ML20052B626
| ML20052B626 | |
| Person / Time | |
|---|---|
| Site: | Seabrook |
| Issue date: | 01/22/1982 |
| From: | Rangananthan B UNITED ENGINEERS & CONSTRUCTORS, INC. |
| To: | |
| Shared Package | |
| ML20052B621 | List: |
| References | |
| 9763-B-04-00-12, 9763-B-4--12, NUDOCS 8205030385 | |
| Download: ML20052B626 (76) | |
Text
{{#Wiki_filter:_. F orm 5604 C ALC. SE T NO. uitted engineers ac.e_..ec ,,s e,. C ALCUL ATION CONTROL SHEET F I N AL 9763-B-04-oo-12 PROJECT TITLE PSNH-SEABROOK UNITS 1 & 2 olSCiPLINE ___PSG VOID SYSTEM REACTOR COOIANT -i 9 SYSTEM SUBJECT PIPE WHIP RESTRAINTS IN THE CONTAINMENT DESIGN CL ASSIFIC ATION STRUCTURAL (h0T SAFETY REIATED) STARTED BY B. RANCANANTHAN DATE I-16-81 AUTHORIZED BY GEORGE CARL DATE 9-24-76 PROBLEM STATEMENT Pipe rupture restraints (PRR's) PW-49-1, PW-49-2, PW-49-4b, PW-49-3a, PW-49-4a and'PW-49-3b for the Reactor Coolant -49 system in the containment are required to control motions and absorb the energy released from a postulated pipe rupture. Analysis must be performed for these PRR's to show that they are capable of withstanding dynamic loads resulting from energy released of the ruptured pipes while maintaining their structural integrity. The blowdown force and applied load directions were provided by the project. (see references (5) DESIGN B ASIS The basis for the designs and analysis of the PRR structures is the ASME III Code, subsection NF and related subarticles addressing linear type of structures. Since this code is not mandatory for the PRR designs, only those sections deemed appropriate were used to generate design guideline criteria presented in section 4.1.2. This criteria simplifies the analysis procedures for the PRR designs. TOTAL NUMBER OF SET COMPUTATION SHEETS 71 FINISHED BY b bMV4hdfu h CHECKED BY di l i z: \\ cwecuta otsien suren cosmizANT rus'n otsten neview l BY kh &f* ,1*y, /Q th *0.4%~ DATE s SL /- fee - P L
- ?'-*u REVISION 1 STARTED DATE BY j
i 8.2050-30385
Form 6603 CALC. SET n!O. mited engineers oc__,,c ,,,c,,. p CALCULATION
SUMMARY
FIN AL 9763-B-04-00-12 a REFERENCE SHEET PROJECT TITLE PSNH-SEABROOK UNITS 1 & 2 oisetPLINE PSG SHEET OF J.O. 9763-006 REACTOR COOLANT -49 SYSTEM SYSTEM ,t COMP. BY CHK,D BY y SUBJECT PIPE WHIP RESTRAINTS IN THE CONTAINMENT ON hf O o,TE oarE DESIGN CL AS$1FIC ATION STRUCTURAL (NOT SAFETY RELATED)
- is.72-l-13-32.
DATE DATE SUMM ARY / CONC LUSIONS See Section 2.0 and 3.0 l (
REFERENCES:
( SPECwiC ArioNS. oR AWINGS, CODES, C ALCUL ATION SE TS, TE XTS, RE PORTS, COMPUTE R D ATA PSAR E TC. ) See Section 5.0 usi .~m* -mee m
TABLE OF CONTENTS (~ SECTION TITLE SIEET 1.'O INTRODUCTION 1 1.1 PRR List 2 2.0
SUMMARY
OF RESULTS 3 2.1 Table of Actual v/s Allowable 4 Stress 2.2 Embedment Loads 10
3.0 CONCLUSION
S 12 4.0 ANALYSIS 13 4.1 Design Criteria 14 4.1.1 Material and Section 15 Properties 4.1.2 Allowable Stresses 16 4.1.3 Load Criteria 19 4.2 DETAILED STRESS ANALYSIS 20 4.2.1 Analysis of PRR W-49-1 21 l 4.2.2 Analysis of PRR W-49-2 29 4.2.3 Analysis of PRR W-49-4b 42 4.2.4 Analysis of PRR W-49-3a 51 4.2.5 Analysis of PRR W-49-4a 37 4.2.6 Analysis of PRR W-49-3b 64
5.0 REFERENCES
73 L- ...__m i
{ 1,0 INTRODUCTION The function of pipe rupture restraints (PRR's) are to protect safety related systems, components and structures from the effect of postulated pipe breaks. This is accomplished by having the PRR's control and limit the motions of the ruptured pipe while allowing thermal expansion and seismic movements to occur when the pipes are in the ir operating modes. The restraints listed in section 1.1 of this report are located in the containment and are welded to the embedments. The PRR's FW-49-1 and PW-49-2 consist of energy absorbing crush pads to absorb the postulated pipe break loads for line RC-49-1-14. U-Bolts are used for PRR PW-49-1 to resist rebound loads. PRR's FW-49-4b,.PW-49-3a and PW-49-4a are designed to resist postulated break of line RC-49-1-14. Also U-bolts are provided for PRR's PW-49-4b and PW-49-4a to resist rebound loads. PRR PW-49-4b also serves as a pipe support. U-bolts are provided for PW-49-3b to resist postulated pipe break loads. The purpose of this report is to show by analysis that these restraints will perform their intended functions without exceeding the stress limits set forth in section 4.1.2. 1 i i \\. ~ -. - - "~'
- g
.n. r 1.1 PRR LIST 4 I SERIAL NO. PRR NO. DRAWING NUMBER t 1 W-49-1 9763-F-104028 Rev. 3 2 W-49-2 9763-F-104028 Rev. 3 3 W-49-4b 9763-F-104028 Rev. 3 4 W-49-3a 9763-F-104029 Rev. 6 5 W-49-4a 9763-F-104029 Rev. 6 6 W-49-3b 9763-F-104030 Rev. 4 j I 1 2-e w r g---
2.0
SUMMARY
OF RESULTS The PRR structures were analyzed to the criteria specified in section 4.1.2. All members of the structures as well as connections were within allowable stress limits. Plastic deformation of members and U-bolts for PRR's PW-49-3a, 4a and 4b is less than 507. of the minimum ultimate uniform strain. Also deformation of crush pad is less than 757. of the crush pad core height. u (. _ _ -.
