ML051580337

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Calculation M-11165-048-1, Rev 00, Evaluation of Bottom-Mounted Instrument (Bmi) Conduits for Postulated Reactor Vessel Displacement
ML051580337
Person / Time
Site: Point Beach NextEra Energy icon.png
Issue date: 05/19/2005
From: Tokarski G
Sargent & Lundy
To:
Office of Nuclear Reactor Regulation
References
M-11165-048-1, Rev 00
Download: ML051580337 (51)
v • d • e


Text

ENCLOSURE 4 REACTOR VESSEL BOTTOM MOUNTED INSTRUMENT TUBE ANALYSIS (50 pages follow)

Calc No. M-1 1165-048-1 Revision 00 SrgenojS Lzrady'X*Project No. 11165-048 Page 1 of 10 ISSUE

SUMMARY

DESIGN CONTROL

SUMMARY

CLIENT: Nuclear Management Companv UNIT NO.: 2 Page No.:. 1 PROJECT NAME: Point Beach PROJECT 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 Reactor Vessel Displacement EQUIPMENTNO.: N/A IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDNOIDED & REVIEW METHOD First Issue INPUTS/ ASSUMPTIONS 0 VERIFIED o UNVERIFIED REVIEW METHOD: Detailed Review REV. 00 STATUS: Approveg { DATE FOR REV.: 05-19-2005 PREPARER G. Z. Tokarski DATE: -s -ULD REVIEWER* J.N.Tolia Ji4'Ec ok\° DATE: s,/qtof APPROVER' G. Z. Tokarski DATE: Laos-° IDENTIFICATION OF PAGES ADDED/REVISED/SUPERSEDEDNOIDED & REVIEW METHOD INPUTS/ ASSUMPTIONS o VERIFIED o UNVERIFIED REVIEW METHOD: REV.

STATUS: ' DATE FOR REV.:

PREPARER DATE:.

REVIEWER* DATE:

APPROVER DATE:

IDENTIFICATION OF PAGES ADDEDREVISESUPERSEDEDNOIDED & REVIEW METHOD INPUTS/ ASSUMPTIONS O 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 following items: correctness of mathematics for manual calculations, appropriateness of input data, appropriateness ofassumptions, and appropriateness of the calculation method.

Calc No. M-11165-048-1 i *Revision 00 Project No. 11165-048 Page 2 of 10 CALCULATION TABLE OF CONTENTS Page No.

Signature Page and Issue Summary ........................ ;..................1 Table of Contents .................................................... 2

1.0 Purpose and Scope

........... 33........................................

2.0 Design input .................................................... 4.

3.0 Assumptions .................................................... 5 4.0 Methodology and Acceptance Criteria ................................................... 6 5.0 Calculations .................................................... 7 6.0 Results .... 9 7.0 References ................................................... 10 Attachments No. of Pages A. AutoPIPE Output .34 B. Walkdown Information ................ .6

Calc No. M-1 1165-048-1 Revision 00 l-ge4LIJctY Project No. 11165-048 Page 3 of 10 1.

1.0 PURPOSE AND SCOPE

/

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

.4

.:0..

Calc No. M-1 1165-048-1 Revision 00 uu L ady' Project No. 11165-048 Page 40f 10 2.0 DESIGN INPUT 2/1 The overall configuration and routing of the instrumentation conduits are shown In the UnIt 2 drawings (Reference 7.1).

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

2.3 Material allowable stresses are obtained from Reference 7.2.

Calc No. M-1 1165-048-1 v eRevision 00 Project No. 11165-048 Page 5 of 10 3.0 ASSUMPTIONS Conservative assumptions have been made to simplify this evaluation; therefore they do not 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 less flexibility 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 between the conduit and the floor. The "bottom" conduit has the smallest gaps; therefore these gaps are conservatively used to determine the allowable tubing movement downward before contact Is made with the floor.

3.3 Per the as-built information in Attachment B, the clearance between the bottom set of conduits and the floor varies from 1" to as much as 4.5" (based on the smallest distance between any support hardware attached to the conduit and the floor). The analysis conservatively assumes that the entire run Is only allowed to deflect 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 and the support U-Bolts. These gaps were conservatively not considered in the analysis.

Calc No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Page 6 of 10 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". Iterative analyses were performed using Increasing RPV nozzle movements, until the maximum conduit 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 single nonrepeated anchor movement shall be below 3.0XSc. This may be used as a reasonable upper stress limit In the conduit for the postulated vessel deflection.

4.3 Computer Programs Used AutoPIPE Version 6.00.16 (Reference 7.3).

Calc No. M-11 165-048-1 Revision 00 Project No. 11165-048 Projec .Page7 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.

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'..S.....

.123

.J 115.-

.. .. .. .. *.;; ;

  • 2  ; 120: . : . :. ,..  :  % , . ; .' . . . ,

5.2 Conduit Properties The conduit outside diameter was cdded as 1", with awall thickness of 0.313" (average of the two values shown InReference 7.1.1). The material Is ASTM A213 Type 304 per

'Reference 7.1.3.

- 1Calc No. M-11165-048-1 Revision 00 4u L~redy'. Project No. 11165-048 Page 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 first bend. The bends were modeled using an 8'-0" radius (per Reference 7.1.2). The first bend off the RPV was subdivided Into four sections to provide more accurate displacement 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'are approximate, and are representative of the 36 instrumentation conduits entering the bottom of the RPV (see Section 3.1); An SIF of 1.3 was coded at the vessel connection and 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 the minimum clearance between support hardware and the floor Is as low as 1" (see Section 3.3). This will be used as the allowable deflection downward before the floor begins to restrain conduit movement.

There are several variable/constant spring hangers and snubbers on the conduit; these are not considered in the analysis since they will not provide significant resistance to the downward movement of the conduit. The as-built information shows that the spring and constant supports have sufficient travel to accommodate a downward deflection of at least 1"; therefore they will not restrain the conduit before it contacts the floor. There are two 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 and increasing it until maximum stresses in the conduit approached 3.OSc, which equates to t56,400 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 contact was modeled as a vertical support at node "30 F", with a gap below the conduit of 1" and a large gap above the conduit to allow unrestricted upward movement. The analysis was then performed again, noting the vertical displacements of the conduit on the horizontal run. Any location exceeding 1" downward was then restrained In subsequent runs. 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 points either deflect upward, or deflect less than 1" downward.

