ' Qgx = 2 7 o v to ' ") LE/'fD ~ f 0 ?{4 7"l(??) hh6 L/ ? b '" b _ lO T b 2 5 ~ S ' g' }(I 5t 3 ~ i 9. Sz ,1 ( oy. 33 R&, 5 l (1, r,i j : 2 70 v10 i'J Ll,l(/D 36 37 38
*f N f).
V 4t 42 43 44 4$
v.
)* , .
STONE E WEBSTER ENGINEERING CORPORATION
'- CALCUL ATION SHEET i i soio ns C ALCUL ATION IDENTIFICATION NUMBER l 'rfAg l J.O. O R W.O. NO. DIVISION O GROUP C ALCUL ATiON NO. OPTIONAL TASK CODE PAGE h i 7V9 4 N 1(H ) C4J if 7 7.idwR of i
- REF.
R%hhotJ fLV&* (1151 A 1) # Cett BC} c c ET kSS?/s.-Y d d , / ! 5 /Ifi 4,15 i
)
( ) ( o.
,? O q O O O is : , I l L ,, .
l Io ~l
- l. .l '
.,, 3J%.,$;_-. ' ' ytL-- P i .. [ !
se
} hr f '8 Ma'pEL ry)R Atu L'/5 g IS ./cruAL cc#Fh/kr10/J I
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^
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24
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= /6 4
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- STONE & ' WEBSTER ENGINEE RING'CORPOR ATION '
"'r
- a. ; ,
CALCULATION SHEET , .. .. A 5010 65 _ j y , C ALCUL ATION IDENTIFIC ATION NUMBER PAGE 'l CALCUL ATION NO. OPTIONAL TASK CODE
~
!= ' J 0, O R W.O. NO. = DIVISION 0 GROUP jqytp LtJ2 (H ) Of A IJ7-7op s gf :rfj '-j
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= /;/d'tf 110 6 L 6/us.
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27 gf,3
- i+ E
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&6ir
{0, A Y IO l. It) 33 34 is .
,3b 36 37 18 39 - 42 .43 '44 . 4$ 'l N __-
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% 4 seio 63 t- . ) C ALCUL ATION 10ENTIFIC ATION NUMBER J. O. O R W. O. N O. DIVISION E. GROUP CALCUL ATION NO. OPTIONAL TASK CODE PAGE ')
l l n4 ^!2 G1) n'a?)20I-Svri 9 43 l 4
- REF.
3 g gg gg fg .ggp .i FD2CE Gi tMM) M f'L.M ^1U T~ Thq LAcev v k* ? N/fffd N /M LOCkl #M LOCAL N6Td7 toocp (oo e.Tp ( m') M c c o,J-(<a) 8
' E iM [,07yxth to @(YI f f X /0 l, o'/F x;o l4I'(,. Wttf D1?blSIi lo /M
- 0 ]lt ] Th.1lKQ- V ' '+ l / 0 ' A 0 Y; ?
== c. ? 97A 7f:.7 (od VMiv) -; == 1. I d v u o*5 i3 d ie, lc.11<'O lCCCi)t,7]2] h'22."lXKS E..h b a l b o.6 Wf ,
- $ G. ft v f.l$f'y iOT ==- Y, l I LL rd (6
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I 5* h 5 0O 1 I.'orw6 m = gj Q = 1. s 3 r * < D ' ==
..?] is ** [gg y c 2}c zgo / C1/ s uN '< C ~; r ~ \ @ to.200Y t b ?fl> i I$ yg =- 79 2- 1. c o ? g io** c 75 5 ?
