Text

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
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

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

-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/ 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

3........................................

3 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

l-ge4LIJctY Calc No. M-1 1165-048-1 Revision 00 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

.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" (average of the two values shown In Reference 7.1.1). The material Is ASTM A213 Type 304 per

'Reference 7.1.3.

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

.1..-

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

-J LLJrIdy w

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

'Revision 00 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

0

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0 000000000 0*

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00 00

00 00000*

0*

00

0 00

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0*0*0 000*0*0

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0*00 00

0 000*0*0 0000000 0*

0*

0 00 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 Software 1600 Riviera Ave., Suite 300 Walnut Creek, CA 94596 I

Sr-gnru L.zu-,cfy Calc. No. M-11165-048-1 Revision 00 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 VERTICAL AXIS AMBIENT TEMPERATURE COMPONENT LIBRARY MATERIAL LIBRARY MODEL REVISION NUMBER

B31.1

Y 70.0 dog I S AUTOPIPI s AUTOB311 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

- - SEGMENT A 5

Run 0

7.83 1S 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 dog 8Si r 1.00 Flex -

1.000 O zlbow, Radius

95.00 inch Bend angle change

22.46 dog Sir 1.00 Flex -

1.000 0 Elbow, Radius -

95.00 inch Bend angle change a 22.46 deg 817 -

1.00 Flex.- 1.000 0 Elbow, Radius -

95.00 inch Bond angle change

22.54 dog 8Si r 1.00 Flex

1.000 2.25 2.94

-2.25

-1.22 40 Run 43 Run

.44 Run

-45 Run 50

. Run

-55 Run 57 Run 58 Run 60 Run 65 Run 67 Run 70 Run 73 Run 75 Run 8S Bend 90 Run 95 Run 100 Run 105 Run 110 Run 115 Run 120 Run 122 Run 2.59 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 1.00 9.00 0

0 0

0.-

0

. 0

.-0 0

0 0

.0 Elbow, Radius - 96.00 £ncb Bend angle change -

90.00 dog 817 -

1.00 Flex -

1.000 0

0 0

11.00 0

2.33 0

2.00 0

2.00

.0 2.46 0

2.38 0

5.00 0

0 0

0 I

I

. I N

t.

2. P.

1.

Caic. No. M-11165-048-1 Revision 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 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 AMEZ X

- - . SECMEN a 5

0.00 LDXNATU(ft

)------ DATA S

Z TYPE DESCRIPTION 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

15 15 F

20 N

20 20 r

25 N 25 25 F 30 N

30 30 1 40

43

44 45 50 55 1

57 58 2

60 1

65 1

67 3

70.

2 73 75 2

0.00 6.82 0.00 0.00 5.24 0.00 TX 0.60 3.79 0.00

.0.62 3.76

.0.00 1.22 2.30 0.00 TX 2.33 1.19 0.00 2.36 1.16 0.00 3.47 0.05 0.00 TX 4.92

-0.55 0.00 4.95

-0.56 0.00 6.41

-1.17 0.00 TX 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 9.00

-1.17 0.00 USRFLS In

1lO0, Out

1.00, Flex -

Automa Override all other values

No 10.00 11.00 12.00 L3.00 L4.00 L5.00 L6.00 L7.00 L8.00 19.00 10.00 11.00 22.00

-1.17 0.00

-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

-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 Override all other values

- No USRFLX In - 1.30, Out - 1.30; Flex a Autoza Override all other values -

No D0 USRFLX In -

1.00, Out -

1.00, Flex -

Automa Override all other values -

No 0.I 0.I 0.t D0 00 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

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 Material 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 1.00 1.00

.V ml.,..

Ldy

Caic. No. M-11165-048-1 Revision 00 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 A L D A T A L I 8 ST IN Material Name 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 1165-048-1 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 NIam Pipe ID rNs 1.

Tmp r. Allow.

dog F pei 70.0 18800.0 70.0 18800.0

'. A,

> >{.* 9

}.,'I

,;.; X

-j.,..

Calc. No. M-11165-048-1 Revision 00 Project No. 11165-048 Attachment A Page All of 34 CONIWST 0/19/2005 REBIS AutoPIPE+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 A

5 0

70.00 130 0

70.00 0.000 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 CA SEZ 1------

POIM NOT NO NAME ALLOW USED USED ALLOW B L ZS (pi )

C A S Z 2------

C A 8 3------

NOT N

NOT NOT ALLOW USZD USED ALLOW USED USED SzG~E~T A 18800*

130 16800*

User-defined code allowable Non-code material

"rg dy.

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

.Attachment A Page A14 of 34 CONDUIT 05/19/2005 REBIS AutoPIPE+6.00 MODEL PACE 13 TSERMAL ANCHOR MOVENE1TS8 AND DISPLACEMENTS POINT DX DY NAME 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

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 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 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 11:27 AM 0.0010 in 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

%':>':>. '.,<.'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-1165-048-1 Revision 00 Project No. 11165-048 Attachment A Page A16 of 34 CONDUIT 05/19/2005 REBIS 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:

-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-1165-048-1 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.........

