Text

Rev 1 to Calculation M-8, Pressurizer Surge Line - Class 1 Piping Analysis
	ML20107B306
Person / Time
Site:	Davis Besse
Issue date:	01/31/1985
From:	; BECHTEL GROUP, INC.
To:	;
Shared Package
ML20107B302	List: ML20107B306;
References
	M-8, M-8-R01, M-8-R1, NUDOCS 8502200336
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t

- SURGE L HI SUFFRZ5501/EANGER 14 ADS ,

{ (See Figure 4)

Type of Loading Forces (Kiss) Moments (Ft-Kiss)

Fx Fy Fs Mr My Ms Dead weisht 0 -3.8 0 0 0 0 .

ont 7.5 h 3.2 0 0 0 Dst 13.7 3.8 0 0 0

'P R o s . H o . n - t (*)

1 ATT AcHMS NT 41 .,

SHT. No. 1 oF IM

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pagg s.3 stel&L 3002/uss-14 h5stBAft: APRIL 7. 1972 Sebtesk & Wilsoa m . . . . . . . . - .

D i.

l

. -. - 3

. e

. 3

_ l i . !

Introduction '

)

. , c This report contains the stress analysis of the surge lias. .All I. ,i points in tlGr surge line are analysed including the biastallie wald at ;

1 thehoting$surgenossle. The analysis of the intersection at the pres- '

q j\

suriser end is contained in pressuriser Design Report "8 urge Nossle Analysis". ; ,)

The braneh intersection analysis is cdontained in this Design Report under a jl

- different section " Surge Nosale". j!

i o

Results l

1 All points in the surge line satisfy primary stress limits either in :

acco.rdance with equation 9 or per Appendix r of the 331.7 oods. .

per equation 9 simplified analysis i unw== Primary 8 tress = 2207k.06 psi <15 8 Marians for an elbow (joint 3) = 22074.96 pf <= 24800. poi 24800. psi e6708F i 2 -

l Maxiina for a straight (joint 1) = 1Gt20 536 psi < 24800. psi .

j ..

l !<

All points in the surge line do not satisfy the 3 8, primary plus secondary I l

stress limit. However, calculations are paavided showing that an Elastic-Plastic -

Analysis is applicable. 54 i l l u=w== primary plus secondary stress (sinstallie weld) (joint 54)

= 75997.62 psi ) 3 8 = 50100 psi e650.*F (PAG E C-il)

M f

Mad == primary plus seccEdary stress for.an elbow (joint 2) .

p

= 67368.71 psi) 50100. Psi (Pear c-13) j Primary plus secondary stress for cycles occurring more than 240 tiass: ;

Joint 2 = 36860.4 poi < ~3 8, = 50100. Psi ! L Joint 3 = 33787.9 psi < 3 8 =

Joint 19 - 36929 7 psi < 3 f, =50100.3 m00 poiPsi Maximas Usaae Factors: .)

e!

e j

Usage Usage Factor at Biastallic Factor for weld (j(oint joint 3 = 0.04s 1.0 =2)allavable

= 0.37 ( 1.0 = r.11avable L '

usage Factor for Joint 19 = o.oM < 1.0 = allowable i Pet.o S . N o. 14 -8 (od &f. ,,J/reas Analyso.s *f J.*q s AtrACHM M T# 1 'I'E Y d N- e jf n4 4 Ga C*~ry ,

('

~'

Sny, ae. 3 af }4 p.<t,- B=srel C 20* *!4-50, -

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ASE : Y f* $ I"30~ f S Cp/& Q

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T .

This section demonstrates that all points in the surge line satisfy primary stress limits according to either Equat, ion 9 or Appendix F of B317 A flexibility analysis was run for dead weight, and either (x + y) or (s + y) earthquakes. The moments generated by this analysis are shown on Pages A 4 thru A-7 These moments are then combined with design pressure of 2500 Psi to generate primary stresses in accordance' with equation 9 using applicable indicies. The indicies used are listed in the stress output. Two cases were ran: 1) pressure, deadicad, (x + y) earthquake; 2) pressure, deadioad, (x + y) earthquake.