2.1 TABLE OF ACTUAL V/S ALLOWABLE STRESS PRR PW-49-1 ALLOWABLES STRESS SHEET ACTUAL STRESS STRESS DESCRIPTION TYPE NO STREE3 F(ksi) RATIO f (ksi) (1) G1.0 (2) W (4 v 145 cogpec3sgyg 27 16 11 32 4 (NITH STIFFNER5) $TIFFMER$ Fct Co MREMtN C 27 15 86 2l.09 pg., g gp g Mc is x 45.S WiTH conpcs sswe 27
- 14. G S 32 4 6TIFFNE C 5 STIFFNil$ FoR.
Mcisx45.s LcMPRG55tV6 26 13 44 2219 R '/$ x 2 N 16' B E M D iM 6, 26 s.1 (.;, 32 4 ~ V - Boi-T TE M stc M 2G 18 15 32 4 W El. D S 7$ f'wr to 2.6 15 16 32 4 SToffMil of MC IS '/ FILLET To WEB 80.o9 32 4 e miu ms 1e 1. See section 4.1.2 for allowable stress limits. 2. See section 4.1.2.2for equations to determine stress ratios. 2.. =. -.-. . = _ e
. 9 Nv a ,ea,m+ 9M+ mens g. 2.1 TABLE OF ACTUAL V/S ALLOWABLE STRESS ( k. PRR PW-49-2 ALLOWABLES STRESS SHEET ACTUAL STRESS STRESS DESCRIPTION TYPE NO STRESS F(ksi) RATIO f (ksi) (1) (1.0 (3) (2) W 14 (109 CO M PC.E SSiv E B3 12.I 32 4 - cotumu c# 6EuoiMG 33 29 47 s2 4 w 14 x 283 T eu sion 3
- S'S S24 c,g SEMDtNG Al i1 23 32 4 l-
~ o HEAR i4.qi iq. 4 C R USl-l PAD De,pgc7 cy 32, t 3 69 IN4H-3 5" iNc"- ~ {" W E LLS 5/h FittET S ET. 3g o 32 4 n14.> es G LBx4 UT.B) Ya' riti.s t a:T. wt4s2s.3 3B 24 6 32 4 Aub Be Au v414 SEBB NT. 6) 3/4 Fitts, s c1. Wl4 4 gq 21 5 32 4 Ec AM Wla cS3 (7T. b') 3 " Fiu er ett. nt4 4 4 E M I. R.145 ( IT. A* ) 40 W M*4 3' flu.f7 S cT. W l4 /4 & EMB. 4.147 OT. E ') 40 22 6 37,4 MOTES : 1. See section f. 3 9 for allowable stress limits. 2. See section 4.1.2.2 for equations to determine stress ratios. 3. See sheet no. 31 for joint locations.. _.. _. L. m u-r
2.1 TABLE OF ACTUAL V/S ALLOWABLE STRESS PRR PW-49-4b ~ ALLORABLES STRESS SHEET ACTUAL STRESS STRESS DESCRIPTION TYPE NO STRESS F(ksi) RATIO f (ksi) (1)
- (1.0 (2)
U - SoLT STR AiN 46 c'034 mms 0 2 2 5 iutaci ~ lElongdyn) ( g,,,,,4;c n) J WIAv283 Scuosaq q 25 3 32 4 _ (ft Auct) '[2 STtFF4Et g TENsiou 46 7 31 32 4 PG Wtox263 (CM PEE ssied 47 46 52 4 [NE E) lAIELD A(o 3/g Fiun to '/z snrruet. ~ 6 69 32 4 ~ ~ ~ ~~~~ g ig ;.un., watzs3e eue.t 47 L 6 '4 32 4 3 '6 Fiait To wr6 er / 47 4 53 32 4 Wi4 1. See section 4.1.2 for allowable stress limits. 2. See section 4.1.2.2 for equations to determine stress ratios. -. n.- -.
2.1 TABLE OF ACTUAL V/S ALLOWABLE STRESS PRR PW-49-3a ALLOWABLES STRESS SHEET ACTUAL STRESS STRESS DESCRIPTION TYPE NO STRESS F(ksi) RATIO f (ksi) (1) (1.0 (2) Wid K 43 ST E A tu 54 o ol2 tuents o. o 95 iwto I [Elo m gc.lio b) [g tomg4 trow) C AP E Fa t W L4 x 43 seutig4 55 g1 % S24 titFFMER
- 4. Es t evd (CMP AC SSWE 66 26* &
B2 4 CAP n. WELD (" \\ 55 5/ig Fit.LET To 32 4 W stirr N t cJ 3/6 Fittri To EAsc n. g 16 4 S24 1. See section a_1_9 for allowable stress limits. 2. See section 4.1.2.2 for equations to determine stress ratios., -- r
2.1 TABLE OF ACTtr.L V/S ALLOWABLE STRESS PRR PW-49-4a ALLOWABLES STRESS SHEET ACTUAL STRESS STRESS DESCRIPTION TYPE NO STRESS F(ksi) RATIO f (hsi) (1) 41.0 (2) Wr6er wi2565 STR A IN Gl o.o St # AIM o/ '*"' WEB er wl2 s es d coupeession 6l 20.B2 ~22 29 WCB cf WT7 U-SoLT TE M 5 tou 63 2.1 $ 5 32 4 FLAM6C oF WT 7 x mid SENSiN6 63 34 96 32 4 4.21 32 4 VJtF. ri NTTtIAl T TE M stan $3 wsLDS ~ -- Ultr.4 $8 FtLLET B E T. g.g HEB oF m 2. A ND EM B. Q_ l[ FtLLci Bot. Pc wt2. M.6 32 4 i f\\MD E to b. Il 3 ' fu.tc1 t.e T. /S ~ 3 31 12 4 w T 7 2 E M S. R. 63 1. See section 4.1.2 for allowable stress limits. t 2. See section 4.1.2.2 for equations to determine stress ratios..- e