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

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

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

.1..- Revision 00 Project No. 11165-048

........... Page 9 of 10 6.0 RESULTS The conduit can accommodate a downward displacement of approximately 23" before stresses approach the 3.0*Sc stress limit.

, .3- ... ...

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

-J LLJrIdy Project No. 11165-048 w Page 10 of 10

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 with Winter 1978 Addenda.

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

Calc. No. M-11 i 65-048-1

  • 00

'Revision a.^cLlJun.y. Project No. 11165-048 Attachment A v Page Al of 34 Attachment A AutoPlPE Output

Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048

.Attachment A Page A2 of 34 CONDUIT REBI8 05/19/2005 AutoPZPE+6.00 MODEL PAGE I 000000* *0 000*0*0 0000000 00 00 *00 0* 0* *0 00

    • *0 00000* 0* 00 0* 0* 0* 00

.o *0 *0 00 o. 0*0*0 000*0*0 0* 0*00000 *0000 000000000 *0 00 00 *0 00 *00 0* 00 00

    • ** 0* 00 00 0* 0* 0* 00 00 00
    • 0* *0000 00 *0*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 Software 1600 Riviera Ave., Suite 300 Walnut Creek, CA 94596

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Calc . No. M-11165-048-1 Revision 00 Sr-gnru L.zu-,cfy Project No. 11165-048 Attachment A Page A3 of 34 CONDVUIT REBS OA/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

  • B31.1 VERTICAL AXIS
  • Y AMBIENT TEMPERATURE
  • 70.0 dog I COMPONENT LIBRARY S AUTOPIPI MATERIAL LIBRARY s AUTOB311 MODEL REVISION NUMBER $ 54

Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A 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 Z DESCRIPTION

      • SEGMENT A 5 Run 0 7.83 0 PIPE ID
  • 1S Send 0 -2.59 .0 Elbow, Radius - 95.00 inch Bend angle change - 22.54 dog 8Si r 1.00 Flex - 1.000 20 Bend 1.22 -2.94 O zlbow, Radius
  • 95.00 inch Bend angle change
  • 22.46 dog Sir 1.00 Flex - 1.000 25 Bend 2.25 -2.25 0 Elbow, Radius - 95.00 inch Bend angle change a 22.46 deg 817 - 1.00 Flex.- 1.000 30 Bend 2.94 -1.22 0 Elbow, Radius - 95.00 inch Bond angle change
  • 22.54 dog 8Sir 1.00 Flex
  • 1.000 40 Run 2.59 0 0 43 Run 1.00 0 0

.44 Run 1.00 0 0.-

-45 Run 1.00 0 0 50 . Run 1.00 0 .0

  • -55 Run 1.00 0

.- 0 57 Run 1.00 0 0

58 Run 1.00 0 0

60 Run 1.00 0 0

65 Run 1.00 0 0

67 Run 1.00 0 0

70 Run 1.00 0 73 Run 1.00 0 0 75 Run 1.00 0 0 8S Bend 9.00 0 .0 Elbow, Radius - 96.00 £ncb Bend angle change - 90.00 dog 817 - 1.00 Flex - 1.000 90 Run 0 11.00 0 95 Run 0 2.33 0 100 Run 0 2.00 0 105 Run 0 2.00 0 110 Run .0 2.46 0 I 115 Run 0 2.38 0 120 Run 0 5.00 0 122 Run 0 5.00 0 I . I

  • N

, t. . 2. P.

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

.'Attachment A

Page A5 of 34 1.

CONDUIT.'-. .. RZBIS 05/19/2005- . . AutoPIPZ+6.00 MODEL PAGE 4 P O N T. D AT A L ST8 T I a POINT --OFFSETS (ft )--------

KNAS TYPE

  • T Z DESCRIPTION 123 -Run 0 5.00 0 130 Run 0 5.00 0
  • Total weight of sty pipe. s 0 lb I

I %:- I _ ..

  • ;: .. .Caic. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A6 of 34 CONDUIT REB1S 05/19/2005 AutoPZPE+6.00 MODEL PAGZ 5 CONMPONZNT DATA' LISTING POINT ------ COOR LDXNATU(ft )------ DATA AMEZ X S Z TYPE DESCRIPTION
      • . SECMEN a 5
  • 0.00 7.83 0.00 ASCROR Rigid Thermal movements a TI USRFLF In - 1.30, Out - 1.30, Flex - Automa Override all other values - No 15 N 0.00 6.82 0.00 15 0.00 5.24 0.00 TX 15 F 0.60 3.79 0.00 20 N .0.62 3.76 .0.00 20 1.22 2.30 0.00 TX 20 r 2.33 1.19 0.00 25 N 2.36 1.16 0.00 25 3.47 0.05 0.00 TX 25 F 4.92 -0.55 0.00 30 N 4.95 -0.56 0.00 30 6.41 -1.17 0.00 TX 30 1 7.99 -1.17 0.00 V-STOP ID t 30 F1, Connected to Ground GOp-Dolow - 1.00 inch Gap-Above - 50.00 inch Friction
  • 0.00.

Gape set Weightiess 40 9.00 -1.17 0.00 USRFLS In

  • 1lO0, Out
  • 1.00, Flex - Automa Override all other values
  • No
  • 43 10.00 -1.17 0.00
  • 44 11.00 -1.17 0.00 45 12.00 -1.17 0.00 VSRnLX In'- 1.30, Out a 1.30, Flex - Autoar
.Override all other values .- No USR.LX In,! 1.30,.Out - 1.30, Flex - Autona Override all other values -No TSRFLX In - 1.30, Out.-1.30, Flex a Autoua Override all other values - No 50 L3.00 -1.17 0.00 UsRFLzx In - 1.00, Out - 1.00, Flex - Automa Override all other values - No 55 1L4.00 -1.17 0.00 UsRFLX In- 1;00, out - 1.00, Flex - Automa Override all other values
  • No 57 L5.00 '-1.17 0.00 ,

58 2L6.00 -1.17 0.00 60 1L7 .00 -1.17 0.00 USRFLX In -. 1.30, Out - 1.30, Flex - Auto=a Override all other values - No USRFLX In - 1.30, Out - 1.30; Flex a Autoza Override all other values - No 65 1L8.00 -1.17 0.I D0 USRFLX In - 1.00, Out - 1.00, Flex - Automa Override all other values - No 67 319.00 -1.17 0.I D0

70. 210.00 -1.17 0.t 00 USRPLX In - 1.30, Out .1.30, Flex - Automa Override all'other values a No '

73 11.00 -1.17 0.00 .

