enclosure 4 reactor vessel bottom mounted … · calc no. m-11 165-048-1 revision 00 project no....

ENCLOSURE 4

REACTOR VESSEL BOTTOM MOUNTED INSTRUMENT TUBE ANALYSIS

(50 pages follow)

Calc No. M-1 1165-048-1Revision 00

SrgenojS Lzrady' X*Project No. 11165-048Page 1 of 10

ISSUE SUMMARYDESIGN CONTROL SUMMARY

CLIENT: Nuclear Management Companv UNIT NO.: 2 Page No.:. 1

PROJECT NAME: Point BeachPROJECT NO.: .11165-048 0 NUCLEAR SAFETY- RELATED

CALC. NO.: M-1 1165-04B-1 0 NOT NUCLEAR SAFETY-RELATED

TITLE: Evaluation of Bottom-Mounted Instrument (BMI) Conduits for Postulated ReactorVessel Displacement

EQUIPMENTNO.: N/A

IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDNOIDED & REVIEW METHODFirst Issue

INPUTS/ ASSUMPTIONS

0 VERIFIEDo UNVERIFIED

REVIEW METHOD: Detailed Review REV. 00STATUS: Approveg { DATE FOR REV.: 05-19-2005PREPARER G. Z. Tokarski DATE: -s -U LD

REVIEWER* J.N.Tolia Ji4'Ec ok\° DATE: s,/qtof

APPROVER' G. Z. Tokarski DATE: Lao s-°

IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDNOIDED & REVIEW METHOD

INPUTS/ ASSUMPTIONSo VERIFIED

o UNVERIFIEDREVIEW METHOD: REV.

STATUS: ' DATE FOR REV.:

PREPARER DATE:.REVIEWER* DATE:APPROVER DATE:

IDENTIFICATION OF PAGES ADDEDREVISESUPERSEDEDNOIDED & REVIEW METHOD

INPUTS/ ASSUMPTIONSO VERIFIED

o UNVERIFIED

REVIEW METHOD: , REV.

STATUS: DATE FOR REV.:

PREPARER DATE:REVIEWER DATE:

APPROVER DATE:

v The reviewer's signature indicates compliance with S&L procedure SOP-0402 and the verification of, as a minimum, the followingitems: correctness of mathematics for manual calculations, appropriateness of input data, appropriateness ofassumptions, andappropriateness of the calculation method.

Calc No. M-11165-048-1i *Revision 00

Project No. 11165-048Page 2 of 10

CALCULATIONTABLE OF CONTENTS

Page No.

Signature Page and Issue Summary ........................ ;..................1

Table of Contents .................................................... 2

1.0 Purpose and Scope ........... 3........................................ 32.0 Design input .................................................... 4.

3.0 Assumptions .................................................... 5

4.0 Methodology and Acceptance Criteria ................................................... 65.0 Calculations .................................................... 7

6.0 Results .... 9

7.0 References ................................................... 10

AttachmentsNo. of Pages

A. AutoPIPE Output .34B. Walkdown Information ................ .6

�l-ge4LIJ�ctY



1.1.0

/

PURPOSE AND SCOPE

The purpose of this calculation is to determine the maximum permissible movementdownward of the reactor pressure vessel without compromising the integrity of thebottom-mounted instrumentation conduit attached to the reactor pressure vessel (RPV).

.4

.:0..


uu L ady' Project No. 11165-048Page 40f 10

2.0 DESIGN INPUT

2/1 The overall configuration and routing of the instrumentation conduits are shown In theUnIt 2 drawings (Reference 7.1).

2.2 The AutoPIPE model of a representative Unit 2 instrumentation conduit is based on theas-built walkdown information found In Attachment B.:

2.3 Material allowable stresses are obtained from Reference 7.2.

. . ... .' ..

Calc No. M-1 1165-048-1v eRevision 00


3.0 ASSUMPTIONS

Conservative assumptions have been made to simplify this evaluation; therefore they donot require verification. These assumptions include:

3.1 The representative model is based on the dimensions of the "top" set of conduits,since they~have the shortest horizontal run dimensions and hence provide lessflexibility to accommodate the vessel movement than do the longer "middle" and"bottom3 conduit runs.

3.2 The downward deflections of the conduit are limited by the existing gap betweenthe conduit and the floor. The "bottom" conduit has the smallest gaps; thereforethese gaps are conservatively used to determine the allowable tubing movementdownward before contact Is made with the floor.

3.3 Per the as-built information in Attachment B, the clearance between the bottomset of conduits and the floor varies from 1" to as much as 4.5" (based on thesmallest distance between any support hardware attached to the conduit and thefloor). The analysis conservatively assumes that the entire run Is only allowed todeflect 1" downward before floor contact is made.

3.4 The rigid guides on the riser have gaps of 1/8" to 1/4" between the conduit andthe support U-Bolts. These gaps were conservatively not considered in theanalysis.



4.0 METHODOLOGY AND ACCEPTANCE CRITERIA

4.1 Methodolo6q

A simplified AutoPIPE model of a representative instrumentation conduit was created,running from the connection to the RPV up to the seal table at elevation 41'-0". Iterativeanalyses were performed using Increasing RPV nozzle movements, until the maximumconduit stress reached the stress limit Identified in Section 4.3.

4.2 Acceptance Criteria

Subsection NC-3652.3(b) of Reference 7.2 states that the stress due to any singlenonrepeated anchor movement shall be below 3.0XSc. This may be used as areasonable upper stress limit In the conduit for the postulated vessel deflection.

4.3 Computer Programs Used

AutoPIPE Version 6.00.16 (Reference 7.3).


Project No. 11165-048Projec .Page 7 of 10

5.0 CALCULATIONS

5.1 AutoPIPE Model

A plot of the AutoPIPE model of the In-core Instrumentation conduits Is shown below.The model is based on the Unit 2 walkdown information in Attachment B.

;'>;S. '..S..... -; ........... ''i-''''.-:: ... .... .. . ;

.123

.J

120.. .. .. ..

.*.;; ; * 2 ; : . : . :. ,.. : . .% , ; ' . . ,

..

115.-

5.2 Conduit Properties

The conduit outside diameter was cdded as 1", with a wall thickness of 0.313" (averageof the two values shown In Reference 7.1.1). The material Is ASTM A213 Type 304 per'Reference 7.1.3.

- 1Calc No. M-11165-048-1Revision 00

4u L~redy'. Project No. 11165-048Page 8 of 10

5.3 Routing and Support Arrangement

A 1V-0" straight vertical segment was coded from the RPV nozzle to the start of the firstbend. The bends were modeled using an 8'-0" radius (per Reference 7.1.2). The firstbend off the RPV was subdivided Into four sections to provide more accuratedisplacement information for various parts of the bend. The horizontal skew(approximately 200) of the run beyond the first bend was ignored to simplify the model.This will not have a significant effect on the results. The dimensions used'areapproximate, and are representative of the 36 instrumentation conduits entering thebottom of the RPV (see Section 3.1); An SIF of 1.3 was coded at the vessel connectionand at various coupling locations as shown in the as-built sketch.