2.1 TABLE OF ACTUAL V/S ALLOWABLE STRESS ( PRR PW-49-3b ALLOWABLES STRESS SHEET ACTUAL STRESS STRESS DESCRIPTION TYPE NO STRESS F(ksi) RATIO f (ksi) (1) G1.0 (3) (2) W I4 x 61 COMP RESS LV C bb 3o.97 32 4 C A P (1 To N14 56 / B E N D IN (a 67 2 1. l b 52 4 3 ' 5 TIFF. 6 EIT. N64 MI C oMP RE 55)M E 20.% 32 4 /4 gg M Wl4% 253 WEB er Pc wg4 wag 3 comp RE 55tV E 72 l~l. % 32 4 FL AN 4E er Pc.. BEMoguG 63 23 27 32.*4 NtaxtB3 .L[ stirF. To R. Wi45233 T e u $1 0 Al 71 7 3l 32 4 U-BoL7 STEALM 70 e.co39 sum 225im NEL DS 3/g FILLET BET. CAPQ. S7 32 4 & W14 % (et 8f FILLET B CT. N 144(,] / 4] $2 4 32 4 4 ViFitttiWid S 2 65_h..... W-S cl. 4 GS 29 3G 32 4 wiA r,. Pt.iuta };~ {f5LCT 6 E T-._ g g g c p p c. W14 4'. F L Au4t 66 22 4'l II'4 oF Wi4 " D W B' E y" 4 Q 5'ittti BE T. ~ wi452ss e cas.R. 66 t B- (.7. 32 4 af[ FiLLtT FeR 'r$itstr. 7 'l 6.SCL 32 4 ~ 1. See section 4.1.2 for allowable stress limits. (,') 2. See section 4.1.2.2 for equations to determine stress ratios.,- .~- -. _ n: L. : L ' iN - :'. * ' ".:
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i GENERAL COMPUTATION SHEET CALC SET NO REV COMP By CHX'D BY I (DISCIPUNE) g PREUM Q
- N" FINAL 9/43-8-0 4
- 2 DATE DATE
/~ "^ t - i l - $ 2. e.n gs COMPANY PSNH - Seabrook Station UNIT /S 1&2 j SUBJECT PRR DESIGN AND ANALYSIS J 9763.006 EMBEDMENT LOADS SYSTEM: R6A4 tor. co ct A MT 3 P LINE: R c - 4 9 - l - 14 J ) Vi N
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0~ N HORIZ H = ..s y es '- N ,j- . p y LOCATION: coNTAIMMENT 1 [*7 s, 2 S 3[, 2 SIGN CONVENTION: . V ;.2. c 2 /. Y 1 FORCES: POSITIVE AS SHOWN 3*. \\' VERT. MOMENTS: FOLIIM RIGHT HAND RULE 8 V = 1 id '\\ P .',WgN v, 2-3 .- j LOADS ABOUT CENTERLINE OF EMBEDMENT PIATE EMBEDMENT PIATE PRR NO. KIPS IN - KIPS MT M1 M NO. H/V DWG. NO. P Y1 Y2 2 P W 1 l46 s/ LO4c 26 339 82. isS6 i I i I I PW 2 147 H 32o l 296 l - - 8745! i i l l PW 49 - 2 las v 90 - 320 G308 ,I i PW-49-4b 153 H 1 354 8 I PN Ba l49 v to4o 2.9 -ses,2a9 l Q 5s.4 PW. 49 4a. 152 v u 154 PW 3b iso H 104o30 - 564
.. - J. ..L - =- ^'
3.0 CONCLUSION
S t The PRR'S listed kn section 1.1 will perform their intended functions of protecting safety related systems, components and structures from I the effects of postulated pipe breaks. The PRR designs are adequate to i j withstand the applied loads given in section 4.1.3 and meet the stress limits specified in section 4.1.2. i l 2 i l' 1-k. i I I f 4 3 q. i i a i .. ~.......- = - _ q g p.,-f mm,. M-W"'Ps.- P* ~
e U t 9 4.0 ANALYSIS s us.__ _.. _ _ _ _. _ _.
( 4.1 DESIGN CRITERIA Pipe rupture restraints must be capable of withstanding dynamic loads resulting from pipe rupture and restrain the motion of the ruptured pipe. In applying plastic deformation design, maximum strain in the members is limited to 507. of the minimum ultimate uniform strain. Maximum deformation of crush pads must be limited to 757. of the crush pad core height. For limits of allowable stress, see section 4.1.2. i I
- 6
[ 4,1,1 MATERIAL AND SECTION PROPERTIES I i 4.1.1.1 MATERIAL h Tabulated be' low are the materials and properries.used for the l I PRR designs taken at 100 F ambient temperature inside the l ; containment. ~ i HECHANICAL PROPERTIES (KSI,) HATERIAL Su Sy E i l i 3 AS E A - 36 58 36 27.9x10 I' I 6 i i. i L 4 l' l \\ 4.1.1.2 SECTION PROPERTIES: Standard sections are used for the PRR structure. See reference 1 for section properties of the standard sections. e e 15-m. s.,e.s., ,.s, m-< w.
- w
-m.. ~ m.-
^ 4.1. 2 Allow-bt, Strosses for Ele:stic Restreint2 All symbols used in the following table are according to ASME III e article XVIII-1000 (page #331) except symbols with hyphen (e.g. F') are used to' define allowable stresses for faulted condition. / 4.1 2.1 TABLE OF ALIMABLE STRESSES ITEM STRESS TYPE ALLCMABII STRESS COMMENIS i e - Tension F't = 0.90 Sy STRUCTURAL STEEL - Shear F'y = 0.55 sy - Bending T'b = 0.90 Sy - Compression T'a = 0.66 Fa See Section 4.1.2.2 for Fa FULL PENr.rKATION ALL Same As Base Metal - Compression normaf to weld axis PARTIAL - Tension & PENETRATION >Same As Base Metal Compression parallel to weld (. axis. - Shear See note (1) - Tension normal to weld axis. s - Tension & Same As Base Metal Compression to weld axis. - Shear F'w = 1.5 f w 4' I I i Note: (1) fw = 0.3 x normal tensile strength of weld material. 1 +,me..-.- -.+= -+-.