75 222.00 -1.17 0.00 USRFLX In - 1.00, Out

  • 1.00, Flex
  • Automa Override all other values - No I . . .. . .. . I -, : .

Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A7 of 34 CONDUIT REDIS 0,/19/2005 AutoPXPZ+6.00 MODEL PAGE 6 COMPONENT DATA LISTING POINT ------ COORDIAVTE (ft )------ DATA NAME X Y Z TYPE DESCRIPTION 85 N. 23.00 -1.17 0.00 V-STOP ID s-85 NI, Connected to.Ground Gap-Below

  • 1.00 inch Cap-Above a 50.00 inch Friction a 0.00 Gaps get Weightless USRFLX In a 1.30, Out - 1.30, Flex - Autoca Override all other values - No 85 31.00 -1.17 0.00 TX 85 r 31.00 6.83 0.00 90 31.00 9.83 0.00 GUIDE ID : 90 1, Connected to Ground 8tiffness - RIGID USRrLX In - 1.00, Out - 1.00, Flex - Automa Override all other values - No 95 31.00 12.17 0.00 USRFLX In - 1.30; Out - 1.30, Flex-- Autom Override all other values
  • No 100 31.00 14.17 0.00 USRFLX In- 1.00, Out a 1.00, Flex - Automa Override all other values- No 105 31.00 16.17 0.00 USRFZX In *-1.00, Out - 1.00, Flex.- Automa Override all other values - No 110 31.00 18.62 0.00 GUIDE ID x 110 1, Connected to Ground Stiffnes. - RIGID VSRFLX ln - 1.00. Out - 1.00, Flex - Automa Override all other values a No 115 31.00 21.00 0.00 USRrLX In - 1.00, Out - 1.00, Flex - Automa Override all other values a No 120 31.00 26.00 0.00 122 31.00 31.00 0.00 123 31.00 36.00 0.00 130 31.00 41.00 0.00 ANCHOR Rigid Thermal movements t None USRrLX 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 1165-048-1 Revision 00

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

PageA8of34 CONDWI REBIS 05/19/2005 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)----- Spec Weight(lb/ft ) ' ZL/

Material Sch inch W.Th.'Corr Mill lnau Ling Grav Pipe Other Total ZC NS U1- 1.000 0.313 *0 0.04 0 0 0 0.00 0 0.00 1.00 1.00

. : .V ml., ..

Caic. No. M-11165-048-1 Revision 00 Ldy Project No. 11165-048 Attachment A Page A9 of 34 CONDUIT I EBS qi/19/2005 AutoPZPE+6.00 MODZM PAGZ 8

  • A T Z R I AL D AT A L I 8ST IN Material Density Poci. TSiVer. Modulus Z6 psi Expans.

Name Pipe ID lb/cu.ft Ratio dog F Axial Boop Shear inflOOft NB 1. 0.1 0.30 70.0 28.300 28.300 10.885

CaIc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048

.Attachment A Page Al0 of 34 C TNDOXT REBlS 05/19/2005 AutoPIPE+6.00 MODEL PAGE 9 5ATER1AL ALLOWABLZ DATA LSTING Material Tmp r. Allow.

NIam Pipe ID dog F pei rNs 1. 70.0 18800.0 70.0 18800.0

..;'. ..A, >>{.* 9 . . . . }.,'I Calc. No. M-11165-048-1

... ,;.; X -j.,..

Revision 00 Project No. 11165-048 Attachment A Page All of 34 CONIWST REBIS 0/19/2005 AutoPIPE+6.00 MODEL PAGE 10 TEMPERATURE AIM PRESSURE DATA

C A AC8 E : 1I------ - ----- 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 A 5 0 70.00 0.000 130 0 70.00 0.000

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

.Attachment A Page A12 of 34 CODUIT - HIS 05/19/2005 AutoPIPE+6.00 MODEL PAGE 11 XO! T M O D U L U S (Z6 psi )

POINT NWA CASE 1 CASE 2 CASE 3

      • OEGM A 5 28.300*

130 . 28.300*

  • Non-standard -material
- .. I,i .. I

Calc . No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page Al3 of 34 COLUIT REMIS O9/19/2005 AutoPIPZ+6.00 MODEL PAGE 12 H 0 T ALLOW B L ZS (pi )

CA SEZ 1------ ------ C A S Z 2------ ------ C A 8 3------

POIM NOT NO NOT N NOT NOT NAME ALLOW USED USED ALLOW USZD USED ALLOW USED USED

'** SzG~E~T A 18800*

130 16800*

< User-defined code allowable

  • Non-code material

Calc. No. M-1 1165-048-1 "rg; dy. ' Revision 00 Project No. 11165-048

.Attachment A Page A14 of 34 CONDUIT REBIS 05/19/2005 AutoPIPE+6.00 MODEL PACE 13 TSERMAL ANCHOR MOVENE1TS8 AND DISPLACEMENTS POINT DX DY DZ RI RY NAME LOAD CASE (in ) (in ) (in ) (dog ) (dog ) (deg )

5 Thermal 1 0.00 -23.00 0.00 0.000 0.000 0.000

Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A15 of 34 CCNDUZT RZBIS 05/19/2005 AutoPIPE+6.00 RZSULT PAGZ 1 AN LXYSS

SUMMARY

Current model revision number : 54 Static - Date and Time of analysis ............. M ay.19, 2005 11:27 AM Model Revision Number . 54 Number of load cases . 2 Load cases analyzed . GR S1 Gaps/Friction/Soil considered . Yes Tolerance - Force. Displacement . 1000.00 lb 0.0010 in Friction - Scale Factor, Tolerance .... 1.00 0.10 Hanger design run .o. No Cut ahort included . no Include Dourdon rotational effect .. o Pipe radius for Bourdon calculation ... Mean Occasional load analysis type .... ..... Nonlinear Non-linear analysis summary file ...... CONDUIT.LOG Use default load sequence ............. Yes Bass load cases for nonlinear analysis GR - None T5

  • OR Weight of contento included .... .......Yes Pressure stiffening case .... ..........0 Water elevation for buoyancy loads .... Not considered Hot modulus case used in analysis ..... 0 Use corroded thickness in analysis .... No

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Calc. No. M-1165-048-1

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Attachment A Page A16 of 34 CONDUIT REBIS 05/19/2005 AutoPXPE+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 Default Max 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-11165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A17 of 34 CON=UT REBlS o%119/2005 AutoPIPE+6.00 RESULT PAGE 3 OTHER USERA COMBINAT:CONS

-c6iuiatiorL Metbod Load ractor Remarks Default GASum Gravitk 1.00 Default Ti UM Tlienna I 1.*00

. c- .