The horizontal portion of the lowest conduit is approximately 4" off the floor, but theminimum clearance between support hardware and the floor Is as low as 1" (see Section3.3). This will be used as the allowable deflection downward before the floor begins torestrain conduit movement.

There are several variable/constant spring hangers and snubbers on the conduit; theseare not considered in the analysis since they will not provide significant resistance to thedownward movement of the conduit. The as-built information shows that the spring andconstant supports have sufficient travel to accommodate a downward deflection of atleast 1"; therefore they will not restrain the conduit before it contacts the floor. There aretwo guides on the riser below the deck plating at the 21'-0" elevation.

5.4 Analysis Methodology

The analyses were performed by Inputting a vertical nozzle movement at node 5 andincreasing it until maximum stresses in the conduit approached 3.OSc, which equates tot56,400 psi based on the line material (A213 TP304, per Reference 7.1.3).

It was postulated that the bottom of the bend below the RPV would contact the floor first,after being allowed to displace 1" before being restrained (see Section 3.3).; This contactwas modeled as a vertical support at node "30 F", with a gap below the conduit of 1" anda large gap above the conduit to allow unrestricted upward movement. The analysiswas then performed again, noting the vertical displacements of the conduit on thehorizontal run. Any location exceeding 1" downward was then restrained In subsequentruns. The final configurati6n shown In the preceding plot has supports at nodes "30 F"and "85 N, simulating contact with the floor at those two locations. All the other pointseither deflect upward, or deflect less than 1" downward.

It is postulated that all 36 lines will move in phase, reducing contact between individuallines when the RPV displaces downward.

The AutoPIPE output Is found in Attachment A. The maximum stress for a 23" downwarddisplacement of the RPV is 55,385 psi at node "30 F". This is below the 56,400 psiallowable of 3.OSc.

.1..-

.. ..... ....... ...

...........



6.0 RESULTS

The conduit can accommodate a downward displacement of approximately 23" beforestresses approach the 3.0*Sc stress limit.

, .3- ... ...

-J LLJrIdy

w

Calc No. M- 1165-048-1Revision 00


7.0 REFERENCES

7.1 Westinghouse Drawings of the Bottom-Mounted Instrumentation Lines

7.1.1 Drawing 685J765, Sheet A, Rev. 7.7.1.2 Drawing 685J765, Sheet B, Rev. 7.7.1.3 Drawing 685J765, Sheet C, Rev. 8.

7.2 ASME Boiler and Pressure Vessel Code, Section Ill, Subsection NC, 1977. Edition withWinter 1978 Addenda.

7.3 AutoPIPE Pipe Stress Analysis and Design Program, Version 6.00.16, REBIS IndustrialWorkgroup Software.

Calc. No. M-11 i 65-048-1* 'Revision 00

a.^cLlJun.y. Project No. 11165-048Attachment A

v Page Al of 34

Attachment A

AutoPlPE Output

Calc. No. M-1 1165-048-1Revision 00

Project No. 11165-048.Attachment APage A2 of 34

CONDUIT REBI805/19/2005 AutoPZPE+6.00 MODEL PAGE I________________________________________________________________________________-

** *0

.o *0

000000000

** **

** 0*

000000*

00 00 *00

00000* 0* 00

*0 00 o. 0*0*0 000*0*0

*0 00 00 *0 00 *00

0* 00 00 0* 0* 0*

*0000 00 *0*00 00

*0 000*0*0 0000000

0* 0* *0 00

0* 0* 0* 00

0* 0*00000 *0000

0* 00 00

00 00 00

*0 0* 00*000*

Pipe Stress Analysis and Design Program

Versions 6.00.16

Editions Plus-Win

Developed and Maintained by

REBIS Industrial Workgroup Software1600 Riviera Ave., Suite 300

Walnut Creek, CA 94596

;: >. I

.... . ..

S�r-gnru L.zu-,cfy

Calc . No. M-11165-048-1Revision 00

Project No. 11165-048Attachment A

Page A3 of 34

CONDVUIT REBSOA/19/2005 AutoPIPE+6.00 MODEL PAGE 2

- **-.-*-- ---- *---*- --------*-**.*4*-*4****---4-**4*-4-4**4-*4* **

* at .AUTOPIPZ SYSTEM DATA LISTING *** *Y 44

SYSTEM NAME a CONDUIT

PROJECT ID i (SEE PAGE 1 FOR SIGNATURES)

PREPARED BY X

C0ECKED BY X

PIPING CODE

VERTICAL AXIS

AMBIENT TEMPERATURE

COMPONENT LIBRARY

MATERIAL LIBRARY

MODEL REVISION NUMBER

* B31.1

* Y

* 70.0 dog I

S AUTOPIPI

s AUTOB311

$ 54



Page A4 of 34

CONDUIT REBIS

05/19/2005 AutoPIPE+6.00 MODEL PAGE 3________________________________________________________________________________-

POINT DATA LISTING

POINT ---------OFFSETS (ft

RAME TYPE. x F_____ ___ ---- _ __ ---- --- - _____---

***SEGMENT A5 Run 0 7.831S Send 0 -2.59

20 Bend 1.22 -2.94

25 Bend

30 Bend

Z DESCRIPTION

0 PIPE ID *.0 Elbow, Radius - 95.00 inch

Bend angle change - 22.54 dog8Si r 1.00Flex - 1.000

O zlbow, Radius * 95.00 inchBend angle change * 22.46 dogSir 1.00Flex - 1.000

0 Elbow, Radius - 95.00 inchBend angle change a 22.46 deg817 - 1.00Flex.- 1.000

0 Elbow, Radius - 95.00 inchBond angle change * 22.54 dog8Si r 1.00Flex * 1.000

2.25

2.94

-2.25

-1.22

40 Run43 Run.44 Run-45 Run50 . Run

*-55 Run

57 Run58 Run60 Run65 Run67 Run70 Run73 Run75 Run8S Bend

90 Run95 Run100 Run105 Run110 Run115 Run120 Run122 Run

2.591.001.001.001.001.001.001.00

1.001.001.001.001.001.009.00

000000000000000

000.-0

. 0

.- 000000

00

.0 Elbow, Radius - 96.00 £ncbBend angle change - 90.00 dog817 - 1.00Flex - 1.000

0000

0 11.000 2.330 2.000 2.00

.0 2.460 2.380 5.000 5.00

0000

I

I . I

* N

, .t. 2. P.

1.

Caic . No. M-11165-048-1Revision 00

Project No. 11165-048.'Attachment A: Page A5 of 34

CONDUIT.'-. .. RZBIS

05/19/2005- . . AutoPIPZ+6.00 MODEL PAGE 4

P O N T. D A T A L ST 8 T I a

POINT --OFFSETS (ft )--------KNAS TYPE * T Z DESCRIPTION

123 -Run 0 5.00 0130 Run 0 5.00 0

* Total weight of sty pipe. s 0 lb

I

I �%:- I _ . .

* ;: .. .Caic. No. M-1 1165-048-1Revision 00


Page A6 of 34

CONDUIT REB1S05/19/2005 AutoPZPE+6.00 MODEL PAGZ 5

CONMPONZNT DATA' LISTING

POINT ------COORAMEZ X

***. SECMEN a5 * 0.00

LDXNATU(ft )------ DATAS Z TYPE DESCRIPTION

7.83 0.00 ASCROR RigidThermal movements a TI

USRFLF In - 1.30, Out - 1.30, Flex - AutomaOverride all other values - No

15 N15

15 F20 N2020 r25 N2525 F30 N3030 1

40

*43* 44

45

. ..