.-.m-- 4.1. 2. 2 COMBINED STRESSES Axial compression and Bending I /{ For members subjected to both axial compression and bending, stresses shall be proportioned to satisfy the following equation: f is b
- FT F.' = 0.66 F, i
Where F. = 1
- U 'i
for Kt/r > 25 s 2c,s, e and C, - f' # m;; Kt/r - see note (1) also F.* = 0.90S for Kf/r 4 25 p i Axial Tension and Bending ( Members subjected to both axial tension and bending stresses shall'be proportioned to satisfy the following equation: ft fb A O F}
- Fb Note: (1) for Ce> Kl/r,see ASME section XVII - 2213.2 to determine Fa i
e
- 1 1
4.1. 2. 3 ALLOWABLE STRESS VAttQ (. i Allowable stress values are calculated with reference to section 4.2.1. Equations used to calculate these values are according to section 4.2.2'. Following are the values of allowable stresses l l for ASTM A-36 steel and E70 XX electrode for weld. i I STRUCTURAL STEEL i Tension F't = 0.90 Sy = 32.4 kai r Shear F8v = 0.55 Sy = 19.8 ksi Bending F'b = 0.90 Sy = 32.4 ksi Compression T's = 0.66 Fa See section 4.2.2.2 for determination i of Fa where Sy = 36 kai I I WEIb s F'w = 1.5 fw = 1.5 x (0.3 x 72.0 ksi) = 32.4 ksi F e I i ~~ ~ ^" ~ ~' ~ ~ ~ ~ y
.m = { 4.1.3 LOAD CRITERIA From NRC postulates break criteria, only one break at a time is postulated to occur. 'Ihe PRR's shown in drawing no. 9763-F-104028,104029 and 104030 are designed to resist the pipe break loads given in reference 5 PRR's W-49-1 and W-49-2 are designed to absorb energy released due ;o a postulated pipe break. U-bolts used for PRR W-49-1 are designed for 207. of blowdown force (F = 277 kips). b PRR's W-49-3a, -4a and -4b are designed to withstand postulated pipe break load of 454 kips, 356 kips and 354 kips respectively. PRR W 3b is designed for 554 kips load (+ y direction) and 354 kips load (- y direction). 9 I,
pg g pg ,,w. mee e ( 4.2 DETAILED STRESS ANALYSIS ,r e I ( i 20-y..v__
~~ =-Mwe6m m e ~ p 4.2.1 ANALYSIS OF PRR PW-49-1 i l - -
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- oiv63. cog ATE DATE SUBJECT 10 4 C 2.S f W. 49-1 r-I N E.
RC.-4Gl-I-IM ' DATA 6 L CVJ 30WM f OR C L. f6 s 2 'I T KIPS L 4 LC? to4 88 t, Lo vJ towW N 6 5* W LATA PO t47 b0 COLb G, A P 'N HoALIoWTAL 'D ia t e'T i c N l '/4 ' 4 COLD LAPS " N6 li o7 G AP en koai a cw t Aw t
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..m-. ro== soo7 ary 7m GENERAL COMPUTATION CHEET CALC. SET NO REY coup sv CHr0 ev (DISCIPLINE) PRELIM g- {' 6 - ( 4. g p -l 1 DATE FWAL DATL 2 9 inc.4-b (3 PSNH-SEABROOK ST.ATNDN voo NAME OF i, o. C UNIT /S COMPANY SHEET kO OF 3$lgt/CTURAL CA' ~ ~~E WHIP RESTRAINT oArt oATE
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e -e al -ew - w-- \\ 4.2.3 ANALYSIS OF PRR PW-49 4b (. l L.:
sonu exo7 acy 7n, CENERAL COMPUTATION SHEET CALC SET NO TEv COMP By CHWD BY (DtSCIPLINE) PREuu gM Mg r:NAL .$.o4-40 / s wome n DATE DATE
- 02. I Sl i&.O.%1 f'^
couedvPSNH-SEABROOK STATION "^" UNIT /S swEEr 43 or 61HUU s vxAL CALCS-PieE WHIP RESTRA!NT
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ATE DATE SUBJECT 1o4 o?. 8 P a*_ Qo P w 4 k lin e. Rc 4 9. i-i 4" s t V. 4;: L 79 ., v. 9 To i of RincTcR / .1 ( //\\ // s // s '(,. \\ ' - Fw A 1, a I -. -, $ l '- S j Lo c AT to t4 PLAg I a r e,c4ca. 2.77 Kf6 d e W N W A R I). 6w ys ocwa (oAct = -7/'6" 'I - co's GAP s y. %r cnP e - la " 1 ~/ C 4-CCLD C AF e L-bc7
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FOIHS SOO7 Rhe..*!*9 GENERAL COMPUTATION SHEET CALC SET NO aty coup :Y CHWD BY h=in:ted engineers U.Nf unsemunci O = " " final - B - O t} - 0 0 - l 2. part pays n.q. si. (7 CoEEPSMH-SEABROOK STATION unms setor 44 or Jo 9
- o4 syf@CTURAL CALC 3
.niPI V/H!P RCSTRAINT P R R* P W - 49. 4 % L w e,- R c. 49 - l - 14" l__l04 Om y _ _ 4. _. __-. __. .... 3 I , s - L-_ D '._.u-__- e ca o o g
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- O d*O O "I2" DATE DATE 12 3 d*/
9 0. t}. hl. NAME Or VOID bd COMPANY PSNH-SEABROOK STATION UNIT /S SHEET 4,. or STRUCIURAL CALCS-PIPE WHIP RESTRAINT DATE DATE ,,,;,,,g SUBJECT tra g o 23 rw.49-4 k L m e. Rc-4 9 - l- % U-re.c 7 A u n t, v cis = :- 7/lk Oc L. .% A P A" U - A.c L. r '/4 " ' 07 G, e P AT U-h. o r T s ft.L 6 v) 'L o W ra Lc A.D . MF k.1PS L f % T16 ef U-P; e tr oI cf I f " I%V Got W 41 - : 30 seJ A
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FOpis 50C7 Riv 7/79 GENERAL COMPUTATION SHEET CALC. SET NO ret COMPBy CH:rD BV (Ol!CIPLINE) PRELIM ff,,, R gg FINAL - h
- Cd - D O - 8 7-DATE DATE Q. 6 - t? -
l d].Q.$ f, NAME OF VolD COMPANY PENM RFABRnny gTATinM UNIT /S i SHEET d 7 OF ATE ATE gJgCTURAL CALCS-PIPE WHIP RESTRAINT
- o 976c c-o c, Ic 4. o *AS p yg. A. 9. f Io liNE R C.