22 (;$ys'270tro /cro y C,3* 7El vif Ti3<*v~,01~7!I
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s/ Ifllky L3 x go y' /. %'n m
.=. r )
- s
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fling = 2 Bo. f . /. 9 411 si' - : l- 4 < i 7
'I O I'l s d
( j ( ,< y ( ' revo a: 13.J t') * ) Y s .- ! a c i '. " C.) s t o. 2 v in' 'l13l10.1xso nn = w . ,. r -e< = , a ..: 31 32 33 3* T O. d 0 i
'Tc* f/t L A' l u n/
35 l 36 4Gfl ff*tJ Vph Ch SYff0 38
~~~
G S, $ $ Y } $ n 2 6 , u o, y /j 41
%c (a ovanc (= [ 5 x t o' dl'a & il y & ct,/ / CC. ** ] 10.l \
(KCff[rkt (mia s I,$X(O Lf id
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" M. . CALCULATION SHEET '
- 8
' ;' Ni ', CALCULATION IDENTIFICATION NUMBER - PAGE $
." JO. OR WO. NO. DIVISICN & GROUP CALCULATION NO.-
15454 -NZ(f})- c 7.,g . ~g p g q q - a i y -
.+
STRUC" URAL ACACEMENT LOADING SCHEDULZ G T # 3 '2.- ' NODE Pr. IOO5 STRESS PROBLD4 NO. SUPPORT NO, dT- W 13Y -h 1 - 6'Z 61 BRH DWG. REV. BRHL- /'T -- l - 4 B - CDS REV. l .Q/A CAT. M YL 4 f/d #./'ff 7'/ V BUILDING 6 /tFF G1) F W b UM @ '
- ,i North Direction d>l.D 3 % '
tl6TL_ i 30WORf' AfI A4N LD To f0' A' P 5 ~E C ov d
'AfIA4d,TFr_.C00f_i MAX!MLH ABSOLU"I VALUES o LCAD , JOINT ORIENTATION COND.
NO . , SUFFORT REAC*ICNS - Fy Fz Mx_ My M: o Fx (1bs) (1bs) (ft-lbs) Ift-lbs) (ft-lbs)
~ ( 1bs ) ' ~
j- ,
' a i '
tr y s si 2?10 66nt O o .s. e- l 5 is- ?& t h j 1 I l
'j j
I i i , i i I ( ,l
.I I i 1 . . .a- !
l l l l i
. i , j l
l
- LCADING CONDIT!CNS , ?
I 1.' NORMAL (DL + THER )
- 2. UPSC (DL + THIR 2 SRSS(CBC,0CCU))
- 3. UPSC (DL + THER 2 SRSS(CBET,0CCU)+SL)
- 4. EMERGENCY (DL + THIR t CCCE)
- 5. FAULTED (DL + THER 2 SRSS(SSC,0CCF))[WDC67GI5E) t
- 6. HYDRCTEST-
*)
- 7. SPRING SC (COLD) ,s7c7 Ye wl h ' / y g;- >
, b. h twt an. as on
l.. . . . . act 6wy - sc(0-un in-701- nrL ! .n .- - fk16I !' .;"/7RI3 51 AKl~ JOB ~ ~13,81825 A .K WONG ' e'HS'GL'EV EL =T,M SGCTA5 5= 5, T YPRDtTi CL P Y . JOB 2R
/ C J00P ARM R E G IOff= 80K , T IM E= 1, UR I V E S= 0,RE S T AR T = Y, X= 22 5 FORM S= 6001 3
! *0UTPUT.XX DES T= ( TR , SW ) ,C = ( S ', F ) , F= (X 336,6001) i
/* *****de******************************** //*
- PITRIFE * '
l? //*
- ME;2I'1TVO GIOT *
! //*
- S TURE 0 C T 113 7701525RP1:10u; ; ANY; A NY .* .