50

55 1

5758 260 1

65 1

67 370. 2

7375 2

0.00 6.82 0.000.00 5.24 0.00 TX0.60 3.79 0.00.0.62 3.76 .0.001.22 2.30 0.00 TX2.33 1.19 0.002.36 1.16 0.003.47 0.05 0.00 TX4.92 -0.55 0.004.95 -0.56 0.006.41 -1.17 0.00 TX7.99 -1.17 0.00 V-STOP ID t 30 F1, Connected to Ground

GOp-Dolow - 1.00 inchGap-Above - 50.00 inchFriction * 0.00.Gape set Weightiess

9.00 -1.17 0.00 USRFLS In * 1lO0, Out * 1.00, Flex - AutomaOverride all other values * No

10.0011.0012.00

L3.00

L4.00

L5.00L6.00L7 .00

L8.00

19.0010.00

11.0022.00

-1.17 0.00-1.17 0.00-1.17 0.00 VSRnLX In'- 1.30, Out a 1.30, Flex - Autoar

;:.Override all other values .- NoUSR.LX In,! 1.30,.Out - 1.30, Flex - Autona

Override all other values -NoTSRFLX In - 1.30, Out.- 1.30, Flex a Autoua

Override all other values - No-1.17 0.00 UsRFLzx In - 1.00, Out - 1.00, Flex - Automa

Override all other values - No-1.17 0.00 UsRFLX In- 1;00, out - 1.00, Flex - Automa

Override all other values * No'-1.17 0.00 ,

-1.17 0.00-1.17 0.00 USRFLX In -. 1.30, Out - 1.30, Flex - Auto=a

-1.17

-1.17-1.17

-1.17-1.17

Override all other values - NoUSRFLX In - 1.30, Out - 1.30; Flex a Autoza

Override all other values - NoD0 USRFLX In - 1.00, Out - 1.00, Flex - Automa

Override all other values - No0.I

0.I0.t

D000 USRPLX In - 1.30, Out .1.30, Flex - Automa

Override all'other values a No '0.00 .

0.00 USRFLX In - 1.00, Out * 1.00, Flex * AutomaOverride all other values - No

I . . .. . .. . I - , : .


Project No. 11165-048Attachment APage A7 of 34

CONDUIT REDIS0,/19/2005 AutoPXPZ+6.00 MODEL PAGE 6

COMPONENT DATA LISTING

POINT ------ COORDIAVTE (ft )------ DATANAME X Y Z TYPE DESCRIPTION

85 N. 23.00 -1.17 0.00 V-STOP ID s-85 NI, Connected to.GroundGap-Below * 1.00 inchCap-Above a 50.00 inchFriction a 0.00Gaps get Weightless

USRFLX In a 1.30, Out - 1.30, Flex - AutocaOverride all other values - No

85 31.00 -1.17 0.00 TX85 r 31.00 6.83 0.0090 31.00 9.83 0.00 GUIDE ID : 90 1, Connected to Ground

8tiffness - RIGIDUSRrLX In - 1.00, Out - 1.00, Flex - Automa

Override all other values - No95 31.00 12.17 0.00 USRFLX In - 1.30; Out - 1.30, Flex-- Autom

Override all other values * No100 31.00 14.17 0.00 USRFLX In- 1.00, Out a 1.00, Flex - Automa

Override all other values - No105 31.00 16.17 0.00 USRFZX In *-1.00, Out - 1.00, Flex.- Automa

Override all other values - No110 31.00 18.62 0.00 GUIDE ID x 110 1, Connected to Ground

Stiffnes. - RIGIDVSRFLX ln - 1.00. Out - 1.00, Flex - Automa

Override all other values a No115 31.00 21.00 0.00 USRrLX In - 1.00, Out - 1.00, Flex - Automa

Override all other values a No120 31.00 26.00 0.00122 31.00 31.00 0.00123 31.00 36.00 0.00130 31.00 41.00 0.00 ANCHOR Rigid

Thermal movements t NoneUSRrLX In * 1.30. Out - 1.30, Flex - Automa

Override all other value. * No

Number of points in the system t 40

* Caic. No. M-1 1165-048-1Revision 00

.. ........ Project No. 11165-048Attachment A

; PageA8of34

CONDWI REBIS05/19/2005 AutoPZPE+6.00 MODZL PAGE 7________________________________________________________________________________-

P I P 1 D A T a L I S T I N G

Pip. ZD/ No=/ O.D. -----Thickneus(inch)----- SpecMaterial Sch inch W.Th.'Corr Mill lnau Ling Grav

U1- NS 1.000 0.313 *0 0.04 0 0 0

Weight(lb/ft ) ' ZL/Pipe Other Total ZC

0.00 0 0.00 1.001.00

:. : .V

ml. , ..

Ldy�

Caic. No. M-11165-048-1Revision 00


Page A9 of 34

CONDUIT I EBSqi/19/2005 AutoPZPE+6.00 MODZM PAGZ 8

* A T Z R I A L D A T A L I 8 ST IN

MaterialName

NB

Density Poci. TSiVer. Modulus Z6 psi Expans.Pipe ID lb/cu.ft Ratio dog F Axial Boop Shear inflOOft

1. 0.1 0.30 70.0 28.300 28.300 10.885

CaIc. No. M-1 1165-048-1Revision 00

Project No. 11165-048.Attachment A

Page Al0 of 34

C TNDOXT REBlS05/19/2005 AutoPIPE+6.00 MODEL PAGE 9________________________________________________________________________________--

5ATER1AL ALLOWABLZ DATA LSTING

MaterialNIam Pipe ID

rNs 1 .

Tmp r. Allow.dog F pei

70.0 18800.070.0 18800.0

..; .. '. A, > >{.* 9 . . . . }.,'I

;... ,;.; X -j.,..Calc. No. M-11165-048-1

Revision 00Project No. 11165-048

Attachment APage All of 34

_- - - -- - - - -_ - - -- - - - -- _- -- - - - -- -_-- - - - -- - - _-- - -

CONIWST0/19/2005

REBISAutoPIPE+6.00 MODEL PAGE 10

__________________________ -----------------------------------------------------

TEMPERATURE AIM PRESSURE DATA---- C A 8 : I------ -----AC E 1 - 2------ ----- c a s z 3------

POINT PRESS. TEMPER EXPAN. PRESS. TE(PER EXPAN. PRESS. TEZPER EXPAN.NAM psi dog r in/lOOft ps1 dog J in/lOOft psi deg F in/lOOft_____ ------ ------ -------- ------ ------ -------- ------ ------ --------

-** SEGMW A5 0 70.00130 0 70.00

0.0000.000

Catc. No. M-11165-048-1Revision 00


Page A12 of 34

CODUIT - HIS05/19/2005 AutoPIPE+6.00 MODEL PAGE 11________________________________________________________________________________

XO! T M O D U L U S (Z6 psi )