4 o - 1 84 VJ C r:., eF PC w e a s 2.Sy lo s, -') eo N 5. e., cArsr'LLVfR L o A 2) -fbt a 343f[$?s*as.38) 4-% kGl C.
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1 GENERAL COMPUTATION SHEET CALC. SET NO ret' COMP BY CHCPD BY (DISCIPLINE) NEuM th R gg g FINAL O 4
- O O
- 17-DATE DATE
(,.18 3 ) If 7 81. NA EO PSNH-SEABROOK STATION co p UNWS ISO swcti 46 or ^" ^" sue;EgTRUCTURAL CALCS-PIPE WHlP RESTRAINT;o %. c, e a 104 C?S Pw-444L t m t. Rc. 4et-i-li j 4-Il6 s.4 % 9 _,i- . p *-I1__f 4-1 l I i l I 20 i i i 8 i i l 3 r _ _ _ _ _ __ _ a _ _ _ _ _ _ _ _ _ _ _ - _ _ _ _. _ _. l l l I l i f.2y l 4 3}[g r 3 2Y l l k I l l 1 1 i I I l'f fs p .7 l I 6.M li.?J l l 7 I l I i I I I i i _.______s_. l l l i l I l I i Il $16 t/c. q (to LT I i S L O T T E_D HOLE. FoR U - ra c tT, ,e..,%... ..,-.. m..~ .._----4. - -. ~_ w ...e.,..-..---
..-.... = - - - - -. FO8He 5007 REY 7/79 CENERAL COMPUTATION CHEET CALC. SET NO uv coup ey CHX*D BY (DISCIPLINE) PREUM g.( g t riNAL -B.04-oc-JL carg o,yg m.9 9' NAME OF PSNH-SEABROOK STATION /> 2 / COMPANY UNIT /S SHEETd-k OF STRUCTURAL CALCS-PIPE WHIP RESTRAINT oATE o*Tc
- o em ces SUBJECT l%4 C 2.S f' W. 4 9 - A (1 b'N L R C.- /A-I- I k
p i - <' ff Qve -,)? <, re 3- _. _ m. _ _,,,_ _ _ __#f y _. _j i l, i 4_ i ( m_ __l _i. c._ _3 i 8 i 8 L' F. i i g ~ ...a - T r - - - - ] - - y-' ' ' e ll i il l ..- s i .t .f_ [ ~'s 6 f * * *, i J b. '\\ l' ' - C" r i i .y, p.. .1
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- - I 32S 14 A3 -
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- s. I in t 18 t, a e w A g cc 5Tr.r%G 2ra T*L A2r r>
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-e . ~. - - - - _.. -. -. FOpu 5007 Rtv 7/79 GENERAL COMPUTATION CHEET CALC. SET NO. REV CO%P By CHK'D BY (D!SCIPLINE) PREUM g pQ gg FWAL - 3. O g$ - Oc =l *2 DATE DATE G. 9 61
- 14. *t. $ f.
~ NAME OF volD COMPANYPSNH-gramonny qTATinN UNIT /S ' '
- SHEET TO OF STRUCTURAL CALCS-PtPE WHIP RESTRAINP DATE DATE
,o qg yj SUBJECT 10 4 C 2.9 P VJ 4 6 l IPJ L RC - 4 9 - l - 14' l TT Y C9 s 1-3S L t;r.s T H A ra i 4 *,5 l 18 %ENCE A L M &LR- 'I7 l A FO R TeREAD To SE C M G EN. O 16
- ) 16 IM QO.
of T* Q E A )G PER I N Cu a 8 c 73 3 ( t.TS - O 9T4
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C-cit 'T H R E A275:3 IS o '3E. q o A T EL, T% C A.!- LLtdTH CALC t/ A ATIO N (
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4.1.4 ANALYSIS OF PRR PW-49-3a ,r I l l \\ .g.. -. w
_.2 .m.._s.~;..___--_w-__u---------.----u.ss.s. FOpes soo7 ety 7/?g CENERAL COMPUTATION SHEET CALC. SET NO-REV COMP BY CHK'D CY PRE U M 6C ggp (DISCIPLINE) g FINAL
- 8 a t* 4 -O b -f 1 DATE DATE
.3 27 8J g p, g4, pg, -y NAME OF YOID PSNH-SEABROOK STATION UN:T/S I 8, k COMPANY SHEET D2 or dTRUCTURAL CALCS-PIPE WHIP RESTRAINT DATE DATE 20. 373s.,,g SUBJECT 104 029 PW-4 9-3 R L iu P_ R.c 4 9 1 - W = 277 k. N 31 76 6 6 Low town F e nc e_ f sb C ot.3 CAP i s 'D # R C ct i o N y 1%T C= A P o e 1'/4 'b se a cT i ou h cett G, A e = l'o T 4 ge 3 / i t, fG.6x12x 19 % CRVSH PA3 < e n t. Gi A v c, E. 12. n ik.- l 39.3 5 R 7 rACToR CENTRE / + -p. o' 2; Q 9,
- $ f
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tS 84 C PPO s f*E D et C c-r e e, u
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FOpas 5007 DE7 7 fit GENERAL COMPUTATION SHEET CALC. SET NO. REV COMP BY CHTD BY (DtSCIPLINE) PRELIM g., p
- -~
rm4L -S c4 -ce -l 2. oarE oarE e er t o. l4. Bl. NAME OF VOID COMPANY PSNH-SEABROOK STATION UNIT /S 1 SHEET 63 OF STPUCTURAL CALCS-PIPE WHIP RESTRAINT Jo % c-3 co G SUBJECT to e c 2q p w, 4 9 3 pp. R c. 49-n-14" l ,/ 3/s ' s y sf r EN LR ry P ic A L. f l' %[,., o i, . _ _.. _.. [ W 16177 f 'i ll ..M' l"I rl 'Y F A tr. )f,- [e r rser y (3 : _5 } -~V' O-r--q T7? w 4 v ti f%i, '$, .r: d.. p, i ' x q, i t, 4 re \\,hy - f g 1o5w25x55 Pa c T u ccLo ..r. -.,Vis 1% sg i l ( W l0 % Il 2. lI A /p; l 's - cyr 3 'Y F > - j ') , u,l gy kyg l5 g.g p p s i i ,-- A W; i - b y M N N )- g - A j;" l ' ./ / / ? / __G -.., ,p j' ,9 Ne 'n e,N ,csfe N Y. l ? /s 's k__ 3[_ lf e([' } l I a l2.