//* .' , 4 . - - - . . . l /oROU TE PR I N T -TR ' . // s' . '~~~7 6 FTE H e URIGS=4 /
- FIC HE ORI G TG =1 'RECORO RETENTI CN CENTER.401/5 '
/8 FICHE' URIGID=3 'S . ELK EL ISH/PI P E SUPP OR I EN GI N E ER ING, T R /13 ( J 15 4 54 ) '
7
- F1 C~h E ~~~C UP 1 E S =1-~ ~ ~" ~ - - ~ - ~ ~ ~ ~~
/0 FICHE CCP I E S TU =' S . ELK ELI SH/ PI P E SUPP OR T EN GIN E ER ING T R/13 (J 154 5418 /* FI C HE . T IT L E1=' SPR T .NU. C T- t- 13 7- 701- 52 5R , P ROB #1 -032 ,NP.1805' /WFTC'He i 11 L b2~=' C PS ESTI /TUGCO',P ITR'IFETME;-2T1 V00 E017FICTiEW TT70P A ' // EXEC P I TR I F E ,PRIN T =' ( S , , XX ) ' , T IM E=1 .
t // SYS IN 00 * '
~~~ TEX Ar~JTI L~IT MEN E K4 T ING~ COMP ANY -~~~ ~~C 'PS E Sil 15454 05 77 90P A A. K n0NG .
8 I S4 5 4-N Z ( H )-C T-1-13 7-701-52 5R , PITRIFE ME-211.' '
' FROU;~#1~-034 , IP;I 8 0 5T-i 18600. 18580.0 2 2 2 10.75 0.365- 6. 62 5 O.432 325.0 . @L 848. -671. O. 2834. O. 12J80. O. *CIB EI .1814. 899. O. 3793. 0. 6908. O.
OB EA ~~ TT551. z/6IT 11655". 0 ~. v. 21226. u. SSEI 3246. 1620. O. 6839. O. 12455. O. TH ER 1 0. U. O. O. O. O. O.
, LTC'Cifl - ~ ~ '~0 . 0. O. 0. 0. O. 0.
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13', ' l '8 25- A . K WONG ' ,"MS G L E VE L'=1 ~4 SG C'L'AS S= S ,'T Y PR UN= CL P Y ~~ ~iU
- ~
f4 V 7 0 JGBP A RM R= 300 K, T= 1, DR I VES =0,R ES TA RT=Y , X =531 FCR MS =6001
/00UTPUT XX DES T= ( T R , Sh ) , C= ( 5, F ) , F= ( X314,60 01 )
l // c
***r***********************************
- 8.A.P. * -
//o - ~ :*~ ' ~ " - ~ ' ~ ST-383 V01 LOO ~ ~ ~ ~ ' ~ ~ ~ ' - ~ ~ ~ ^ ~ ~ ' .l //*
- STORE CT 113 / 791525Ral:100 3 ; AN Y; AN Y ~~~~~~l
-s //o . .- .. * * * * * * * * * * * * * * * * * * * * * * = . . * * * * * , * * . * . . . * * * * * * . ' * . . ' * . * . . . . - . ~ . - . . . . . . . - - . . - - . . /*HJUTE PR INT TR , -//c ' /* FICHE ORIGS=3~' - ~ ~ " ~ ' ~ ~' " -~ /
- FI C HE~ ChlGTU=1 ' R E C Ch D P E TE N T I CN C EN TE R ,4') 1/ 5 ' ,
./oFICHE- u R I GT J=2 'S . ELKEL ISH/P I PE S UP PORT E NGI NEERI NG. TR/13( J15 454 ) '
- /
- F I C HE CCPIES=1
' ~~ ~ ~ ~ /+ FICHE CCP I E S TO = ' S . ELKELISH/ PIPE SUP PORT E AGI NEE RI NG, TR/13 ( J15454 )' /* FI C HE T IT LE1=' SPR T .NO. CT-1-1 J 7- 701- 5 2 5R ' , PROB IJ 1-032 NP.180S8 /* FICHE T I T L E 2 =' C PS E S# 1/ T Uv t.0, S T-3 8.$ V01 L9 0, FI CHE No. 7 7 9d .8c ~ // EXEC B AP, PRINT =' ( S ,, X X) 8 T ITL E 15 4 54-NZ ( H) -CT- 1-l'3 T-70'l-52 5R '