The results are then compared to 15 S, at 670 F0 for SA-376-TP-316 -

(straights) and A 403-WP-316 (bends). Part of the surge line actually has a

< design temperature of 650*F. S ,= 16,500 psi. for both materials thus the

t. _]i allowable primary stress is 15 (16,500.) = 2i+,800 psi.

The largest primary stress is 22071 4 96 psi at joint 3 for the x + y earthquake at an elbow juncture. Complete usults'are tabulated on Page A-8 and 9

. 7 gos, w o- M - 8 (ol) l ATTACHHIEN T # I l

i sHT. No. 4 of 14

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STCESS IMOICES 4 _ _ . . _ .. . . . . . .. . . - _ . . _ - - (JOINT CLAS$1FICATIONS . . .. . - -

- .. ... . . TYPE . .

DESCRIPTION. - - - -

1 STRAIGNT PIPE, REMOTE FRON WELOS OR OTHER DISCONTINUITIES 2 GIRIN SUTT WELO SETWEEN STRAIGHT PIPE.OR SETWEEN PIPE ANO SUTT-WELOING COMPONENTS. FLUSH

.. __ . . . . . ... . 3 .. .. GIRIN SUTT WE LO SETWEEN STRAIGHT PIPE OR DETWEEN PIPE . ANO. 8UTTrWELOING COMPONENTS.. AS.NELDEn __. __

4' GIRTH FILLET WELO TO SOCKET WELO FITTINGS, SLIP-ON FLANGES, 04 SOCKET-WELDING FLANGES.

s....... . .. .

5 LONGITUOINAL SUTT WELOS.IJi STRAIGHT PIPE. FLUSH

... .. . ....! 6 . LONGITU0INAL SUTT WELOS IN STRAIGHT PIPE 4.AS NELDEn .-

J_.

7 TAPERED TRANSITION JOINTS PER SUBPAR. 1 727.4.2(Cl ANO FIG.1-72F.3.1 8 BRANCH CONNECTIONS PER SUSOIV.1-704.3 9 . CURVED PIPE OR BUTT-wELOING ELBONS PIR .US AS 816.9 .USAS_816.21._DR_ MSS SE4a ,_ ,_, _,

i t

18 BUTT-utLDING TEES PER USAS S16.9 04 MSS SP48 z.t...... . . . . . . . . _ _ _ . .

11 SUTT-NELOING RE00CERS PER USAS S16.9 OR NSS SP48 %

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_ _ _ _ . _ = - - - - _ -

SECTION PR0PERTIES

OUTSIDE OUTSIDE MONENT BEND SECTION . RADIUS._.. 0!ANETER TNICKNESS- _.0F INERTI A RADIUS _DESCRIP. TION _ . .. ._ _.

SINI IINI IINI ( IN"8el IIH) t '

.. . . . . _ . ._. 1 ..... . 5.3751b.... 18.7508 1.000J _ ... .367.885 KU RG E._LIN E..S T. . _ . . ._ ._ .

2 5.3750 10.7500 1.0008 367.005 15.0008 $ URGE LINE CR.

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11 4809.10 128.24 1611 11

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14 942.24 426.09 1794f94 10 23 1eSt.2r tes.2e 512.r9 36 ._ . 180.86 .- _251.45 _.. 142.st.- __ ..

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1 552.91 STF4.54 13644.50

1C91.14 ._ 3158.34 . 8890.93.. _.. __

3 552.91 1462.31 19615.8e 5 803.58 3093.78 583F.96

. . . . . 6 . 552.91 2393.62 415n.89 .._ _ ___ ..._...