POINTNWA CASE 1 CASE 2 CASE 3

*** OEGM A5 28.300*130 . 28.300*

* Non-standard -material

:- .. I, i'' .. I

Calc . No. M-1 1165-048-1Revision 00


Page Al3 of 34

COLUIT REMIS

O9/19/2005 AutoPIPZ+6.00 MODEL PAGE 12________________________________________________________________________________

H 0 T

------ CA SEZ 1------POIM NOT NONAME ALLOW USED USED_____ ------ ------ ------

ALLOW B L ZS (pi )------ C A S Z 2------ ------ C A 8 3------

NOT N NOT NOTALLOW USZD USED ALLOW USED USED______ ------ ------ ------ ------ ------

'** SzG~E~T A18800*

130 16800*

< User-defined code allowable* Non-code material

"rg ; dy. '



Page A14 of 34

_- - - - - - - - - -- - - - - - - - - - -- - - - - -_-- -- - - - - - - - - -

CONDUIT05/19/2005

REBISAutoPIPE+6.00 MODEL PACE 13

_________________________________-_____________________________________________-

TSERMAL ANCHOR MOVENE1TS8 AND DISPLACEMENTS

POINT DX DYNAME LOAD CASE (in ) (in )

5 Thermal 1 0.00 -23.00

DZ(in )

0.00

RI(dog )

0.000

RY(dog )

0.000

(deg )

0.000



Page A15 of 34

CCNDUZT RZBIS05/19/2005 AutoPIPE+6.00 RZSULT PAGZ 1________________________________________________________________________________-

AN LXYSS SUMMARY

Current model revision number : 54

Static - Date and Time of analysis ............. M ay.19, 2005Model Revision Number . 54Number of load cases . 2Load cases analyzed . GR S1Gaps/Friction/Soil considered . YesTolerance - Force. Displacement . 1000.00 lbFriction - Scale Factor, Tolerance .... 1.00 0.10Hanger design run .o. NoCut ahort included . noInclude Dourdon rotational effect .. oPipe radius for Bourdon calculation ... MeanOccasional load analysis type .... ..... NonlinearNon-linear analysis summary file ...... CONDUIT.LOGUse default load sequence ............ . YesBass load cases for nonlinear analysis

11:27 AM

0.0010 in

GR - NoneT5 * OR

Weight of contento included .... ....... YesPressure stiffening case .... .......... 0Water elevation for buoyancy loads .... Not consideredHot modulus case used in analysis ..... 0Use corroded thickness in analysis .... No

: .'.':'..': %':>':>. '.,<.'2.. '..'.:. . ;. .. 'l: \ . :: ;; : v .:i Ow- ; ; : . Z b N . *

;s >.>^,\scls.\ .^. :.o; g..: ..

Seent; ndyu

^.@:..$i. s.*w:-r>..-..:-.^ * ....C e * ... , ;: eA,,;/ , ,->t, %/; - -; ,%

Calc. No. M-1165-048-1Revision 00


Page A16 of 34

CONDUIT05/19/2005

REBISAutoPXPE+6.00 RESULT PAGE 2

________________________________________________________________________________

CODE COMPLIANCE COMBINATIONS

Conbination Category Method Load Factor M/S Allowable Remarks

OR + Max P Sustain Sum Gravity 1.00 Automatic DefaultMax Long 1.00

Cold to TI Expansion sum Thermal 1 1.00 Automatic Default

Max P Hoop Max Hoop 1.00 Autcuatic Default

r

---

. Calc. No. M-11165-048-1Revision 00


Page A17 of 34

CON=UT REBlSo%119/2005 AutoPIPE+6.00 RESULT PAGE 3

OTHER USERA COMBINAT:

-c6iuiatiorL Metbod Load

GASum Gravitk

Ti UM Tlienna I

CONS

ractor

1.00

1.*00

Remarks

Default

Def ault

. c - ..1

:: ... .. .. s.:Calc. No. M-1165-048-1Revision 00

Laridy' Project No. 11165-048-.Attachment A

Page A18 of 34

CONDUIT REBI805/19/2005 AutoPIPE+6.00 RESULT PAGE 4

CODZ COMPLIANCZ

Y - Factor ......... 0....... ... 040Weld efficiency factor. 1.00Range reduction factor ................ 1.00Design Pressure Factor .... ......... 1.00Minimum stress ratio used in reports ... 0.00Number of stress points per span ...... 0Include corrosion in stress calc. .... Yinclude axial force in code stress NSet sustained Sir to 1.00 ............ NTotal stress .O.. ............ OctahedralDirect shear ..... ............ NoneLongitudinal pressure calculation ..... PD/4tInclude rigorous pressure ............ Not analyzed

Calc . No. M-111 65-048-1:Revision00

O;{ 3Project No. 11165-048Attachment A

: Page Al9 of 34

CONDUIT REBIS

O/19/2005 AutoPXPE+6.00 RESULT PAGE 5____________D---- -- P__C----_________-__ ___________________________

DX 8P LACZXZNTSS

Point Load TRANSLATIONS (in )name combination X Y Z

__ _ ___ -_ _ _ __ __ __ __ -____-----__ ----- -- --- -L

ROTATIONS (deog )x Y Z

. - - - ------ ____ _ -____

-*** Segment A

5 GRTi

15 N ORTi

S5 r ORTi

20 N GRTi

20 F GRTi

25 N GRTi

2S r CRT1

30 N GRT1

30 F GRT1

40 ORTi

43 GRTi

44 GRTi

45 CRT1

50 GRT1

55 GRTI

begin ***

0.000 0.000 0.0000.000 -23.000 0.000

0.000 0.000 0.0000.062 -23.000 0.000

0.000 0.000 0.0001.957 -22.506 0.000

0.000 0.000 0.0001.996 -22.490 0.000

0.000 0.000 0.0006.993 -1.976 0.000

0.000 0.000 0.0007.064 -18.904 0.000

0.000 0.000 0.00012.393 -10.796 0.000

0.000 0.000 0.00012.437 -10.690 '0.000

0.000 -0.001 0.00014.446 -0.999 0.000

0.000 -0.001 0.00014.446 1.409 0.000

0.000 -0;001i 0.00014.446 3.263 0.000

'0.000 -0.001 0.00014.446 4.637 0.000

0.000 -0.001 0.;00014.446 5.575 0.000

0.000 -0.001 0.00014.446 6.116 0.000

0.0000.000

0.000* 0.000

0.0000.000

O.0000.000

* 0.0000.000

0.0000.000

0.0000.000

0.0000.000

' 0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.000 0.0000.000 0.000

0.000 0.0000.000 0.689

0.000 0.0000.000 5.964

0.000 0.0000.000 6.037

0.000 0.0000.000 12.729

0.000 0.0000.000 12.800

0.000 0.0000.000 16.359

0.000 0.0000.000 16.365

0.000 0.0000.000 12.685

0.000 0.0000.000 10.063

0.000 0.0000.000 7.674

0.000 0.0000.000 5.486

0.000 ' 0.000

0.000 3.498

0.000 .0.0000.000 -1.709

O.'000 -0.001 0.000 0.000 0.000 0.0000.000 0.000 0.12114.446 6.304 0.000

. i.