ANAL YS T A. KWONG '
' TH ICKNE SS 1.0 . ,
K ANCH 500J00 G A PA '- 0. 5 E -6
- FO R A LL A NC HORS *
~EX 27.dE6 ' '
BOX 1 1 N1 2. 3 -N2 2 2 N3 32 DUTATE AT TACH 1 -21. 73 D EG C G AT 11.5 6.25 Jt jlV 1'1,2.v' led.0 1,3.0 1,1,125 1, 2. 0
# i IV-1 1.2.25 ' 1,2.375 1i3.25 ,, 1,4.375 1,2.3125 - ~ ~ ~ ~
L A NL H 1 Al 1 1 A2 1 4 A3 4 1 A4 44 i PM OVE 1,1 0.0,-0.25 PMGVE 1,4 0.0.0.3125 ' .. PMOVE 4,4 -0.25,0.0 PMOVE 3,4 -0.25,0.0 PMCVE 4,3 0 .5,-0 .675 ' -~ ~~ ~ ~ ~ ^ - ~ ~ ~ ~ ~~ ~-~~ ~~~~~ ~ PMOVE+4.2 0.5 -0.675 ALLOW 5364. 4532. 1.67 TLLAD 1 . J ALOA0 1 1 11449. 11584. 29068. 0.0 8456. -3370. RUN SHEAR YE S Rd N ' AN5 Y 5 ~ YE S-END
/* ) . w .e -gse.-- . . . . - e.. .m. , --.eo... . . s,s. . .-ee .+ -.... .. ,$ 'k ' .-- -- .- - .. ... ... - .i W
b
1
'*h * ,I 4 m +, ..~ w , w >
9 _. i
% pag "r-i 1 .
L , ATTACSCENT14 I , ,i 1( 1
~Page 1 of 6
- ). _ CALC. 'NO.15454 - NZP. Cr-t ppr_y _ q
! %J,
; DETAILID PIPE SUPPORT @lYS'.S CHICKI.IST '( Qf.4jj Ag y d 3,,y ' 'i l . . .
LA= Acceptable l ,
- g. . AR = Acceptable as' Revised -- +
A RR = Rework Required N/A = Not Applicable. t i s Item Status Remarks Function' Check s A' AR RR N/A
- 1. ISupportperNrmsits M i i m intended. function T 2.: . Correct' relationship between pla'at. north.
and global direction as indicated on' stress isemetrics - Frsces: A ~AR RR N/A m, 1. Member si:es and materials' .
,;g'y. agree with drawing "
(material substitutions: noted). ; _ _
'l
- 2. k' eld sizes , types , and !j lengths agree with-draving. 3
[ls
- 3. As-built frace< geometry is equal to.or within the envelope of the designed frame geometry _ _ _
f ; j!
+
- 4. Additional attachment i loads such'as conduits, etc. have been con-sidered. . - _ _
1
~.
i Support stiffness is ; provided for Class i j l support v f
- 6. Frictf.on Forces /vith !
proper direction considered _ _ _
/ l
{ r i l 0113-1545405-HC4
- ,1
k.,, n .; 1
~ , ;~ . . .'.g- w i
- m. _.;
s i ATTACHMENT NO, t PAGE 1, 2. )
1 k CALC. NO.' 15454 -NZ"}l"-' cr-N39-70 imp .Fage 2 of 6 e
$.f i '%e' .7. JLocal. stresses hue to bearing,. cinched ' ?I U-bolt, and pipe' i
l expansion have'been- )) evaluated _ _ . _ . _
.q A
j
8. ' Support weight self-excitation bas'been .
lj evaluatid- JJ
- 9. Input orientation of-computer model (if l,]
i applicable) has been-properly evaluated i (i.e., member.and i S angle, etc.) .! Support loads have
- 10. .