.1

... .. ..s.:Calc. No. M-1165-048-1 Revision 00 Laridy' Project No. 11165-048

-.Attachment A Page A18 of 34 CONDUIT REBI8 05/19/2005 AutoPIPE+6.00 RESULT PAGE 4 CODZ COMPLIANCZ Y - Factor ......... ... 040 0.......

Weld efficiency factor. 1.00 Range reduction factor ................ 1.00 Design Pressure Factor .... ......... 1.00 Minimum stress ratio used in reports ... 0.00 Number of stress points per span ...... 0 Include corrosion in stress calc. .... Y include axial force in code stress N Set sustained Sir to 1.00 ............ N Total stress .O.. ............ Octahedral Direct shear ..... ............ None Longitudinal pressure calculation ..... PD/4t Include rigorous pressure ............ Not analyzed

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

Revision00 O;{ 3Project No. 11165-048 Attachment 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 ) ROTATIONS (deog )

name combination X Y Z x Y Z

___ _ _ __----- __ __ __-- --- -L . - - - ------

-*** Segment A begin ***

5 GR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 0.000 -23.000 0.000 0.000 0.000 0.000 15 N OR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 0.062 -23.000 0.000

  • 0.000 0.000 0.689 S5 r OR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 1.957 -22.506 0.000 0.000 0.000 5.964 20 N GR 0.000 0.000 0.000 O.000 0.000 0.000 Ti 1.996 -22.490 0.000 0.000 0.000 6.037 20 F GR 0.000 0.000 0.000
  • 0.000 0.000 0.000 Ti 6.993 -1.976 0.000 0.000 0.000 12.729 25 N GR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 7.064 -18.904 0.000 0.000 0.000 12.800 2S r CR 0.000 0.000 0.000 0.000 0.000 0.000 T1 12.393 -10.796 0.000 0.000 0.000 16.359 30 N GR 0.000 0.000 0.000 0.000 0.000 0.000 T1 12.437 -10.690 '0.000 0.000 0.000 16.365 30 F GR 0.000 -0.001 0.000 ' 0.000 0.000 0.000 T1 14.446 -0.999 0.000 0.000 0.000 12.685 40 OR 0.000 -0.001 0.000 0.000 0.000 0.000 Ti 14.446 1.409 0.000 0.000 0.000 10.063 43 GR 0.000 -0;001i 0.000 0.000 0.000 0.000 Ti 14.446 3.263 0.000 0.000 0.000 7.674 44 GR '0.000 -0.001 0.000 0.000 0.000 0.000 Ti 14.446 4.637 0.000 0.000 0.000 5.486 45 CR 0.000 -0.001 0.;000 0.000 0.000 ' 0.000 T1 14.446 5.575 0.000 0.000 0.000 3.498 50 GR 0.000 -0.001 0.000 0.000 0.000 .0.000 T1 14.446 6.116 0.000 0.000 0.000 -1.709 55 GR O.'000 -0.001 0.000 0.000 0.000 0.000 TI 14.446 6.304 0.000 0.000 0.000 0.121

. i.

  • .. -Calc. No. M-1 1165-048-1 Revision 00 u  ? <:

.Project No. 11165-048 Attachment A Page A20 of 34 CONDUIT REB1S 05/19/2005 AutoPIPE+6.00 RESULT PAGZ 6 DI SPLACZXZNTS Point Load TRANSLATIONS (in ). ROTATIONS (dog )

nan. combbination X Y Z _ z 0.000 57 GR 0.000 -0.001 0.000 0.000 0.000 0 .000 Ti 14.446 6.181 0.000 0.000 0.000 -1.267 58 aR 0.000 -0.001 0.000 0.000 0.000 0.000 T1 14.446 5.787 0.000 0.000 0.000 -2.455 60 GR 0.000 -0.001 0.000 0.000 0.000 0.000 Ti 14.446 5.166 0.000 0.000 0.000 -3.443 65 GR 0.000 -0.001 0.000 0.000 0.000 0.000 Ti 14.446 4.359. 0.000 0.000 .0.000 -4.231 67 GR 0.000 -0.001 0.000 0O000 0.000 0.000 T1 14.446, 3.408 0.000 0.000 0.000 -4.818 70 OR 0.000 -0.001 0.000 0.000 0.000 0.000 T1 14.445 2.354 0.000 0.000 0.000 -5.206 73 OR 0.000 -0.001 0.000 0.000 0.000 0.000 Ti 14.445 1.241 0.000 0.000 0.000 -5.394 75 GR 0.000 -0.001 0.000 0.000 0.000 0.000 Tl 14.445 0.109 .0.000 0.000 0.000 -5.381 85 N oR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 14.445 -1.000 0.000 0.000 0.000 -5.169 85

  • OR 0.000 0'.000 0.000 .0.000 0.000 0.000 T1 5.175 0.002 0.000 0.000 0.000 9.711 90 OR 0.000 0.000 . 0.000 0.000 0.000 0.000 Ti 0.000 0.002 0.000 0.000 0.000 5.857 95 OR 0.000 0.000 0.000 0.000 0.000 0.000 Ti -1.745 0.002 0.000 0.000 0.000 1.549 100 OR 0.000 0.000 0.000 0.000 0.000 0.000 Ti -1.844 0.001 0.000 0.000 0.000 -0.881 105 oR 0.000 0.000 0.000 0.000 0.000 0.000 Ti -1.169 0.001 0.000 0.000 0.000 -2.145 110 OR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 0.000 0.001 0.000 0.000 0.000 -2.102 115 GR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 0.837 0.001 0.000 0.000 O .000 -1.279

