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
	Download: ML20107B306 (32)
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Mulaar Power Generation Divisi..

GENERAL CALCULATIONS

. (,

AyyAcHHENT #2.

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L-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 7.5 h 3.2 0

0 0

ont Dst 13.7 3.8 0

0 0

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

ATT AcHMS NT 41 1

SHT.

No.

1 oF IM

(_

Q p.

Mt :

l P T f

v

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m.r< : i-si-b v

(

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

D i.:

3 e

3 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 j l different section " Surge Nosale".

j!

i o

Results 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

i unw== Primary 8 tress = 2207k.06 psi <15 8 24800. psi e6708F Marians for an elbow (joint 3) = 22074.96 pf <= 24800. poi 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 54 Analysis is applicable.

i l

l u=w== primary plus secondary stress (sinstallie weld) (joint 54)

M

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

=

3 m00 poi Maximas Usaae Factors:

.)

e!

e Usage Factor at Biastallic weld (j(oint 2) = 0.37 ( 1.0 = r.11avable j

Usage Factor for joint 3 = 0.04s 1.0 = allavable 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,

~'

Js.n 672. (6te v 1, f

e Y f*

$ I"30~ f S Cp/& Q ASE u a c I-chQ

? bdLOY6A

.4J4145

=

-u

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

1) pressure, deadicad, (x + y) earthquake; 2) pressure, deadioad, (x + y) ran:

earthquake.

The results are then compared to 15 S, at 670 F for SA-376-TP-316 0

(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 96 psi at joint 3 for the x + y 4

earthquake at an elbow juncture. Complete usults'are tabulated on Page A-8 and 9

. 7 gos, w o-M - 8 (ol)

ATTACHHIEN T # I l

l i

sHT.

No.

4 of 14

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STCESS IMOICES

- (JOINT CLAS$1FICATIONS 4

-....... 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 pro 3. No-e4 - P (e08/

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O TOLE 00 SURGE LINE D

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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....

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2 5.3750 10.7500 1.0008 367.005 15.0008

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803.58 3093.78 583F.96 6.

552.91 2393.62 415n.89.._ _ ___

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166.49 371.99 F46.12 5

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13 948.49 471.82 496.78 I

in 1866.14 571.52 381.27 15 117.54 410.45 496.78........

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to 773.38 571.52 711.91 23 186.49.

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O nonEmis in Fr-Les.

stresses in est.

t l

PR! NARY RATIO To

!O JOInr Tvet nx nv n2 nili si e2 STRESS Alt 0W ABL E

!j 1

1

._ 179 e.6 F.-. F4 F5 54 -. 184 29. 78.. 19968.65

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13 9

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TOLE 00 SURGE L!rt EQUATION 9 - PRINARY STRESSES CON 0! TION......

PRESSURE, 2+Y EQ, OEAD WT.

EQ 9 I

MOMENTS IN FT-LOS.

STRESSES IN PSI.

PRIMARY RATIO TO I

JOINT TVPE ME HY M2 MEIS 81 82 STRESS ALLOWABLE 1

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4890.38.

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5993.98 10 2.8 15526.79

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TOLE 00 SURSE LINE EQU8 TION 9 - PRIN8R STRESSES I

CONDITION X*v Ott Ot40 WT., PRESSURE..'.

EQ 9 e

MOMENTS IN FT-L85.

STRESSES IN PSI.

f.

NLl#'^# E I PRIMARY RATIO TO JOINT Tf;C MX MY MZ M(Il 81 82 STRESS ALLOW 88LE A O S' 5 et 1

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2024.62 F120 88._.113T4.37 17571.34 8.0 2.8 18167 98.

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6 1

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7 9

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9 8 0 3. 2 4.~. 8 767. 98 _12 2 69 16. _ 17 9 8 6. 47

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DAT2.E. 9..N CHECKER..I...#.

D A T E. '.'..'.'.

CALC NUM.

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 TTACn. NO: {

PSU-R1 i

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

~

NI P

ML MC MT VL VC NA MB pgog. No.

(LBS)

(IN-LBS) (IN-LBS).jlN-LBS)

(LBS)

(LBS) (FT-LBS) (FT-LBS) g Q9 1 30-( t 1

2400.

0.

20400.

O.

2 3900.

O.

33150.

O.

y 3

2400.

- 0.

20400.

O.

v VESTHK VESDIA C1 C2

' SHAPE PRESSURE SM BENDRehlk I\\

1g

k (IH)

(IN)

(PSI)

(KSI)

(IN) 1 1.0000 13.2500 6.6250 6.6250 CIRCULAR

.0000

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.0000

.0000 l

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1.0000

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.63

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.63

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-2.61 MAXIMUM PRIMARY.PLUS SECONDARY STRESS INTENSITY 1.0000

-1.91 1.03

-8.21 6.30 4.40

-4.25 MAXIMUM PRIMARY PLUS SECONDARY STRFER 1 TENSITY 1.0000

-1.18

.63

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CHECkEP. I.

f.#

D A T E.'.'.I.". /.D-CALC 'HIN.I.N.E.D.~ I

' IANUARD LUMPUIER PROGRAN NL-210 REV Nutt...\\...

SHEET - M OF PROJECT.D M L.M$i ?..

JUB 11 U@.)

S u0iT g. '

i e

'P R O B. N 0 '

M-f

- - - - NE-210 POST-PROCESSOR (VERS. B) 12/8/81 ********

N0' k I

y r A CH =

l DO YOU UANT TO ENTER PRESSURES AND OTHER STRESSES (YES OR NO)? >YES o,

4 oF 4 ENTER ACTUAL PI,PE 0.D.~AND UALL (INCHES) 0.D.,U? >10.75,1.0 ENTER OPERATING AWD DESIGN PRESSURE (PSIG) P-OP.,P-DES.? >2750,2500 M*

~

3 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)?

>YES

@l PIPE 0.D. =

10.75

/

h, glq WM PIPE UALL =

1.000'..

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 '

4 F~ ^] E b[A'd 1B 14.40 49.440 ---,

.l12.'97 24.720 d 2A c

49.440 QM F

=g 2B 117.39

.c 3A 5.oro4 U4.7'8 =

/

49.440

~

3B

~5. O' 4 H17.18 =

4, 49.440 o

FOR CHECK 3A AtiP'3B YOU HUST ADD THE NAX PRI + SEC STRESS INTENSITY FROM THE NE-210,RUN FOR LOAD LASC 113 AND NUST SilLL BE BEL'0U THE SPECIFIED ALLOUABLE i

i.

m m

.~

'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.

H~

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0 10 Fesqu:ney (Ha) s 1

Ffevre 1 Dampfne valust for selsafe Analysts of Pfotae l

I l Applicable to both Or,E & 55E. Independent of pipe Ofaaeter)

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