* .. -Calc. No. M-1 1165-048-1Revision 00

u ? <: .Project No. 11165-048Attachment A

Page A20 of 34

CONDUIT REB1S05/19/2005 AutoPIPE+6.00 RESULT PAGZ 6

DI SPLACZXZNTS

Point Loadnan. combbination

57 GRTi

58 aRT1

60 GRTi

65 GRTi

67 GRT1

70 ORT1

73 ORTi

75 GRTl

85 N oRTi

85 * ORT1

90 OR

Ti

95 ORTi

100 OR

Ti

105 oRTi

110 ORTi

115 GRTi

TRANSLATIONS (in ).X Y Z

0.000 -0.001 0.00014.446 6.181 0.000

0.000 -0.001 0.00014.446 5.787 0.000

0.000 -0.001 0.00014.446 5.166 0.000

0.000 -0.001 0.00014.446 4.359. 0.000

0.000 -0.001 0.00014.446, 3.408 0.000

0.000 -0.001 0.00014.445 2.354 0.000

0.000 -0.001 0.00014.445 1.241 0.000

0.000 -0.001 0.00014.445 0.109 .0.000

0.000 0.000 0.00014.445 -1.000 0.000

0.000 0'.000 0.0005.175 0.002 0.000

0.000 0.000 . 0.0000.000 0.002 0.000

0.000 0.000 0.000-1.745 0.002 0.000

0.000 0.000 0.000-1.844 0.001 0.000

0.000 0.000 0.000-1.169 0.001 0.000

0.000 0.000 0.0000.000 0.001 0.000

0.000 0.000 0.0000.837 0.001 0.000

ROTATIONS (dog )_

0.000

0.000

0.000

0.000

0.000

0.000

0.000

0.000

0O000

0.000

0.000

0.000

0.000

0.000

0.000

0.000

0.000

0.000

.0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.000

0.0000.000

0.0000.000

0.0000.000

0.000.0.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.0000.000

0.000O .000

z

0 .000-1.267

0.000-2.455

0.000-3.443

0.000-4.231

0.000-4.818

0.000-5.206

0.000-5.394

0.000-5.381

0.000-5.169

0.0009.711

0.0005.857

0.0001.549

0.000-0.881

0.000-2.145

0.000-2.102

0.000-1.279

Cal. No. M-1 1 165-048-1Revision 00


Page A21 of 34

COMDUITS R1DZO3/19/2005 AutoPIPE+6.00 RESULT PAGE 7__________________________________________D______P_________C____________________-

D 8PLtA C ZX Z NS8

Point Loadname comnination

120 . GR

T1

122 GRT1

123 GR51

130 GRTi

TR.ASLATIONS (in ) ROTATONS (dog )X Y Z S Z

0.000 0.000 0.000 0.000 0.000 0.0001.459 0.001 0.000 0.000, 0.000 -0.01O

0.000 0.000 0.000 0.000 0.000 0.0001.088 0.001 0.000 0.000 0.000 0.619

0.000 0.000

0.382 0.000

0.000 0.0000.000 0.000

0.000

0.000

0.000

0.000

0.000 0.000

0.000 0.000

0.000 0.000

0.000 0.000

0.000

0.624

0.0000.000

*** Segment A end *^*



Page A22 of 34

CONDUXT REB1S05/19/2005 AutoPZPE+6.00 RESULT PAGE 8

R E ST R A I 2 T aR z aC T Z 0 N 8

Point Loadname combinatiton

5 zAnchorORTi

FORCES (lb ) MOMENTS (ft-lb )T Y Z Result x Y Z Result

0 0 0 .0 0 0 -0 0-99 175 0 201 0 0 62 62

30 F V - Stop lIDt 30 r1]aR 0 . 0TI 0 -208

0 00 208

0.- 0 0 00 0 0 0

85 N V - StopGRTi

90 GuideOR

* T1

110 GuideGRTI

IlDs 8500

Nil0

-520 0 0 0 0

0 52 0 . 0 0 0

(ID: 900

147

EID: 1100

-52

1i

11

0 0 00 0 147

0 0 0 00 0 0 0

0 0 0 0 0 0 0O 0 52 0 0 0 0

130 AnchoraRTi

0 0 0 0 0 ,0 0 04 85 0 e5 0 0 31 31

. 'i "ik:1%

. i .;S t: .

:: . . .



Page A23 of 34

CO11DU1T RZBXS05/19/2005 AutoPIPE+6.00 RZSULT PACZ 9

________________________________________________________________________________

GLOBAL F.ORCZ8 & cMOMZENTS

Point Load FORCZS (lb ) MOMENTS (ft-lbname coenbination X Y Z Result X . S Z Result

------ _____ ____ ------ ------ ------ ------- ------- ------- -------__ __

se Segment A begin *

5 GR *Ti 95

15 1N GRTi 9

1S F GRt151 ! R

TI 9!

2011 ORTi. 9!

207r GRTl 9!

251 .. ,ORT1 9!

Ti 91

30 r: OR C

TI 9!

3 .FOR CTI 9!

30 F+ OR CTI 9S

40- 01RT1 99

.43 ORT1 99

44 OR 0

T1 99

45 OR 05T 99

D a1 -175

3 01 -175

0) -175

O O..g -175

O *0g -175

09 -175

09 -175

P 09 -175

I 09 -175

1 09 33

I. 0I 33

1 .3I 033

033

g 33

0 00 201

0 0e 201

a 0a 201

a. 00 201

o 0

0 201

O - O0 201

0 00 201

0 00 201

0 00 201

0 00 105

0 00 105

o ao 105

0 00 105

o 0

0 105

00

00

00

00

00

00

00

00

0

0

0

0*

0

0

0

0

0*

0

0 0 00 -62 62

0 0 00 -163 163

. 0 00 -358 358

0 0 00 -359 359

0 0 00 -313 313

0 0 00 -311 311

0 .0 00 -32 32

o o 0

0 -27 27

o 0 0O *44 444

0 0 00 444 444

0 ,0 a0 411 411

0 0 00 378 378

0 0 00 345 345

0 . 0 00 312 312

50 CRT1

0 099 33

0 0O 105

0 0 .0 00 . 0 279 279

Calc . No. M-11165-048-1Revision 00

Projeci No. 11165-048.Attachment A

Page A24 of 34

-- -- - - - - _-- - - - -- - - - - - -_-- - - - -- - - - - - -_-- - - - -

CONDUIT05/19/2005

RZ1ILAutoPIPE+6.00 RESULT PAGE 10

GLOBAL FORCF8 & 1OMrNTS

Point Load FORCES (lb ) MOMENzTS (ft-lb )name combination X Y Z Result X Y Z Reault______ ----------- ------ ------ ------ ------ ------- ------- ------- -------

55. GRTI

57 GRT1

0 099 33

0 099 33

0 00 105

0 00 105

0 0 00 0 246

0 0 00 0 213

246

0213

58 aR 0. 0 0 0TI 99 33 0 105

0 0 0 00 0 180 180

60 CRTi

65 GRTl

67 CRTi

70 CRTi

73 CRTS

75 GRTi

85 N- GRTi

85 N+ GRTi

85 F GRT1

90 - GR

Ti

90 + OR

Ti

95 GRT1

0 099 33

0 099 33

0 099 33

0 099 33

0 099 .33

0 099 33

0' 099 33

0 099 85

0 099 e5

0 099 85

0 0-48 85

a a-48 85

0, 0.0 105

0 a0 105

0 00 *105

0 00 105

0 00 105

0 00 105

0 00 105

.0 00 131

0 00 131

0 . 00 131

0 00 98

0 00 98

0 0 00 0 147

0 0. . a

0 0 114

0 0 00 0 81

0 0 00 a 47

0.0

00

00

00

0 a0 14

0 00 -19

0 00 -52

0 00 -52

0147

0114

081

047

014

019

052

052

063

0361

0361

0.249

0 0 00 0 63

0 ***0 00 0 361.