Cal. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A21 of 34 COMDUITS R1DZ O3/19/2005 AutoPIPE+6.00 RESULT PAGE 7

__________________________________________D______P_________C____________________-

D 8PLtA C ZX Z NS8 Point Load TR.ASLATIONS (in ) ROTATONS (dog )

name comnination X Y Z S Z 120 . GR 0.000 0.000 0.000 0.000 0.000 0.000 T1 1.459 0.001 0.000 0.000, 0.000 -0.01O 122 GR 0.000 0.000 0.000 0.000 0.000 0.000 T1 1.088 0.001 0.000 0.000 0.000 0.619 123 GR 0.000 0.000 0.000 0.000 0.000 0.000 51 0.382 0.000 0.000 0.000 0.000 0.624 130 GR 0.000 0.000 0.000 0.000 0.000 0.000 Ti 0.000 0.000 0.000 0.000 0.000 0.000

      • Segment A end *^*

CaIc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A22 of 34 CONDUXT REB1S 05/19/2005 AutoPZPE+6.00 RESULT PAGE 8 R E ST R A I 2 T aRz aC T Z 0 N 8 Point Load FORCES (lb ) MOMENTS (ft-lb )

name combinatiton T Y Z Result x Y Z Result 5 zAnchor OR 0 0 0 .0 0 0 -0 0 Ti -99 175 0 201 0 0 62 62 30 F V - Stop lIDt 30 r1]

aR 0 . 0 0 0 0.- 0 0 0 TI 0 -208 0 208 0 0 0 0 85 N V - Stop IlDs 85 Nil GR 0 0 0 0 0 0 0 Ti 0 -52 0 52 0 . 0 0 0 90 Guide (ID: 90 1i OR 0 0 0 0 0 0 0 0

  • T1 147 0 0 147 0 0 0 0 110 Guide EID: 110 11 GR 0 0 0 0 0 0 0 0 TI -52 O 0 52 0 0 0 0 130 Anchor aR 0 0 0 0 0 ,0 0 0 Ti 4 85 0 e5 0 0 31 31

. 'i "i k:1%

. i .;S t: .

Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A23 of 34 CO11DU1T RZBXS 05/19/2005 AutoPIPE+6.00 RZSULT PACZ 9 GLOBAL F.ORCZ8cMOMZENTS &

Point Load FORCZS (lb ) MOMENTS (ft-lb name coenbination X Y Z Result X . S Z Result se Segment A begin

  • 5 GR *D a 0 0 0 0 0 0 Ti 951 -175 0 201 0 0 -62 62 15 1N GR 3 0 0 0 0 0 0 0 Ti 91 -175 e 201 0 0 -163 163 1S F GRt 0 a 0 0 . 0 0 151 R  !

0 -358 358 TI 9!) -175 a 201 0 2011 OR O O.. a. 0 0 0 0 0 Ti. 9! g -175 0 201 0 0 -359 359 207r GR O *0 o 0 0 0 0 0 Tl 9!g -175 0 201 0 0 -313 313 251.. ,OR 0 O - O 0 0 0 0 T1 9! 9 -175 0 201 0 0 -311 311 0 0 0 0 0 .0 0 Ti 919 -175 0 201 0 0 -32 32 0

30 r: OR CP 0 0 0 0 o o 0 TI 9!9 -175 0 201 0 0 -27 27 3 .FOR CI 0 0 0 0 o 0 0 TI 9!9 -175 0 201 O *44 444 0

30 F+ OR C1 0 0 0 0 0 0 0

TI 9S9 33 0 105 0 444 444 0*

40- 01R I. 0 0 0 0 ,0 a 0

T1 99I 33 0 105 0 411 411 0

.43 OR I 1 .3 0 o a 0 0 0 T1 99 33 o 105 0 378 378 0

44 OR 0 0 0 0 0 0

T1 99 33 0 105 0 345 345 0

0 45 OR 0 o 0 0 . 0 0 0*

5T 99 g 33 0 105 0 312 312 50 CR 0 0 0 0 0 0 .0 0 T1 99 33 O 105 0 . 0 279 279

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

.Attachment A Page A24 of 34 CONDUIT RZ1IL 05/19/2005 AutoPIPE+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. GR 0 0 0 0 0 0 0 TI 99 33 0 105 0 0 246 246 57 GR 0 0 0 0 0 0 0 0 T1 99 33 0 105 0 0 213 213 58 aR 0. 0 0 0 0 0 0 0 TI 99 33 0 105 0 0 180 180 60 CR 0 0 0, 0 0 0 0 0 Ti 99 33 .0 105 0 0 147 147 65 GR 0 0 0 a 0 0. . a 0 Tl 99 33 0 105 0 0 114 114 67 CR 0 0 0 0 0 0 0 0 Ti 99 33 0 *105 0 0 81 81 70 CR 0 0 0 0 0 0 0 0 Ti 99 33 0 105 0 a 47 47 73 CR 0 0 0 0 0 0 a 0 TS 99 .33 0 105 .0 0 14 14 75 GR 0 0 0 0 0 0 0 0 Ti 99 33 0 105 0 0 -19 19 85 N- GR 0' 0 0 0 0 0 0 0 Ti 99 33 0 105 0 0 -52 52 85 N+ GR 0 0 .0 0 0 0 0 0 Ti 99 85 0 131 0 0 -52 52 85 F GR 0 0 0 0 0 0 0 0 T1 99 e5 0 131 0 0 63 63 90 - GR 0 0 0 . 0 0 ***0 0 0 Ti 99 85 0 131 0 0 361. 361 90 + OR 0 0 0 0 0 0 0 0 Ti -48 85 0 98 0 0 361 361 95 GR a a 0 0 0 0 0 0 T1 -48 85 0 98 0 0 249 .249 100 GR 0 0 0 0 00 0 0 0 TI -48 85 0 98 0 0 152 152