- 2_..,
9a a VIEW A-A
fores 5007 REU 7/79 GENERAL COMPUTATION @HEET CALC SET NO REV COMP By CH%'D BV (DISCIPLINE) PREUM g_Q ,g } FINAL -3 44*OC */2 DATE W.a mu, CO=$ PSNH-SEABROOK STATION "^ uNires ', 2 r SHEET M OF sgRyCTURAL CALCS-PIPE WHIP RESTRAINT DATE DATE
- o n c,3. m g 10 4 D 'L4 F W
.4 01 J, a litJ E P_C - 4 % t-44 }N i 4 x 43, w i g
- 4%
16Lova pawg r o u c. t s 2.7 7 v As 2 C, c-o m N o, G, a e s
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4, 2 s - ( 4 ' '-t h' + w ) s u a. > s.~ 4 (L { A C. T ' F F r J f O C i 6 x 29 x ed / 18 S45* s
- 2
= 12 247 5
- /
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e.2 9 s bf w ew.131 im*
wowa m is F ( e r,,o n e 1 x 2 0 7' 4 14 7 i b ( *.4 % -' 19 ) C.'T h') x.1: 13 06 M41s h6 ' I *EN C *W x L : a t as n r i f r F g g ytg mm s ei t s.
- t. e i n e r,t.
Axta s ( 17. 9.1 + n 73 + I S o f. + 2 2 tN/a. 42*% sq N. t i.74 4" f E g",.T svC L E N s,$7 H I6 T4 11 J va u,,, 2 s t 4 m w i u t s s. (3> m u) Amu mA W ( Q. O f PC W t4m!?3 'h 'P J t f" A x Aa r.A Sterff%fvs112L fn A p. s(14 6 2 9 8. E *). E % 3a x t e., or wio2c3 x.9. mai aac wee,a u.e s 32. u mo : s o x < 2 3 s s s >o (12 A h + 1% %o 54-43t S S %NL S43 % 'l ~ A V E R A G. E A m. s e s 4 CfPLcT:vt LLnS rn s n ~
GENERAL COMPUTATION SHEET CALC. SET NO. REY COMP BY CH:fD BY PREUM 6a pq (DISCIPLINE) M ~ O -~ RNAL -$. 04. o p.g g, ~8' MW NAME OF coupaNvPSNH-SEABROOK STATION I -. unit /s 'O SHEET Q-8 or ATE DATE J 9 V ' *>- c' o G supl8UCTURAL cat ^c r - WHIP RESTRAINT rm 404 03o Pee No. PW. 49-a L !. ua t Rc -4 % i-14 = # ro. e. s u 4 w. 7 or n e. 3 er u c c r ie. n a, +c. +63 n c, fa s. v s-
- o. 8 8 e s,,
o. o.9s" = G.9 x C k
- o. \\% f 5,..
s. 8 s x 16 ' " 4 P >- c. 91> e 2 = 4 2. 9 7 < E E-Og Px tt o, I M.t = E -s* g 2 3g x,3 gi. 4 g f_ 3,
- l. I 93 P[f_,
o, o s L Y " be.. L,*L,*Lz-l
- L 2
- 1. I 9.3 f P: 15, G T i F F (V C G C.
s. , M 308 X # 29* W
- c. I s
f.- t 195 k,, DYIJ f\\ f% IC e A ta [A C_"r c M. COLL G. A e A7 v. st. e c. 7 O NOT G f+ e AT U-fJ e5 LT O "I' H E Fe fri e t (h o v C fY1 E N T 0 = 1x k c 7 Y2-K: G t # f p tJ L s s o f G oe pea 7 'b 4. F I 4 1+ frb ~ ea noy 4 6e f6 R Lo w Down FoscL. = 3
- 4_
,p, 14 I4
- 2. x 24 3ap y ro p o
- 2. D b
R E C r R A s tJr l.o n :1> 2.7 7 x 2. = SS-4 6? NfGE s tJ kJ # 4 se G/ 554 87 $ .3# 95-R S/ = f G h b' 12 SG 6 HCR7 COL.. 2 C L E rJ 3r l d.NE G5 RATIO x Oly Nikx6/ : 2. G S
- ' Lo S ALLCwA6LL S TRLM = M. ti kS/
>30 9$ STREGG reJ Act c"T n /R c o rn e'o N E NTS ARE LE CS C't- - _. ~. -. - - -. -. - -.
= roeu soot am Sns GENERAL COMPUTATION SHEET CALC. SET NO REV COMP. QY CHK D B7 (DISCIPLINE) PRELIM g $Q g FINAL
- b
- Od
- O O ~I 1-DATE DATE l2. l. 8 l 11 Il* U.
7 CO% PSNH-SEABROOK STATION uNms I% SHEET 67 OF sg@CTURAL CALC 9-ploE WHIP RERTRAINT JO 9 M.cO6 10l O30 fh No. Pw 3 6 lira Re e i-id C u t_ e s<, P LA T r. { SCE C.ktTc w p,t tow) k122*x9) 4.)S' 7
- 2 /g A9 K st 5 pim PL 4 7 c-
'W4 LeAnins. w Tt w sery P L A i c,, ( A P P e.o na ry1 A 7 c t T c) F lx E. L oNE CDGL. 5 s 8*'5 P LY S uf f e stT E D 2 E9 6 66 % f EL E C. 4 Tw R E. F. 8 o*t.rev tra 5 F o st 6TRE s s Q s Te. A su ey RoAAw.- Cast 7
- (it. 2 9 - a, x o 6 4 ; - e. 5) I 2
,6.o9 eu b s (9.9 9 5 - c.375) /z. 4 si iu al4 : 4..es/4. sis i tss, p, 0 %S @a : C.45 I" 3" mi4 tS H irn
- T H l e. v_N CG G =
If P IP G. IS IN P L e c t. Shim :-
- i' O T A L.