F 803.58 2984.70 F184.48 11 2332.98 3832.C1 536F.42

. 12 .- 2374.46 .. 4664.09 . 5367.42 - - - -

13 1686.F2 208F.29 5367.42 in 1924.39 1927.74 5317.F4 MM C H NE M # 4

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16 762.69 1927.74 1976F.6'.

18 2778.96 1927.74 5636.34 PROS. t4 0 M- 9@9 23 _ .. 552.91 .. 2913.2F .__ 5693.95 ._._ . . .

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3 166.49 371.99 F46.12 - . . - . ._ . . . _

5 4CS.67 782.55 235.87

. _ . - . 6 _. 186.49 . . . 611.C2 .... 711.74 . - - -

7 48S.67 744.95 767.22 3

11 1145.29 1185.58 4'36.78 .

. . . . . . 12 881.24 1481.76 496.74 .... _. _.

13 948.49 471.82 496.78 I 1866.14 in 571.52 381.27 *

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16 2.21.F4 571.52 445.15 8

to 773.38 571.52 711.91 23 186.49 . 788.29 . 522.34.. _ ._

36 241.32 411.28 768.88 . _ . . . _ . . . . '..

54 1842.98 1347.92 1561.55 )

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1 2433.64 7961.39 4184.12

.... . 2 ..- 3388.12 . 8215.63 18 012.18 -.- . _. _ _ _ _ -

3 2433.64 2335.87 3456.56 5 3399.71 276F.35 1725.99

.. . 6 - 2433.64 - 4134.19 - 2241.79 .

7 3399.79 5695.74 6636.94 - . .. _. -

11 6557.96 5244.52 943.78 12 . . 8413.33 5365.99 . . 943.78.. . . - . . . . - - . . . . - - , _

13 6341.99 2a92.85 943.78 .

14 15 4395.61

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16 1675 18 3892.7F 2984 58 . . - ...

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A rT A CHM E r4 T :# 2 36 2629.71 4271.87 1651.72 54 4643.93 9844.89 3448.78 /

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t .. . . . _. _ . . . - - ._ _ . _ . . . _ . . . - . . . . . . .

l PR! NARY RATIO To

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2 9 1454.47 4538.64 *15454.06 16172.28 1.0 20 190F4.58 .FF1

10 3 9 179e.67 2222.71 ll....

t 5

6 9

1 1223.34 1795.67 4256.1s 3011.64 24615.1s 6236.se .

94tF.85 24rse.it 764a.se-19039.13 1.s 1.s

.5 2.s 22sr4 96 2.s - 161 s 3. 6s 10 s479.26

.s92

. 651

.343 O .

r 9 1223.34 42F1.Fs 11317.13 1215s.18 1.s 2.s 176F5.41 .F14

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PRIMARY RATIO TO I JOINT TVPE ME 81 HY M2 MEIS 82 STRESS ALLOWABLE

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PROJECT.9 W.9 .. W .4.. JOB N )M9) STANDARD COMPUTER PROGRAM ME-210 REV NUM...l.. SHEEI - Q OF un a \ .

VERSION : 5 RELEASED : DEC 15, 1982 I USER MANUAL VERSION : 1 THLORETICAL MANUAL VERSION : l VERIFICATION MANUAL VERSI0'N : 5 B I J L A.A R D S T R E S S A N A L Y S I S F 0 R C Y L I N' D E R S PSU-R1 TTACn. NO: {

SHf f 48' 3 0F 4 i I N P U T D A T A ~

P ML MC MT VL VC NA MB , pgog. No. NI (LBS) (IN-LBS) (IN-LBS) .jlN-LBS) (LBS) (LBS) (FT-LBS) (FT-LBS) 1 2400. 0. 20400. O. O. O. O. O.

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y O. O. v 3 2400. - 0. 20400. O. O. O.