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

!3>rgin L y Project No. 11165-048 Attachment A Page A25 of 34 CON=UST REBlS 0'/19/2005 AutoPIPE+6.00 RESULT PAGZ 11 GLOBAL FORCFS & MOXENTS Point . Load FORCZS (lb ) MOMENTS (ft-lb name 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 0 Ti -48 85 0 98 0 0 -62 62 110 0R 0 0 0 0 0 0 0 0 Ti 4 85 0 85 0 0 -62 62 115 OR 0 0 0 0 0 0 0 0 Ti 4 85 0 85 0 0 -52 52 120 GR 0 0 0 0 0 0 0 0 Ti 4 85 0 as 0 0 -31. 31 122 OR 0 0 0 0 0 0 0 0 Ti 4 85 0 85 0 0 -11 11 123 GR 0 0 0 0 0 0 0 0 Ti 4 85 *0 85 0 0 10 10 130 GR 0 0 0 0 0 0 0 0 TS 4 85 0 85 0 0 31 31
      • Segment A end ***

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

%LJiJY. Project No. 11165-048

.Attachment A Page A26 of 34 CONDUIT / REB1S 05/19/2005 AutoPIPE+6.00 RESULT PAGE 12 ASME B31.1 (1998) CODE COMPLIANCE (Moments in ft-lb ) (:Stress in psi Point Load Ma Mb Mo Eq. I Load Code Code name combination (Sus.) (Occ.) (Exp.) B.1.F no. t type Stress ftllo.

    • - Segment A begin ***

5 Mai P ( 3) HOOP 0 18800 aR + Mazx P 0 1.30 (ll) BUST 1 18800 Cold to TI 62 1.30 (13) DIEP 10062 28200 15 N- Max P 3) HOOP 0 18800 GOR Max P 0 1.00 (Il) SU8T 0 '18800 Cold to TI 163 1.00 (13) DIsP 20269 28200 15 N+ Max P ( 3).HOOP 0 18800 GR + Max P 0 1.00 (Il) 8UST 0 18800 Cold to TS 163 1.00 (13) .DiSP 20269 28200 1S F- Max P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) SUST 1 18800 Cold to Ti 358 1.00 (13) DISP 44604 28200*4 with Sun. load margin (13) 44604 46999 15 I+ Max P ( 3) HOOP 0 18800 GR

  • Max P 0 1.00 (11) BUST 1 18800 Cold to Ti .358 1.00 (13) DISP 44604 28200k with Sue. load margin (13) 44604 46999 20 N- Max P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) BUST 1 18800 Cold to Tl 359 1.00 (13) DISP 44707 28200k with Bus. load margin (13) 44707 46999 20 N+ Max P 1 3) HOOP 0 18800 GR-+ Max P 0 1.00 (11) BUST 1 18800 Cold to Ti 359 1.00 (13) DI8P 44707 28200**

with Bus. load margin (13) 44707 46999 20 F- Max P 13) HOOP 0 18800 GR.+ Max P 0 1.00 (11) BUST 1 18800 Cold to Ti 313 1.00 (13) DISP 38981 28200*

with sun. load margin (13) 38981 46999 20 r+ max P 1 3) HOOP 0 18800 GR + Max P 0 1.00 (11) BUST 1 18800 Cold to Ti 313 1.00 (13) DSSP 38981 28200*

with Sus. load margin (13) *38981 46999 25 N- Max P  : 3) HOOP 0 18800 GR + lax P 0 1.00 (11) BUST 1 18800 Cold to Ti *311 1.00 (13) DISP 38728 28200 with Sum. load margin (13) 38728 46999

Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A27 of 34 CONDUIT REBIS 0,/19/2005 AutoPXPE+6.00 RESULT PAGE 13 ASME B31.1 (1998) CODE COMPLIANCZ (Moments in ft-lb ) I:Stream in p.l Point Load Ma Mb Ic Eq. I ,oad Code Code name combination (Bus.) (Occ.) (Exp.) S.I.F no. t type Stress Milow.

------- ------- - I--- ------

25 N* Max P ( 3) HOOP 0 18800

  • GR + Maxc P O 1.00 (11) WUST 1 18800 Cold to T1 311 1.00 (13) DISP 38728 28200"*

with Bus. load margin (13) 38728 46999 25 F- max P 1 3) HOOP 0 18800

¢R + Max P 0 1.00 (11) BUST 1 18800 Cold to Ti 32 1.00 (13) DISP 3935 28200 2S F+ Sax P ( 3) HOOP 0 18800 OR + Max P 0 1.00 (11) WUST 1 18800 Cold to T1 32 1.00 (13) DI8P 3935 28200 30 N- Max P ( 3) HOOP 0 18800 6R + Max P 0 2 1.00 (11) BUST 1 18800 Cold to Ti 27 1.00 (13) DISP 3416 28200 30 N+ MaX P C 3) HOOP 0 18800 OR + Max P 0 1.00 (11) WUST I 18800 Cold to Ti 27 1.00 (13) DIP 3416 28200 30 *- max P ( 3) HOOP 0 18800 OR + M P 0 1.00 (11) WUST 0 18800 Cold to Ti 444 1.00 (13) DIBP 55385 28200**

with Bus. load margin (13) 55385 47000**

30 F+ Max.P ( 3) HOOP 0 18800 GR + MaxP 0 1;00 (11) BUST .0 18800 Cold to T1 444 1.00 (13) DXBP 55385 28200**

with Sus, load margin (13) 55385 47000**

40 Max P ( 3) HOOP 0 18800.

GR + ax P 0 1.00 (11) BUST 1 18800 Cold to Ti 411 1.00 (13) DISP 51216 28200^^

with Bus. load margin (13) 51216 46999**

43 Max P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) BUST 1 18800 Cold to Ti 378 1.00 (13) DISP 47098 28200**

with Sus. load margin (13) 47098 *46999**

44 Max P 1 3) HOOP 0 18800 GR + MaxP 0 1.00 (11) BUST . 1 18800 Cold to Ti 345 1.00 (13) DISP 42980 28200*"

with Su. load margin (13) 42980 46999 45 N" P 1 3) HOOP 0 18800 GR + Max P 0 1.30 (11) BUST 2 18800 Cold to T1 312 1.30 (13) DISP 50521 28200"*

Calc. No. M-1 1165-048-1 fiv. Revision 00 Project No. 11165-048

.Attachment A Page A28 of 34 CONDUIT REBIS 05/19/2005 AutoPIPE+6.00 RESULT PAGZ 14 ASMZ B31.1 (1998) CODE COMPLIANCZ (Momenta in ft-lb ) (Stress in pmi Point Load Ma Fb NC Eq. Load Code Code combination (Bus.) (occ.) (zxp.) 8.1.Y no. type Stress Allow.