E F f C CTiV E THICu. Ness CE P L A 7 E. m :L I4 2 I MAv. 6 T R C C f,, a C.9 9 3 x 4.M < 4 81 2 : T4 18 tt $) 4 32 6 8< $ l c < VJ E LLING w s tt a ty. w i.. <. r, t e = io". i s. t. a ; ' l WrLL LENc TH 9.996 o.t7s = 9 62 ~ ' 12,.f o - - - - - w 14 x G I 13.9's.txo 44g e 9 $ p,,,,,, 49 %2 +c5 .f ~ R. 1"A 10 x l'A 9 "i s " P. I. 7 2. ' A 2. a l l f . t 0.S " A 4. $ ~ X 4.L " 344 N U,1 !/4V FeR 3M F iL L C.T w t.LD t o T o 7 Q = 32. 4 1 - S
- f C AP A c. i T Y 2. L *, K L t s
n .. o = e. P 7 W O M d :. 32 ') vGI WCLD 6*aE05
- /6 4
(. i W 14 A Cs! -J., l'14 <J = i t 8 9, il 0GW b(a 9 *W, ( 0.375 WELD is A*pE q u A T E. L. Ii " d W #4 = 215 ) 4- -- --- -- W I4 t G I l 10 - 54 N - 1_ _. -1[ S T J F F *a f it M Low / W G k. 3 F3. C T W i 4 = C, i L \\N 13 3 *LS 3 ( GEE. Sir ET cM e,ovcj 3lg A L.L. G UU M D Wr s D h. *
- st. e, '3 7 5 ) 4 (#329.zw 6 4 c )],
g4, 43' T' e> r a c wo u ::2 2.[ 7 99; 4 s ur r i cir uT w e e r, ^ c. c., m % u e_ s <;ti w vHe Amr. STRESS s 6 e 4 0_ x 39 : n. 9 g. n si 64 45 . _ - ~ _ W
e<ws w ory 7m GENERAL COMPUTATION SHEU Cf.LC SET NO Rtv Cou) er CMX D BY (DISCIPLfNE) Patur gQ g( g FIPe4 L
- 6
- C4-CO
- fd=
DATE DATE / 2./ ft I it - f t. at. NAME W PSNH-SEABROOK STATION CCMPANY UNIT /S _, 2-STRUCTURAL CALCS-PlPE WHIP RESTRAINT 5"'"[4 o,1,
- o 2,. o o G SUBJECT e w. 49 7 4 Lio s e c-49 I is' to a e ?,o P Fst rse 3/4 "
STif f ENC A 6CTwtcy W t4% Gi (, PC, W 14 s 2 8 d. - ~. -. =. - -. -. ~~- Y - .e f S . yas O TEE c6 iN N l 41C fe I *: .5 0 N 6 CI I%'89 id
- 5. R d' A cf f L A pJ (A [ C,
'.9 Gl 'I A c. Ce 46 % 2. t F 0 64 c. E peJ G L h 4 G F. m LCMA l*L T 9 i.'., 9 %. Cl t 4oc t EMN&E e C' W t Li v (71 RI G H T oggg 3/[ G T if C L PJ E C., M 4 CgC. Le n D Deur : rLy C Le w G into 3/4 S t +F a ea c e_ [9 2) 2 0 T-6 K fa l
- 1" w l' C.C W
57'IILQLR :. 4 00 e. 1: it.1 4s'e a s* lit : o asz A s iths t ows 9 ss ;fI/aV2 I " '"/, 6's e 2.> x.r i v
- it ( C. q t i. 2.. o v ) l e.2.i >
- ic,.9 c
- 2. s-r.2 32 4 w.,,
b/g N L L 'O of c v 4 f f N L o<.- ( hcTunt W E L 'i, Lf N Gm e c.x 5 o c. If. ii. i.29
- 4 80 era C C rJS C,,f,= t rJ G O N Ly 9 999 *l-29
- 1 *2 O *+ r P2 64 S f*J
- s. i. 38 w
re rec w t u a, Lc,47H e2Eos<4 a 4 00 / r e. "6 6 T 'IIS MLt 2-9.164 KS) a 3, 2 4 o.K S T R E t.d s 3 rd c.i n e:Lt A R E f,,--,,P c ._ - --.$ g...,,.A,9. 33 W t & x 2.3. 3, ( o rn v W p 4 x 2. - _-,.,n.-- ,,m,.f.e e e..or u, wt,-.n n g, LerL c- ( 3 /4 " ,T t r r ( rJ C R 7 A e N c reu 7 T r.'n t e_ s A os c 400[12.12. l'8. 9 0 f Cal G T' ed I c,C, s WL L 0 (IG.it - i. 2 9 -
- 2. M. '3 ) A LCt4tu er 1/3 WCLp :
s FF 22 ( '2 - W L t%, (beh t, it t..G } f f I[ CT IVE Apr 4 p. '. c, 7, c. 3 *+ v w gy. 2 g 14 6 G ug w a y 2.s 2 s-nnn 2x0 wt x 0 4 TOTAL g:, g g A /4.G G + 7.C 3 : 1T. 49 Sq iM 4c0 / lY C 5 M is' T e 32 4 o. t. N L L'.D r., T xt ri,
eone soc 7 esv m, GENERAL COMPUTATION SHEU CALC SET NO ets COMPSY CHU D BY (DISCIPLIN D M O s cuema we n FINAL -$
- Od "OO "f b Daig DATE l 7, /. fl 97 II h3 con 47v pRNH_RFARROOK STATION uNms ' ?