0 0 00 0 361

0 0 00 0 249

100 GRTI

0 0 0 0-48 85 0 98

00 0 0 00 0 152 152


!3>rgin L y Project No. 11165-048Attachment A

Page A25 of 34

CON=UST REBlS0'/19/2005 AutoPIPE+6.00 RESULT PAGZ 11

GLOBAL FORCFS & MOXENTS

Point . Load FORCZS (lb ) MOMENTS (ft-lbname combination X Y Z Result S Y Z Result

105, GR 0 0 0 0 0 0 0 0* TI -48 85 0 98 0 0 56 56

110 -OR 0 0 0 0 0 0 0 0Ti -48 85 0 98 0 0 -62 62

110 0R 0 0 0 0 0 0 0 0Ti 4 85 0 85 0 0 -62 62

115 OR 0 0 0 0 0 0 0 0Ti 4 85 0 85 0 0 -52 52

120 GR 0 0 0 0 0 0 0 0Ti 4 85 0 as 0 0 -31. 31

122 OR 0 0 0 0 0 0 0 0Ti 4 85 0 85 0 0 -11 11

123 GR 0 0 0 0 0 0 0 0Ti 4 85 *0 85 0 0 10 10

130 GR 0 0 0 0 0 0 0 0TS 4 85 0 85 0 0 31 31

*** Segment A end ***

%LJiJY�.



Page A26 of 34

CONDUIT / REB1S05/19/2005 AutoPIPE+6.00 RESULT PAGE 12_______________ _______________ _______________ _______________ __________ -____

ASME B31.1 (1998) CODE COMPLIANCE(Moments in ft-lb ) (

Point Load Ma Mb Mo Eq. Iname combination (Sus.) (Occ.) (Exp.) B.1.F no. t

**- Segment A begin ***

:Stress in psiLoad Codetype Stress

Codeftllo.

5 Mai PaR + Mazx PCold to TI

15 N- Max PGOR Max PCold to TI

15 N+ Max PGR + Max PCold to TS

0

0

0

1S F- Max PGR + Max P 0Cold to Tiwith Sun. load margin

15 I+ Max PGR * Max P 0Cold to Tiwith Sue. load margin

20 N- Max PGR + Max P 0Cold to Tlwith Bus. load margin

20 N+ Max PGR-+ Max P 0Cold to Tiwith Bus. load margin

20 F- Max PGR. + Max P 0Cold to Tiwith sun. load margin

20 r+ max PGR + Max P 0Cold to Tiwith Sus. load margin

25 N- Max PGR + lax P 0Cold to Tiwith Sum. load margin

( 3) HOOP1.30 (ll) BUST

62 1.30 (13) DIEP

3) HOOP1.00 (Il) SU8T

163 1.00 (13) DIsP

( 3).HOOP1.00 (Il) 8UST

163 1.00 (13) .DiSP

( 3) HOOP1.00 (11) SUST

358 1.00 (13) DISP(13)

( 3) HOOP1.00 (11) BUST

.358 1.00 (13) DISP(13)

( 3) HOOP1.00 (11) BUST

359 1.00 (13) DISP(13)

1 3) HOOP1.00 (11) BUST

359 1.00 (13) DI8P(13)

13) HOOP1.00 (11) BUST

313 1.00 (13) DISP(13)

1 3) HOOP1.00 (11) BUST

313 1.00 (13) DSSP(13)

: 3) HOOP1.00 (11) BUST

*311 1.00 (13) DISP(13)

01

10062

00

20269

00

20269

01

4460444604

01

4460444604

01

4470744707

01

4470744707

01

3898138981

01

38981*38981

01

3872838728

188001880028200

18800'1880028200

188001880028200

188001880028200*446999

188001880028200k46999

188001880028200k46999

188001880028200**46999

188001880028200*46999

188001880028200*46999

18800188002820046999



Page A27 of 34

CONDUIT REBIS0,/19/2005 AutoPXPE+6.00 RESULT PAGE 13

…__________ ___________---…-_- ________________________________________________

ASME B31.1 (1998) CODE COMPLIANCZ(Moments in ft-lb ) I

Point Load Ma Mb Ic Eq. Iname combination (Bus.) (Occ.) (Exp.) S.I.F no. t

-_____ ----------- ------- ------- ------- ------- ---- -

:Stream in p.l,oad Codetype StressI--- ------

25 N* Max P* GR + Maxc P O

Cold to T1with Bus. load margin

( 3) HOOP 01.00 (11) WUST 1

311 1.00 (13) DISP 38728(13) 38728

Code

Milow.

188001880028200"*46999

25 F- max P¢R + Max PCold to Ti

2S F+ Sax POR + Max PCold to T1

0

0

1 3) HOOP1.00 (11) BUST

32 1.00 (13) DISP

( 3) HOOP1.00 (11) WUST

32 1.00 (13) DI8P

0 188001 18800

3935 28200

0 188001 18800

3935 28200

30 N- Max P6R + Max PCold to Ti

30 N+ MaX POR + Max PCold to Ti

0( 3)

2 1.00 (11)27 1.00 (13)

C 3)1.00 (11)

27 1.00 (13)

HOOPBUSTDISP

HOOPWUST

DIP0

30 *- max POR + M P 0Cold to Tiwith Bus. load margin

30 F+ Max.PGR + MaxP 0

Cold to T1with Sus, load margin

40 Max PGR + ax P 0Cold to Tiwith Bus. load margin

43 Max PGR + Max P 0Cold to Tiwith Sus. load margin

44 Max PGR + MaxP 0Cold to Tiwith Su. load margin

45 N" PGR + Max P 0Cold to T1

( 3) HOOP1.00 (11) WUST

444 1.00 (13) DIBP(13)

( 3) HOOP1;00 (11) BUST

444 1.00 (13) DXBP(13)

( 3) HOOP1.00 (11) BUST

411 1.00 (13) DISP(13)

( 3) HOOP1.00 (11) BUST

378 1.00 (13) DISP(13)

1 3) HOOP1.00 (11) BUST

345 1.00 (13) DISP(13)

1 3) HOOP1.30 (11) BUST

312 1.30 (13) DISP

01

3416

0I

3416

00

5538555385

0.0

5538555385

01

5121651216

01

4709847098

0. 1

4298042980

02

50521

1880018800

28200

188001880028200

188001880028200**47000**

188001880028200**47000**

18800.1880028200^^46999**

188001880028200***46999**

188001880028200*"46999

188001880028200"*

fiv.Calc. No. M-1 1165-048-1


.Attachment APage A28 of 34

CONDUIT REBIS05/19/2005 AutoPIPE+6.00 RESULT PAGZ 14________________________________________________________________________________-