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

50 Xax P ( 3) HOOP 0 18800 GRxP M0x P O 1.00 (11) S8ST 2 18800 Cold to Ti 279 1.00 (13) DISP 34744 28200k*

with Bus. load margin (13) 34744 46998 55 xax P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) SUS 2 18800 Cold to TI 246 1.00 (13) DISP: 30626 28200k*

with Bus. load margin (13) 30626 46998 57 aIZ P ( 3) HOOP 0 18800 CR + Max P 0 1.00 (11) SUBS 2 18800 Cold to 5I 213 1.00 (13) DI8P 26508 28200 58 Max.P ( 3) HOOP 0 18800 CR.+ Max P 1.00 (11) SUBT 2 18800 Cold to TS - 180 1.00 (13) DIST 22390 28200 60 Max P ( 3) HOOP 0 18800 GR '+ Max P 0 1.30 (11) BUSU 2 18800 Cold to T1 147 1.30 (13) DISP 23754 28200 65 Max P ( 3) HOOP 0 18800 GRi + Max P 0 1.00 (11) SUS 2 18800 Cold to Ti 114 1.00 (13) DISP 14155 28200 67 Max P C 3) HOOP 0 18800 GR + Max P 0 1.00 (11) SUWS 1 18800 Cold to TI 81 1.00 (13) DISP 10037 28200 70 Max P ( 3) HOOP 0 18800 GR + Max P C 1.30 (11) SUST 1 18800 Cold to Ti 47 1.30 (13) DISP 7695 28200 73 Maz P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) SUBT 1 18800 Cold to TI 14 1.00 (13) DISP 1801 28200 75 Max P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) SUST 0 18800 Cold to Ti 19 1.00 (13) DISP 2317 28200 85 N- Max P ( 3) HOOP 0 18800 GR + Max P 0 1.30 (11) SUST. 0 18800 Cold to TI 52 1.30 (13) DZSP 8365 28200

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

Revision00 3~rge Lm~a~dy~Project No. 11165-04 Attachment A

. :Page A29 of 34 CONDUIT RBIS Q5/19/2005 AutoPXPE+6.00 RESULT PAGE 15 A8MZ B31.1 (1998) CODE COMPLIANCE (Moments in ft-lb ) t[stress in ]Pi Point Load Ka Mab Mc EZq. I Load Code Code name coabination (Sus.) (Occ.) (Exp.) 8.1.F no. t Y"e Stress Allow.

85 N 1Max P. ( 3) HOOP 0 18800 OR + Max P 0 . 1.30 (11) BUST 0 18800 Cold to TI 52 1.30 (13) DISP 8365 28200 85 P- Mxx P ' ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) OUST 0 18800 Cold to T1 63 1.00 (13) DISP 7878 28200 85 F+ Max P ( 3) HOOP 0 18800 OR + Max P 0 1.00 (11) BUST 0 18800 Cold to Ti 63 1.00 (13) DISP 7878 28200 90 Max P ( 3) HOOP 0 18800 R + MaxP 0 1.00 (11) BUST 2 .18800 Cold to Ti 361 1.00 (13) DISP 44995 28200**

with Bus. load margin (13) 44995 46998 95 Max P ( 3) HOOP 0 18800 GR + MaxP 0 1.30 (11) BUST 1 18800 Cold to TI 249 1.30 (13) DISP 40301 28200**

with Bus. load margin (13) 40301 46999 100 Max P 3) HOOP 0 18800 GR + Max P 0 1.00 (11) BUST 1 18800 Cold to Ti 152 1.00 (13) DISP 19006 28200 105 Max P ( 3) HOOP 0 18800 OR + KaIP 0 1.00 (11) SUST 0 18800 Cold to Ti 56 1.00 (13) DISP 7011 282 00 110 )ax P ( 3) HOOP 0 18800 OR + Max P 0 1.00 (11) BUST 0 18800 Cold to Ti 62 1.00 (13) DISP 7731 28200 115 Max P ( 3) HOOP 0 18800 GR + Max P 0 1.00 (11) 8UST 0 18800 Cold.to Ti 52 1.00 (13) DISP 6498 282 00 120 max P 3) HOOP 0 18800 OR + Max P 0 . 1.00 (11) BUST 0 18800 Cold to Ti 31 1.00 (13) D08P 3907 282 00 122 Max P ( 3) HOOP . 0 18800 GR + Max P 0 1.00 (11) BUST .0 18800 Cold to Ti 11 1.00 (13) DXSP 1316 28200 123 Max P 3) HOOP 0 18800 CR + Max P 0 1.00 (11) 8UST 0 18800 Cold to Ti 10 1.00 (13) DISP 1275 28200

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

%LLY.. Project No. 11165-048

. Attachment A Page A30 of 34 CONDUIT REBIS 05/19/2005 AutoPIPE+6.00 RESULT PAGE 16 ASEE 331.1 (1998) CODE COMPLIANCE (Mcments in ft-lb ) (Stress in psi point Load Ma Xc MM Eq. Load Code Code name combination (Sus.) (occ.) (Exp.) 8.x.r no. type Stress Allow.