been properly ' combined. -
- 11. Frame clearance eval- 4 uation (in acrestraint direction)_ considers '
pipe movements.due to-jf# . deadweight, ther nal,- .. ; :l Dc/; . and dynamic. loads (such
'i ~ ' .as seismic / fluid , "
transients)- _ _ _ Serine' Haneers: ' t
- 1. Spring sine aad associated ' component sizes agree with-drawing. _ _ _
/
c 2. Hot-load and cold load reflect as-built loads and working range of spring is consistent / with stress report. _ _ _
'L Spring hanger meets all j ICDS requirement limi-tation _ _ _
4 Veld sine, type, and , length agree with / drawing. _ _ _ s , il! . o . ; i 0112-1545a05-HCa 4 e
y e4 .7-
-g a; ,
a i ;.. 9 ' <.- ,; ,. N /J5ACEZENT 7'U,' l PAGE I.3- ; i sc y s L CALC. NO.' 15454-NZ"ll'- C'-I-137 - 90t-5sr < f l Uigi . Page 3 of 6. i k.If 5. Piping displacements-(due t.o desc/-4ght, , thermal, seismic, and , r fluid transients, etc)' t
-M i ' considered. ..
I f
- 6. Variability of spring hanger is within the
/ ') ' limit- * *I
- 7. Support l'eads'have been properly.com -
-binded.
r ' j , q n
, . 8. . Swing angle and' , ~ )
movements'are within. /., -j allowable. _ '_
._ g -
j
- 9. Pipe properly guided- ,' *
-l against. lateral move- J. ]
ments'with respect to , , l trape:e spring hanger ,,,,,,, _ _ ,__ r 10.. . Local stresses,due to a
. .. bearing, cinched U- 1 3 ,,) bolt, and' pipe'expan- 0 ' d v M. *;p . - sion have been _ _, 4 evaluated .. -i _, / . 1 i Saubl5 irs /Etr'ut$ J. # >
x
- 1. Snubtrer/s trut s ize . 1 j < j f agrees with drawing. e v .
o
, 3 . . 2. Sadber/stru[ direction 4 of restraint agrees > 'M j j
with drawing./f
,y ,7 _
- 3. Shubbfr/s6 rut end.. ,
bracket wcld size, ty;e, and length agree wi n ' ! drawing. ( > i Soubber/ strut meet.5:'11
~
4 a [ LCDs requirement: 5 and l
' i limitations. ./ >b7' . . - ) '1 - - - - - .y 1 -] a
- 5. . Support leads have been properly combined. _ _ _ _
l
/ Scubber settings reflect t
[ ' $6. an-built movements from
.-- '. / J' stress calculation, in-cluding' travel margins. _ _ _
l
' f r O'113- 1545405-HC4 ' 1 f . J </ l = - _ __ ___ . . +
0: ! I .' .* , gg l qr d- <-
..' Trracte rar neti
_ pacz t a , CALC.' NO.15454-NZ"H- cr b l37 COMER page 4 of 6
'7. Swing; angle is within .
allowable.- - --- o .. l- g. Pipe movementss (due to - ! - deadweight, thermal, seismic, and fluid , transients, etc) _l considcEed. _ _ ,,,,,,
- 9. -Local. stresses due,
.. )- : tc:aring,-cinched q U-bolt, and. pipe ;
expansion have , been' evaluated . 1 i Inteeral Attachments:
- 1. Trunnion /padfhg size agrees with drawing.
- 2. Trunnion /p2dttug meet' .
size criteria _ _
" 3. Weld si:es, types, and '
4
?p lengths.agr e with 2p ' drawing \ '~ ~
- 4. -' Support loads bsve -
been properly combined. _ _, _ I
=: 'TwE Aucwet.c Lct.o nas eaw AEovcac Tc Ac.cs.wr ace pigg spT. ./ !