Point

_____

ASMZ B31.1 (1998) CODE COMPLIANCZ(Momenta in ft-lb ) (Stress in pmi

Load Ma Fb NC Eq. Load Code Codecombination (Bus.) (occ.) (zxp.) 8.1.Y no. type Stress Allow.

with Bum. load margin (13) 50521 46998**

50 Xax PGRxP M0x P O

Cold to Tiwith Bus. load margin

55 xax PGR + Max P 0Cold to TIwith Bus. load margin

( 3) HOOP1.00 (11) S8ST

279 1.00 (13) DISP(13)

02

3474434744

188001880028200k*46998

( 3)1.00 (11)

246 1.00 (13)(13)

HOOPSUSDISP:

02

3062630626

02

26508

188001880028200k*46998

188001880028200

57 aIZ PCR + Max PCold to 5I

.,

58 Max.PCR.+ Max PCold to TS

60 Max PGR '+ Max PCold to T1

65 Max PGRi + Max PCold to Ti

67 Max PGR + Max PCold to TI

0 1.00213 1.00

( 3) HOOP(11) SUBS(13) DI8P

( 3) HOOP1.00 (11) SUBT

- 180 1.00 (13) DIST

( 3) HOOP1.30 (11) BUSU

147 1.30 (13) DISP

0 188002 18800

22390 28200

0

0

0 188002 18800

23754 28200

0

( 3)1.00 (11)

114 1.00 (13)

C 3)1.00 (11)

81 1.00 (13)

( 3)1.30 (11)

47 1.30 (13)

( 3)1.00 (11)

14 1.00 (13)

HOOPSUSDISP

HOOPSUWSDISP

02

14155

01

10037

188001880028200

188001880028200

70 Max PGR + Max PCold to Ti

73 Maz PGR + Max PCold to TI

CHOOPSUSTDISP

HOOPSUBTDISP

01

7695

01

1801

188001880028200

188001880028200

0


...

85 N- Max PGR + Max PCold to TI

0( 3) HOOP

1.00 (11) SUST19 1.00 (13) DISP

( 3) HOOP1.30 (11) SUST.

52 1.30 (13) DZSP

0 188000 18800

2317 28200

0 188000 18800

8365 282000

Calc. No. M-1 1165-048-1;Revision00

3~rge Lm~a~dy~Project No. 11165-04Attachment A

. :Page A29 of 34

CONDUIT RBISQ5/19/2005 AutoPXPE+6.00 RESULT PAGE 15________________________________________________________________________________

A8MZ B31.1 (1998) CODE COMPLIANCE(Moments in ft-lb ) t

Point Load Ka Mab Mc EZq. Iname coabination (Sus.) (Occ.) (Exp.) 8.1.F no. t

[stress in ]PiLoad CodeY"e Stress

85 N 1Max P. ( 3) HOOPOR + Max P 0 . 1.30 (11) BUSTCold to TI 52 1.30 (13) DISP

______

00

8365

CodeAllow.

188001880028200

85 P- Mxx PGR + Max PCold to T1

85 F+ Max POR + Max PCold to Ti

0

0

90 Max PR + MaxP 0

Cold to Tiwith Bus. load margin

95 Max PGR + MaxP 0Cold to TIwith Bus. load margin

' ( 3) HOOP1.00 (11) OUST

63 1.00 (13) DISP

( 3) HOOP1.00 (11) BUST

63 1.00 (13) DISP

( 3) HOOP1.00 (11) BUST

361 1.00 (13) DISP(13)

( 3) HOOP1.30 (11) BUST

249 1.30 (13) DISP(13)

00

7878

00

7878

02

4499544995

01

4030140301

188001880028200

188001880028200

18800.1880028200**46998

188001880028200**46999


105 Max POR + KaIPCold to Ti

110 )ax POR + Max PCold to Ti

0

0

0

115 Max PGR + Max PCold.to Ti

120 max POR + Max PCold to Ti


123 Max PCR + Max PCold to Ti

0

0 .

0

0

3) HOOP1.00 (11) BUST

152 1.00 (13) DISP

( 3) HOOP1.00 (11) SUST

56 1.00 (13) DISP

( 3) HOOP1.00 (11) BUST

62 1.00 (13) DISP

( 3) HOOP1.00 (11) 8UST

52 1.00 (13) DISP

3) HOOP1.00 (11) BUST

31 1.00 (13) D08P

( 3) HOOP1.00 (11) BUST

11 1.00 (13) DXSP

3) HOOP1.00 (11) 8UST

10 1.00 (13) DISP

0 188001 18800

19006 28200

0 188000 18800

7011 282 00

0 188000 18800

7731 28200

00

6498

00

3907

. 0.0

1316

00

1275

1880018800282 00

1880018800282 00

188001880028200

188001880028200

%LLY�..

CaIc. No. M-11165-048-1Revision 00


Page A30 of 34

CONDUIT REBIS05/19/2005 AutoPIPE+6.00 RESULT PAGE 16________________________________________________________________________________-

pointname

130

Loadcombination

Ma POR + Max PCold to Tl

ASEE 331.1 (1998) CODE COMPLIANCE(Mcments in ft-lb ) (Stress in psi

Ma MM Xc Eq. Load Code Code(Sus.) (occ.) (Exp.) 8.x.r no. type Stress Allow.

( 3) HOOP 0 188000 1.30 (11) BUST 0 18800

31 1.30 (13) DISP 5025 28200

*** Segment A end ***


L rdy* . Project No. 11165-048;-Attachment A

. Page A31 of 34

CONDWIT REBlS0,/i19/2005 AutoPIPE+6.00 RESVLT PAGE 17

8Y8 5 Z SUMMARY____________________________

Maximum displacements (in)___________________________--

Max4mm X

Maximum Y sMax. totals

14.446-23.00023.000

Point : 30Point : SPoint I S

r Load Comb.: TILoad Comb.: TILoad Comb.: Ti

Maximum rotations (dog)_______________________

Maximum ZMax. totals

16.36516.365

Point s 30 KPoint s 30 N

Load Comb.s TILoad Comb.: TI

Maximum restraint forces (lb)______________________________

MaximumMaximum Y :Max. total:

147 Point : 90-208 Point * 30208 Point t 30

rFr

Load Ccmb.s TiLoad Comb.l TILoad Comb.: Ti

Maximum restraint moments (ft-lb)__________________________________

axi4u- Z : 62Max. total: .62

Point a 5Point s 5

Load Comb.: TiLoad Comb.s Ti

* |



Page A32 of 34

CONDUIT REBI805/19/2005 AutoPIPE+6.00 RESULT PAGE 18________________________________________________________________________________-

SYSTEXI SuNNARYS Y 8 T Z ---- 8--------a-R-S

laximm pipe forces (lb)__________________ _______

Xaxiiuzm zMaxiji Y tMax. totals

99 Point s 20-175 Point r 20201 Point - 5

NF

MSaxi4m pipe ah=ntx (ft-lb)