130 Ma P ( 3) HOOP 0 18800 OR + Max P 0 1.30 (11) BUST 0 18800 Cold to Tl 31 1.30 (13) DISP 5025 28200

      • Segment A end ***

CaIc. No. M-1 1165-048-1 Revision 00 L rdy* . Project No. 11165-048

-Attachment A

. Page A31 of 34 CONDWIT REBlS 0,/i19/2005 AutoPIPE+6.00 RESVLT PAGE 17 8Y8 5 Z

SUMMARY

Maximum displacements (in)

Max4mm X 14.446 Point : 30 r Load Comb.: TI Maximum Y s -23.000 Point : S Load Comb.: TI Max. totals 23.000 Point I S Load Comb.: Ti Maximum rotations (dog)

Maximum Z 16.365 Point s 30 K Load Comb.s TI Max. totals 16.365 Point s 30 N Load Comb.: TI Maximum restraint forces (lb)

Maximum 147 Point : 90 Load Ccmb.s Ti Maximum Y : -208 Point

  • 30 rF Load Comb.l TI Max. total: 208 Point t 30 r Load Comb.: Ti Maximum restraint moments (ft-lb) axi4u- Z : 62 Point a 5 Load Comb.: Ti Max. total: .62 Point s 5 Load Comb.s Ti
  • l Calc . No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A32 of 34 CONDUIT REBI8 05/19/2005 AutoPIPE+6.00 RESULT PAGE 18 SYSTEXI SuNNARY S Y 8 T Z ---- 8--------a-R-S laximm pipe forces (lb)

Xaxiiuzm z 99 Point s 20 N Load Coub. s Ti Maxiji Yt -175 Point r 20 F Load Ccmb.,t T1 Max. totals 201 Point - 5 Load Caonb.: TiS MSaxi4m pipe ah=ntx (ft-lb)

M3aximua Z t 444 Point s 30 r Load Comnb.s TS Max. totals .444 Point s 30 r Load Ccomb.: TI I

Caic. No. M-1 1165-048-1

,age~

L -: ?rldy",: Revision 00 Project No. 11165-048 Attachment A Page A33 of 34 CONDUIT REBI O%/19/2005 AutoPIPE.6.00 RESULT PACE 19 SYSTEZM SUvMARY Maximum sustained stress Point t 57 Stress psi i2 Allowable psi a 18800 Ratio 2 0.00 Load combination r GR + Max P Maximum displacement stress; Point  : 30 F Stress psi  : 55385 Allowable psi t 47000 Ratio S 1.18 Load combination t Cold to T1

Calc. No. M-11 65-048-1 Revision 00 Project No. 11165-048

.Attachment A Page A34 of 34

---------r-------- -----------------------------------------------.______________

COTDUfS REB:I 05/19/2005 AutoPXPZ+6.00 RESULT PAGE 20 SYSTEM

SUMMARY

Maxizmm sustained stress ratio Point s 57 stress psi t2 Allowable psi 2 18800 Ratio 8 0.00 Load cobination *R + Max P Maximum displacement stress ratio point i 30 F stress psi  : 55385 Allowable psi a 47000 Ratio 2 1.18 Load combination a Cold to TI

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

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

C.s ~
  • ..o .e . Revision 00 Project No. 11165-048 Attachment B Page B1 of 6 I

Attachment B

/

As-Built Information

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

~LAJ1dY.Project No. 11165-048

.Attachment aeB Bf Maean......a..e.To ~ORGE2.TOKARStdbswgeni~nyw.

c~an~si~resnnmco 'rJYESHANTOLIACsarqenimdycm S~~etabdown kifo2u,:i2 DU d 07:54 A.... . ..

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

01.. TE.:

.Teeaetwo,,snubbers bolding .the::*spider jueb!_ support.,under th 7 sinln o

.FedDt RS '2it t7 tiibl E-7Grnl uprsoFgure gidSters 20,Seia 3571.!',(odl I H L302Z' "Stroke =5 -

NOE CW4S ha at Dffrsfro theF .Feld. Data

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

2. . ll Bltsupports haegp~sc ht~oa'clearance ifromto sraeo ot and pipe:]is approx> 3/,"to 0'iie 1/4" NDTotl sde-sidet clearanc betwen ipe ~ and~-Bolt iA,.18to31.

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

.toardkeyay ntrnce. To "prig 'ansHold up tree: strcua channel` to .WhiC'h thei gUide Mubes -are--otd' . .

iSpring Can Data GrZiiel'piqHne'Fur 2Sieo8

' 2Z  ;-:.he'sup~~"jport syste iscS. htteSporchnescudov s iCh asaprx ~1" dowinwid beifor6 ea omtlcnatocr

!.4. ' Btee -hesiderwbsupr i sse andthspigan te c...:'-learance boetween: the fTloor anid :-boto ro fguide. tbs -wvas tmesuired a th Owe St: Ipot'te tube_

botmf n 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 canste tubs sli ighatly in a, horizo..tl Sen 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 Fo SpigCnUBl upports.

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

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

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

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

- ~.Ls

. nngr. s4oios i".' ~ -a Cod ..

back-he.... .

. Calc. No. M-1 1165-048-1 Revision 00 Project No. 11165-048 Attachment B Page B3 of 6

'"cc..'.'.':',t '..'.- C.h.

BotmRo f12 Tubes Cupig ar lcae 4" - 4"after t:':>.',.c '.......... , ....

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

  • Cnw.: a ortField Data rin.aelC t Spr 7,gu F c.tre Theporsuprsytmisuhtathchnescudov41/ .one "of 'the suports),..Size'BOOS',fcfx..'i KillE-B. 'Seria 355045 (Se rialSt takei'fro Two

." Ct" ~

.bofthese'ConstantuSupports hold up0three structural channels

4t 'It4-

'keywayten:

enrnc haltbl ......

  • ~to which the gud 'tubes'.are:U bolt*edc2' d<:ownwrd befor e there is metal .to ata icontacti  :;j: 0;~.:;5 . ,

'.:.8 >: _~o..

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

-;*. '.'t'Tx..he Tangent line frthsbedn is ai+proxinatei rih atth

ssc; :4 -

.'; Sye UDolts ... -R;hi.-,Ihanne>,.,,..u,.d,=v,,

-.<s.;.

Consant, Sport .The bending continues untilfthetubespare vertical ,vhich cscurs;.

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

. .~~ap

<:9--' 'wdef o"e.

e ..', an.;

.C.:

.-..;.,.,....Az thertical. runs directly below q:the key.aytentrance.area i.'x;.w,..,;e 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;':;'.^;

' nce deck' plat enr  :.'cing

.ff.<'", eU.he' T'. second seta offU-Bolts is 10 1/2 b'elow the Keyway,.entrance.,e c 10>l c. TfS here,' is a'second set'.of pipe couplings- they exist in .the c,-h,*.

  • ':vertical rnigt . below
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