- 6. Local st'ress has been f-l properly addressed.
f Base plates /M tMets , 1 1., Base plate size and . { 1 bolt type and size agree , with drawing. _ _ _
- O r
- 2. For base plate designs, bolt and attachment locations are within tolerance and m2.c mum /
edge distance was s/ l j maintained. _ _ _ I 3.< Richmond inserts and threaded rod have ' / been evaluated.
- ~ ,
ff
- 0113-1545405-HCL -
7, . . y ) ,. $ j g. iPig,.,N, ,; y , M T:n ;. .s _ i# -- 4 H y' y AITACHMENT; No , 1 PAGE )m m o :.7 [ ..,' 4 CALC.~ NO.15454 NZH- cr 33.b\-525R
'8'
!. - l 4. Bolt - spa cingsl and X. j L t' K eabedment~ lengths l
- i. : are considered in I? f ; detemining bolt e ')
L > allowables. ... j g :{J
,LS. Bolts separation . violation (EISV) l U- with adjacent supports _have been considered- _ _ _ .-Bolted Joint Connections 1
- 1. . Bolted joint con-
+ nections have been .
evaluated. _. _ _.
- U
- 2. Bolt' torque require-
~y 'ments have been'evalu-atedi _ _ _ / .,
4 l
.3. Locking devices-provided' _ _ _. /.
9;
. '. s Calculation Documentation: ;"s,v - 1. Support category _,
(nuclear or non- , nuclear safety- 1 '
,related) is clearly defined _ _ _
- 2. Input data / Output data clearly identified /
. distributed
- 3. Consistency between the stress calculation /
support calculation _ _ _
- 4. Consistency between hK LUD") h ,
support drawing / support ;g c , gg go 2 010 [N m' f) ' calculation - -
- 5. Latest outstanding change'on support incorporated _ _ ,,,,
/
- 6. All items in analysis section include proper references and, refer-
- - f 3
,y ernees are up to date _ _ _
Oll2-1545405-HC4 , l e i_:__z______._______.___
i
. ,; y n, :-- .> > ,
A7"ACEMER No, I ~ PAGE- LA I,
..- --CALC. NO.' 15454 - NZ"H"-dT-l- 137 -70) . 525t Page-6 of 6 . ! o ,. s a
y .. I
- 1
- 7. ' All' acceptable computer ,
g M}h ' runs are properly ~ - p; documented on' computer
- log _ __, ,.
1 8'. ' Summary of.results satisfies objectives. ._ _ _
,+
Reviwer's. Evaluation:
$0WoTT- M h T@YM g j
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stoNc a cressTrn rNsiNetRiNo comronAttow L ,,,,,. - CALCULATION SHEET e; g - C ALCUL ATION IDENTIFICATION NUMBER el. 0. 0 R w. 0. h o. DivislON C, sROUP CAL CUL ATION NO.
' (-' '
15454 NZ (4 ) 07-1. IM -W -hst OPTIONAL TASK CODE PAGE H - I < c-9, e r 2,3 g
, a
- 8 4
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- I l
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,, A?tACIDiENT No.
88 TITLE: SUPPORT (s) . LOADING BUywARy j es 1
-44 .,
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* ~ .. STONE 8, CEBSTER ENGINEERING CORPORATION 4 .. . CALCULATION SHEE1 '
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- C ALCUL ATION IDENTIFICATION NUW8f R
. J.O. O R W.O. N O. OlVISION 0 SROUP
( 15454 CALCUL AT40N No. OPTIONAL TASK CODE PACE b*I 4 NZ ( H) ~ 51- 137- bk%5 E ~2 or 2, .G - 1' 8 Ie : $ e s .1 4 *
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e e It ATTACEMENT No. 3 ,
. it TITLE: MCPEAL 444 O (P5H-;-39Q IS .i6 I? .