0.......

040 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

)

name combination X

Y Z

-L ROTATIONS (deog

)

x Y

Z

-*** Segment A 5

GR Ti 15 N

OR Ti S5 r

OR Ti 20 N

GR Ti 20 F

GR Ti 25 N

GR Ti 2S r

CR T1 30 N

GR T1 30 F

GR T1 40 OR Ti 43 GR Ti 44 GR Ti 45 CR T1 50 GR T1 55 GR TI begin ***

0.000 0.000 0.000 0.000 -23.000 0.000 0.000 0.000 0.000 0.062 -23.000 0.000 0.000 0.000 0.000 1.957 -22.506 0.000 0.000 0.000 0.000 1.996 -22.490 0.000 0.000 0.000 0.000 6.993 -1.976 0.000 0.000 0.000 0.000 7.064 -18.904 0.000 0.000 0.000 0.000 12.393 -10.796 0.000 0.000 0.000 0.000 12.437 -10.690

'0.000 0.000

-0.001 0.000 14.446

-0.999 0.000 0.000

-0.001 0.000 14.446 1.409 0.000 0.000

-0;001i 0.000 14.446 3.263 0.000

'0.000

-0.001 0.000 14.446 4.637 0.000 0.000

-0.001 0.;000 14.446 5.575 0.000 0.000

-0.001 0.000 14.446 6.116 0.000 0.000 0.000 0.000

0.000 0.000 0.000 O.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 0.000 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 0.689 0.000 0.000 0.000 5.964 0.000 0.000 0.000 6.037 0.000 0.000 0.000 12.729 0.000 0.000 0.000 12.800 0.000 0.000 0.000 16.359 0.000 0.000 0.000 16.365 0.000 0.000 0.000 12.685 0.000 0.000 0.000 10.063 0.000 0.000 0.000 7.674 0.000 0.000 0.000 5.486 0.000

' 0.000 0.000 3.498 0.000

.0.000 0.000

-1.709 O.'000

-0.001 0.000 0.000 0.000 0.000 0.000 0.000 0.121 14.446 6.304 0.000

. 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 nan.

combbination 57 GR Ti 58 aR T1 60 GR Ti 65 GR Ti 67 GR T1 70 OR T1 73 OR Ti 75 GR Tl 85 N

oR Ti 85 OR T1 90 OR Ti 95 OR Ti 100 OR Ti 105 oR Ti 110 OR Ti 115 GR Ti TRANSLATIONS (in ).

X Y

Z 0.000

-0.001 0.000 14.446 6.181 0.000 0.000

-0.001 0.000 14.446 5.787 0.000 0.000

-0.001 0.000 14.446 5.166 0.000 0.000

-0.001 0.000 14.446 4.359.

0.000 0.000

-0.001 0.000 14.446, 3.408 0.000 0.000

-0.001 0.000 14.445 2.354 0.000 0.000

-0.001 0.000 14.445 1.241 0.000 0.000

-0.001 0.000 14.445 0.109.0.000 0.000 0.000 0.000 14.445 -1.000 0.000 0.000 0'.000 0.000 5.175 0.002 0.000 0.000 0.000

. 0.000 0.000 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 0.000 0.000 0.001 0.000 0.000 0.000 0.000 0.837 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

.0.000 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 0.000 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 0.000 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 0.000 O.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 0.000 9.711 0.000 5.857 0.000 1.549 0.000

-0.881 0.000

-2.145 0.000

-2.102 0.000

-1.279

Cal.

No. M-1 1 165-048-1 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 name comnination 120 GR T1 122 GR T1 123 GR 51 130 GR Ti TR.ASLATIONS (in )

ROTATONS (dog )

X Y

Z S

Z 0.000 0.000 0.000 0.000 0.000 0.000 1.459 0.001 0.000 0.000, 0.000

-0.01O 0.000 0.000 0.000 0.000 0.000 0.000 1.088 0.001 0.000 0.000 0.000 0.619 0.000 0.000 0.382 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 0.000 0.000 0.000 0.000 0.624 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 aR z aC T Z 0 N 8 Point Load name combinatiton 5

zAnchor OR Ti 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

0 TI 0

-208 0

0 0

208 0.-

0 0

0 85 N

V -

Stop GR Ti 90 Guide OR

T1 110 Guide GR TI IlDs 85 0

0 Nil 0

-52 0

0 0

0 52 0

0 0

0 (ID: 90 0

147 EID: 110 0

-52 1i 11 0

0 0

147 0

0 0

O 0

52 0

0 0

0 130 Anchor aR Ti 0

0 0

,0 0

0 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.ORCZ8 cMOMZENTS Point Load FORCZS (lb

)

MOMENTS (ft-lb name coenbination X

Y Z

Result X

S Z

Result se Segment A begin

5 GR Ti 95 15 1N GR Ti 9

1S F GRt 151 R

TI 9!