void wcn 69 or gIggCTURAL CALCS-PIPE WHIP RESTRAINT o^ ^"
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rea. e te g w. 4 9. v., 6 Lio t Rc-49 i 'V M
- 664 EM 1, 3 p --
"* r i VJ ) 6. t 2.31 t TOTAL Lo A 2) s va t e d 9 9 o V'b C D 1 A ~4 7 x 0.70 T % 0 5 + M 16. i t A 0 3 0 4 v. D. ?sW s
- 2. '1 7 $
d et su TC4/E9.W = 8 3. G '2. Kst c E2 4 C.K r.:,
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7 08888 S007 #f1 7/79 GENEZAL COMPUTATION CHEET CALC. SET NO REY COna? 8v CMX D BV (DISCIPLINEI PREU 2 p, R gQ P ifvA L = $ = 4 4
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DATE DATE I21 tl s1 IL h. "^"' coup,[y PSNH-SEABROOK STATION UNIT /$ 2-saccr 7 e or STRUCTURAL CALCS-PIPE WHIP RESTRAINT oart oatt
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, n ~3# SUBJECT ICA o to P v4 4 9 - L b L t PJ E RC-M - I- 'I U. G., e L -- A eQ A _, y.",,,1;,G NATLktAL_
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% IO Eb! I @ & 4c7 c;. e. P APJ3>
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= S e. 1 7 2. A < I d s ,D Y H o rq i C Le At f A c reR, OL.F 2. AG rot G A P n. o V(Ctr4idi Lr; A 3, Re
- 2. X ?.i 't
'I S" 4 6 8FS t C. I. A t J 1t, ~L l A -a f '). 6 o c,.* . t '/ a_" 3 43: I %T ",q s o tir T Gi c.".~, 'O V* Fi,0 L. T " 04 (4x l. T'G *+ ) 7% ~6 8 G' s G - % t L *f )O V r
- L,o 3 t L t,,,3,>
Re 4 % t M *f x. We e 152. 4 ne. t c*_4 Ec r_ U - P.o t. e fo re. E v-ra c,nTieva ( REF U - 52 o t r 'D E TA L L P, i 'J "D wA*g L CtJ 4 T H e0 U-8to L T-oF "D ' A IG eu = 4 t i,
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E rn ( % +hq+dP ) i dP (kip b o-
- HO7 G. A P = C>
n he E LASTic r_ Lo ts a T e ot ) s R,,. w & a c, 23 r ( o 4 o o si 4 b ) - 3, s s. 4 ( o -es if, + J e ) e ,o.os-io fe..t-d
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g o. C G T [ d.o - a 2 4 m e0 C d dc+G, 3 94,4
- ed 3
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- 2.. o S GQ
'+J. sA7 'T E Nc, i c,J A R C. A = o 4 R AT to CF 5MANK NREA To 'T H P.E. A'D 486A
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a.o g
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0. S T R C c,,.C otu T FF C.R.b 8s b 85 x & T RC=s~ tM :s M g 5 /d E G Lr eT # r4 LT R C "".~.C. cc:' ev C C-MTR A T 'Ord. 0 - T f = *,, o : 42.C MS/
GCNE A AL COM'f *UT ATION SitL LT catc ut No ) '~
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ne g -~~' ~ ,.w,, rmuw ,u _ e.. c4., o. n. c,.,
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o*rt o*Te STRUCTURAL CALCS-PIPE WHIP RES1RAINT a.12 C. 4 /! ! 1-a.,,- suanci Ae. e.*.
- - sa to c o s c.
e s t. 3 -,,. n .i.t..our u ; rc> .s u r<, o s_ r
- Low,
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r is. - nt CHt .v Leap rs e. L L ci er
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., s;4 / o t e.st =. i S.,6 9 g $,. i 3 e /;,.a. g o u. ,y C A NTIL F yl P L F l i c.u. e, 4*, t' A H C s e i c. a... a w w764 s G.TG.o.s s G.:e S seJ
- 7. 84 TS i 4. %2M e 'T. o s #ed a
lifttTIVs temp 4y surr snTT.D ".' r A ta i &.) $ '41 W 'D T H s 'YO T A L. LeeA m f a % C. "J W t. In ta. ') I' l.o a as a t r. s. i t t, e<. y s em e s. c se, c A m, kP by cam vi c.t vs - 3 ( i. k ) a 2.. f a,", I' 7,,,c..n v3. f/,z. 4 c, J. .u* D r.FLE c.Tio u o F' c A eli e L a u.. s b f. 7. A f a h. 2 $ 'en a.n * "I > e T S e s. 3.o Tyss. ti 01 84 ,, t F L f e t IO N of f,. T.. 85 t A rt i &C 1, a II 45; C Gt V A v eN C. D C T (f C'T 80 eJa (e. k ) *A. S tg '4 *$ A tt 1.2 5,
- ib.53
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- A *td4 10 3. &G Ir taJ d h tO T.
mpm(Nr s STAE54 s l e'!',.153 10 ff s 2 3,. 2. f e '6 s. 4 o. st.. .'ir
- C. 2
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- 18 3.. ** " % T [G 1$
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- n. v ',. 4 e s
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- s. s a c 32 4__
e-W Li.2p et A C L g, a 4 l N TE.- A Pe t A W 6, 08 1,, &/4 MIMim0M sing Fl u tT W et.0* A e dt'O. Fe t 5 ste t. Mt*J 64T.I. 5 640* - -e _ W C (b OF f'C. w) I t, v 2 ? L og DLTAIL DWG,
- # ' ^ -- ^ ^
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16 1 [ ? e. .s.5.3, k si
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roen w ntovns GENERAL COMPUTATION SHEET CALC SET No aEv coupav cHTD BY PRELIO ($, @ %k (DISCIPLINE) g
- N'"
FINAL " 6 * #d
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r-coup 8vPSNH-SEABROOK STATION unius ' 1 "^"' SHEET N OF STRUCTURAL CALCS-P!PE WHIP RESTRAINT
- o 4 76 3. oc a SUBJECT me, e> zo e n. 49. s k L i,s c ac-a m i is
..-4 y T 58 E. E Me
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M* W 'Y Fe g, ( p cf 'lg " W [ g3 1 Id4 A R S. A of 5 /g" W f. L L ? D Y *Oe4 Y Ex 4 "' =
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t ? e ( C C, t 3,5 4 19 ^t5 11 *l " Ll
- E7 4
0*' (- - my eop,+ e - %.se p g gw -+wmw -we*me-
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r {'
5.0 REFERENCES
1. AISC Specifications for Steel Construction Manual. 2. U.S. Nuclear Regulatory Commission - Standard Review Plan, Section 3.6.2. 3. Formulas for Stress and Strain by R.J. Roark. 4. Memorandum # MM-7457 A (Date: 7-29-81). 5. Memorandum # MM-7158 A (Date: 5-19-81). 6. ASME Boiler and Pressure Vessel Code III. ( J, _, -r . _ _ -. _}}