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DESITIN CHA,NGE PACKAGE-(DCP) , ' AUTHORIZATION FORM ATT , 3 T%6 E '3.'2 f',' CAtc, >Jo, 154 54- (@ - ci-n -131 - 7ol -625R DATE: .( DCPNO.b_3rr(br REY. O THIS SUPPORT REVISED PER StJEC SU W RY: '
SUBSYSTEM N0. 4 80 A ANALYSIS - hEFERENCE -kS[T)-l //h #7 _ 7
" BRH NO. OT- l- 139- 90l- S E)Q BRH REY. '
! C.W.0. h0. I ' , 1j DESIGN CALCS WILL REQUIRE FUTURE CONFIR-MTION BY SWEC RISK / FINAL ENG'R. BASIS IF THIS SUPPORT IS REMOVED FOR THIS MODIFICATION, PROVIDE SYSTEMS OPERABILITY: TEMPORARY DEAD WEIGHT SUPPORT. , , j . APPROVAL: Date Project Disciplina Supervisor-PSE APPROVAL: Date Tech. Support Engineer Rep. (TSER) i START WORK AUTHORIZATION:' Date ITF/WG Supervisor PHYSICAL WORK COMPLETE: Date ITF/WG Supervisor POST WORK TESTING COMPLETE: Date ITF/WG Supervisor CWO/DCP CLOSE00T: Date ITF/WG Supervisor
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. cn no, s% - pun- cm rh3 -w-se . M , e> paw se l ' INTEROFFICE MEMONANDUM (o.g,g0. 15454.05 PSM- [-79 7 COMANCHE PEAK STEAM ELECTRIC STATION )
(g - SUBJECT PIPE SUPPORT MODIFICATIONS DATE /dj/gg ' MF REQUEST FOR SWEC-SEO ACTION FROM R. R. Wrucke 4 CC See below S. M. Feldman - 1/All , Reference As-Built Stress Problem No. /- 0 3 2. _ 1 As a result of the headquarters requalification effort, These it hasactions been determined that further action by SWEC-SEO is required. include design qualification completion and . issuance of appropriate ' drawings, or change documents, to qualify the supports listed on Table 1, _a tached. i Original calculations. TUGC0 or SWEC (if gene :ted), are aise attached. j These calculations document the extent of the e,;.:ification efforts a; ready ! completed at headquarters for these supports and provide ccre specific details on the items requiring SWEC-SEO action. Attached are applicable documents f or proposed modifications (per CFFF-7, Rev. 2): l)() Support summary sheet 4 b 2 380 /T [# C C 0 2' 7/ /bb
/ //
{} Piping isometric (work sketch)
.M () Basic piping analytical data sum =ary ..
[] Attachment M d y,t-.a. Prucke i RRW:bjf attachments cc: R. P. Klause - 1/M C. A. Fonseca - 1/M B. S. Moscow - 1/M ,ID OCT. 2 01980 e e. ar .a ! A. Kamdar '- 1/M+T B. W. Porter - 1/M J. Burgess - 1/M+T R. Normandeau - 1/M+T
)
R. Gustafson - 1/M+T
/ J. Ryan - 1/M+T A. Leonard - 1/M
- 0. Love - 1/M+T Lead Supts - 1/M+7 J 4Ad [ -
A. W. Chan - 1/M'T J D. Parika - 1/M+T Il Job Book R2.1.2 - 1/M Job Eook R4.1.1 - 1/M+T R. R. Wrucke - 1/M+T
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tc n-f m" - [ if.,, )s)O f Y,Mk-h.h S - CT' l o bh. hol Page$of -$h} 2h][ *2] pg.,gg 2 ;'.d 's.it, i yv. . ,, Project Log No. orc- (l-03D-0 C '---
^ <-- i- ..PlyE STRESScAND SUPPORTS y , .P;' ble.m No. 1-032-
- e, r1660
- 4. f'y s Pa6PostDMODIFICATION' REPORT Supt . ?!k.0 CT-1-137-701-S(/fa - '
' s 7 NUPIPE RUN: R$a 000).