M3aximua Z t 444Max. totals .444

Load Coub. s TiLoad Ccmb.,t T1Load Caonb.: TiS

Load Comnb.s TSLoad Ccomb.: TI

Point s 30 rPoint s 30 r

I

,age~ L -: ?rldy",:Caic. No. M-1 1165-048-1


Attachment APage A33 of 34

CONDUIT REBIO%/19/2005 AutoPIPE.6.00 RESULT PACE 19________________________________________________________________________________

SYSTEZM SUvMARY

Maximum sustained stress

PointStress psiAllowable psiRatioLoad combination

t 57i2a 188002 0.00r GR + Max P

Maximum displacement stress;

PointStress psiAllowable psiRatioLoad combination

: 30 F: 55385t 47000S 1.18t Cold to T1



Page A34 of 34

:---------r-------- -----------------------------------------------.______________COTDUfS REB:I05/19/2005 AutoPXPZ+6.00 RESULT PAGE 20________________________________________________________________________________

SYSTEM SUMMARY

M axizmm sustained stress ratio

Pointstress psiAllowable psiRatioLoad cobination

s 57t22 188008 0.00*R + Max P

Maximum displacement stress ratio

pointstress psiAllowable psiRatioLoad combination

i 30 F: 55385a 470002 1.18a Cold to TI

* * * The system does not satisfy ASZE B31.1 code requirements * * ** ^ * for the selected options

: C .s ~ *..o .e .


Project No. 11165-048Attachment BPage B1 of 6

I/

Attachment B

As-Built Information

Caic . No. M-1 11 65-048-1Revision 00

~LAJ1dY.Project No. 1 1165-048.Attachment aeB Bf

Maean......a..e.To ~ORGE2.TOKARStdbswgeni~nyw.c~an~si~resnnmco 'rJYESHANTOLIACsarqenimdycm

S~~et abdown kifo2u,:i2DU d 07:54 . ..A....

Mtr ttevsel: and'work~ back ito ..the ikeyway e.4ntrance at" te .21 E:lelvatibion~,..

01.. ...TE.: .... . ..

.Teeaetwo,,snubbers bolding .the::*spider jueb!_ support.,under th

RS 7 sinln '2it t7 tiibl gidSters.FedDt o E-7Grnl uprsoFgure 20,Seia3571. !',(odl I H L302Z' "Stroke =5 -

NOE ha CW4S at Dffrsfro theF .Feld. Data

... ereVera no Moderlmn~brsi et.-n2S3l ' 3".. ... . -.. . ' '

2. . ll Bltsupports haegp~sc ht~oa'clearance ifromto0'iie sraeo ot and pipe:] is approx> 3/,"to 1/4" NDTotl sde-sidet

clearanc betwen ipe ~ and~-Bolt iA,.18to31.

,SrigCasar se.or-he mex upport after: then Znbes"i i~.next' suipport:,after. snbe sie reba tubes.: tr avel'ba ck:Ilrom vesse

.toardkeyay ntrnce. To "prig 'ansHold up tree: strcuachannel` to .WhiC'h thei gUid e Mubes -are--otd' . .

:iSpring Can Data GrZiiel'piqHne'Fur 2Sieo8

' 2 Z ;-:.he'sup~~"jport syste S. isc htteSporchnescudovs iCh asaprx ~1" dowinwid beifor6 ea omtlcnatocr

!.4. i ' Btee -hesiderwbsupr sse andthspigan tec...:'-learance boetween: the fTloor anid :-boto ro fguide. tbs -wvas tmesuired a

th Owe St: Ipot'te botmf n tube_ ws: 1 1/4'. fro h for..nost ~;All: .oiers .Were -alt leakst 2 ro .tefloor at: the' lowe st i-spots Rt h

-uesare, qitflxbeitisaean- . appatosgaitl

S-Between .the:. Spider: we suprytem and -the: spri g canstetubs Sen sli ighatly in a, hori zo..tl pln ih fter the. Spring can; u Bls

the trvel hoizntaly nti thy tari-t6 tobend ~vertically;:supward -:- The" ipproxiiar.e% Tagn.ie.o tesato hsVerticalpar~--bending ~is:as folows

,.Botto o'o12Tbs--anetle is approz 9-:'B-1 FoSpigCnUBl upports.

Kidd~eP~ov f 12-ubes'-'Tanent lne isApprox.:'''8 FoSpigCan:.U Bolt ,Supor

:T~op liow;,of l,2 iT~ikbes :-Tange~nt linie is ajpprox V~!.- .- SI.: From Srn

Can i Bot:Sppot . .......-- '

6' - ~~First sat of iPipe icoulng nth ub4u sarigatte

nngr. i".' Co -a d .. .he....- .~.Ls s4oios ~ :back-

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Project No. 11165-048Attachment BPage B3 of 6

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BotmRo f12 Tubes Cupig ar lcae 4" - 4"after

.>7 -: .:Constant Supports then exist in the tubing runs 149 11R4 a.fter'-;i: ,

* Cnw.: a ortField Data rin.aelC t Spr F ''' '''7,gu c.treKillE-B. 'Seria 355045 (Se rialSt takei'fro .one "of 'the suports),..Size'BOOS',fcfx..'i

Two .bof these'ConstantuSupports hold up0three structural channels

* ~to which the gud 'tubes'.are:U bolt*edc2'

Theporsuprsytmisuhtathchnescudov41/

d<:ownwrd befor e there is metal .to ata icontacti :;j: 0;~.:;5 . ,

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'.:.8 >:'' <><;" T>he Cuide tubes.'then start bending vertically 'upward';toward the';;cf:s

'keywayten: enrnc haltbl ......

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Consant, Sport UDolts .'; -.<s.;..The bending continues untilfthetubespare vertical ,vhich cscurs;.

~approximately 36 belo : the'ne set ofU-Bolts'an;the'vertical'rn',p towar ds

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Sye :ssc; ... -R;hi.-,Ihanne>,.,,..u,.d,=v,, :4 -

<:9--' 'wdef o"e. thertical. runs directly below the key.aytentrance.area deck"'pilating have tw osets of U- Bolts holding them<i- i;,*;t-<,,f;:

.;One setis 36 afe~thertes'coplete ,there verticalyupw ard

."-cbends '(as described in *8 above), .these U-,bolts are'c140 .. Below the keyvay;':;'.^;enr nce ' deck' plat :.'cing

.ff.<'", T'. eU.he' second seta of fU-Bolts is 10 1/2 b'elow the Keyway,.entrance.,e c

;. e ..', an.; q: .~~ap i.'x;.w,..,;e .C.: .-..;.,.,....Az

10>l TfS c. here,' is a'second set'.of pipe couplings- they exist in .the c,-h,*.*':vertical :runs directly below the keyua yentrance deck plating.. The couplings>'s-i;'

ae Ilic the. 'fk2t PbotXset of U oltsin t 'v i

11.-,Mant,:.supp Tre iv pt t a o g ustlikewoccucrssonUnit2

w;ilfl'turn over y field sketches to a^ne Karean (or otherDesilgn Personnel'.working on this:issue' if Jane'isnot yetin) and explayinny details prioreto.

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