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(IH) (IN) (IN) (IN) (PSI) (KSI) (IN) '

1 1.0000 13.2500 6.6250 6.6250 CIRCULAR .0000 .0000 .0000 :

2 1.0000 13.2500 6.6250 6.6250 CIRCULAR .0000 .0000 .0000 l 3 1.0000 .13.2500 6.6250 6.6250 CIRCULAR .0000 .0000 .0000 MAXIMUM PRIMARY PLUS SECONDARY STRESS INTENSITY

.l i 1.0000 -1.18 .63 -1.18 .63 -5.06 3.87 2.71 -2.61 MAXIMUM PRIMARY.PLUS SECONDARY STRESS INTENSITY ,

1.0000 .. -1.91 1.03 -1.91 1.03 -8.21 6.30 4.40 -4.25 .

, MAXIMUM PRIMARY PLUS SECONDARY STRFER 1 TENSITY 4 1.0000 -1.18 .63 -1.18 .63 -5.06 3.87 2.71 -2.61

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ORIGINATOR 9.h.9.h.b DATE.U.\.I? CHECkEP. I . f.# ... D A T E .'.'.I.". /.D- CALC 'HIN.I.N.E.D.~ I .

PROJECT.D M L .M$i ?.. JUB 11 U@.) ' SIANUARD LUMPUIER PROGRAN NL-210 REV Nutt...\... SHEET - M OF

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'P R O B . N 0 ' M-f ********* NE-210 POST-PROCESSOR (VERS. B) 12/8/81 ********

" I y r A CH = N0' k l' DO YOU UANT TO ENTER PRESSURES AND OTHER STRESSES (YES OR NO)? >YES ENTER ACTUAL PI,PE 0.D.~AND UALL (INCHES) 0.D.,U? >10.75,1.0 o, 4 oF 4 3

ENTER OPERATING AWD DESIGN PRESSURE (PSIG) P-OP.,P-DES.? >2750,2500 M* "

~

IS ALL DATA 0.K. S0 FAR (YES OR ND)? >YES ENTER FOLLOUING STRESSES UT,0BE,SSE,THRM, SAM (KSI)? >.825,4.415,8.203.4.546,0.0 -

g,3g _ g gi ENTER SM STRESS ALLOUABLE (KSI)? >l6.48 Q g.

IS ALL DATA 0.K. (Y,ES.OR NO)?

PIPE 0.D. = 10.75

>YES

@l

/

PIPE UALL = 1.000'. . - h, glq WM -

DESIGN PRESSURE = 2500 gd ?

-. p .

OPERATING PRESSURE = 2750 .

UElGHT STRESS = .825 UBE SIRESS = 4.4'15 SSE STRESS = 8.203 THERNAL STRESS = 4.546 SAN SIRESS = 0.000 ALLOUABLE STRESS (SN) = 16.480

^

CHECK VALUE ALLOUABLE IA 1%.03 24.720 A--* M F. 4~

f '

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FROM THE NE-210,RUN FOR LOAD LASC 113 AND NUST SilLL BE BEL'0U THE SPECIFIED ALLOUABLE i i. m

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'IIHE h. .044;5 FURPUR 2SR3A-01 974Til 11/30/84 10:47:25 rt!D PACIC TEXT =7.70Cdl. SYN =? ,

Annex $4-371 Code Case N-411 Alternative Damping Values for Seismic Analysis of Piping Section III, Division 1 Class 1, 2, and 3.

Question:

What alternatives to the damping values given in Table N-1230-1 Appendix N,Section III Division 1 are acceptable for use in seismic analysis of Class 1, 2 and 3 piping?

Rep'ly:

It is the opinion of.the Committee that for Section III, Division 1, Class 1, 2, and 3, construction,'the damping value for seismic analysis of piping shown in Figure 1 may be used as an alternative to those given in Table N-1230-1.

Appendix N.

The damping value in Figure 1 is applicable to both OBE and SSE, and is independent of pipe diameter.

This Code Case number shall be shown in the documentation for this analysis and on the Code Data Report.

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