- 7. Job #' 6007 Co=cnshe Peak I /dUnit 1 I- JUnic 2 :
LProj ect: .
~ ~~ > ' N CC- 89 4 Date 6.24 .. - 1 Sys tern .
Con:iintnent Sprav . . .
.i.
Statenent ofLCendition: l 1 Pipe Overstressed % Over Allowable ,
.Suppor: . Overloaded ,i .m * % Over Allowable No::'e Overicaded' hver Allowable % Over Allowable.- 'Other' Ancher bolts fail, t . Details:
t l
- x. _
Syste= Para:e:ers: Stress Allevable-Te:ptra:cre Pressure Suppor: Allowable '
;g, . '
Others: [ihl.-: Transient Data: %
. Attachments Calculation.#
Ref. Duss: '3RP 71ov Disgram # , EFJ!L - BRE CT-1-137 001-552R Fev.1 Others CE'd To be modified bv fie2d ac necessarv
- Project Sugges:ed Solution:
o b' in
' EC Reco:: .er.da: ion: y // / / [ ' 22-W_
Prcpec _Ingineer Responsible Eng:neer A h(* $. ?w-dkw -
.a /
l2 C"~60 IB G~-D Df C f F v i & D __ A.) C 7 h?C. DIG / G AT t .Y , h EM S)L e nf A 7 T NC7lficcNer. 'v i c, ?SA~ l ' ? $ ? ' W#'
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^^'_ - - .,,/- - D < nr i % q '-] -i i.- , , . .'~'..-- - a w~~~ vt w t si/ i Date Opt : en Review Cc:nsi;t e c
, , , ; n; ^; . \, ,I,.],ftf,, MD'. hkk -' 9 3(h -CT .- } - IM -IrOl -d,- $R [7 3 f[*iGf .3 7 , ;' C INTEROFFICE : MEMORANDUM ' 'sog g, 15454.05 '
HOC- 894' 1
~
PIPE SUPPORT-U "i.
- SUBJECT ' "7
PROPOSED MODIFICATION REPORT ' c G PIPE STRESS PROBLEM 1 032 l FROM . RJBelang er - COMANCHE PEAK UNIT 1 . t TO'
- o. .RRWrucke NYOC/36 CC WJBenson v/o attach.:
,, BJExcell NYOC/36;w/o attach.
JWKuhlmann:dls'w/o attach.: ESMoscow NYOC/36 w/o attach.. I EASweeney.v/o attach. 7 Job Book R2.1.9 m Job Book R2.1.16 .i ' Job ~ Book R4.3 Job Book'R10.9 The' proposed Modification' Reports-(total cf 4) dated July 22,,1986, for the pipe supports (t6 cal'of-6) contained within the boundaries'of Stress Problem 1-032'and associated original TUGC0 and;SWEC calculations are attached for . s your review and recommendation.. 3 Note that'the original SWEC pipe support calculation for supports (Tal-013-009-522K, CT-1-013-011-S22R and Cr-1-137-701-SS2R' vere based on .
,,; CPPP-7,. Revision.1 pipe stress londs.f'OiIr review of CPPP-7, Revision".C - . , pipe stress loads indicates'that these supports vill remain overstressed.
M- . Note that support. numbers CT-1-013-023-S42K and CT-1-017-046-S25A ar:
@' , currently "on hold'? awaiting. receipt of loads. The need for possible required modification of these supports vill-be identified upon receipt of loads.. * ) '
i R.
. Belanger .M_. -
Attachments ' 4 I1655 l c T- l - Ol 3 - 001 - s 4 2 R
, I I656 l. CT 013 - 008 - 5 22 K 16 5 ; ) CT- I - 013 -022- 5 42 K ,
l 16 5 8 - l CT 013 - 009 - 5 21 K
) LL6ssI c T - l - 013 - 0 l l - 5 22. R Il660 l C T - I - 13'7 - 701 - 5 2 S R
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