2011 OR Ti.

9!

207r GR Tl 9!

251

,OR T1 9!

Ti 91 30 r:

OR C

TI 9!

3

.FOR C

TI 9!

30 F+ OR C

TI 9S40-01R T1 99

.43 OR T1 99 44 OR 0

T1 99 45 OR 0

5T 99 D

a 1

-175 3

0 1

-175 0

)

-175 O O..

g

-175 O

0 g

-175 0

9

-175 0

9

-175 P

0 9

-175 I

0 9

-175 1

0 9

33 I.

0 I

33 1

.3 I

0 33 0

33 g 33 0

0 0

201 0

0 e

201 a

0 a

201

a.

0 0

201 o

0 0

201 O

- O 0

201 0

0 0

201 0

0 0

201 0

0 0

201 0

0 0

105 0

0 0

105 o

a o

105 0

0 0

105 o

0 0

105 0

0 0

0*

0 0

0*

0 0

0

-62 62 0

0 0

0

-163 163 0

0 0

-358 358 0

0 0

0

-359 359 0

0 0

0

-313 313 0

0 0

0

-311 311 0

.0 0

0

-32 32 o

o 0

0

-27 27 o

0 0

O

44 444 0

0 0

0 444 444 0

,0 a

0 411 411 0

0 0

0 378 378 0

0 0

0 345 345 0

0 0

0 312 312 50 CR T1 0

0 99 33 0

0 O

105 0

0

.0 0

0 0

279 279

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

.Attachment A Page A24 of 34 CONDUIT 05/19/2005 RZ1IL 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 TI 57 GR T1 0

0 99 33 0

0 0

105 0

0 0

105 0

0 0

246 0

0 0

213 246 0

213 58 aR

0.

0 0

0 TI 99 33 0

105 0

0 0

0 180 180 60 CR Ti 65 GR Tl 67 CR Ti 70 CR Ti 73 CR TS 75 GR Ti 85 N-GR Ti 85 N+

GR Ti 85 F

GR T1 90 GR Ti 90

+

OR Ti 95 GR T1 0

0 99 33 0

0 99

.33 0

0 99 33 0'

0 99 33 0

0 99 85 0

0 99 e5 0

0 99 85 0

0

-48 85 a

a

-48 85 0,

0

.0 105 0

a 0

105 0

0 0

105 0

0 0

105 0

0 0

105 0

0 0

105 0

0 0

105

.0 0

0 131 0

0 0

131 0

0 0

131 0

0 0

98 0

0 0

98 0

0 0

147 0

0.

a 0

0 114 0

0 0

81 0

0 0

0 a

47 0

.0 0

0 0

a 0

14 0

0 0

-19 0

0 0

-52 0

0 0

-52 0

147 0

114 0

81 0

47 0

14 0

19 0

52 0

63 0

361 0

.249 0

0 0

63 0

- - 0 0

0 0

361.

0 0

0 361 0

0 0

249 100 GR TI 0

0 0

0

-48 85 0

98 00 0

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 TI

-48 85 0

98 0

0 56 56 110

-OR 0

0 0

0 Ti

-48 85 0

98 0

0

-62 62 110 0R 0

0 0

0 Ti 4

85 0

0

-62 62 115 OR 0

0 0

0 Ti 4

85 0

0

-52 52 120 GR 0

0 0

0 Ti 4

85 0

as 0

0

-31.

31 122 OR 0

0 0

0 Ti 4

85 0

0

-11 11 123 GR 0

0 0

0 Ti 4

85

0 85 0

0 10 10 130 GR 0

0 0

0 TS 4

85 0

0 31 31

- - Segment A end

%LJiJY.

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

(

Point Load Ma Mb Mo Eq. I name combination (Sus.)

(Occ.)

(Exp.)

B.1.F no. t

- - Segment A begin ***

Stress in psi Load Code type Stress Code ftllo.

5 Mai P aR + Mazx P Cold to TI 15 N-Max P GOR Max P Cold to TI 15 N+ Max P GR + Max P Cold to TS 0

0 0

1S F-Max P GR + Max P 0

Cold to Ti with Sun. load margin 15 I+ Max P GR

Max P 0

Cold to Ti with Sue. load margin 20 N-Max P GR + Max P 0

Cold to Tl with Bus. load margin 20 N+ Max P GR-+ Max P 0

Cold to Ti with Bus. load margin 20 F-Max P GR. + Max P 0

Cold to Ti with sun. load margin 20 r+ max P GR + Max P 0

Cold to Ti with Sus. load margin 25 N-Max P GR + lax P 0

Cold to Ti with Sum. load margin

( 3)

HOOP 1.30 (ll) BUST 62 1.30 (13) DIEP

3)

HOOP 1.00 (Il)

SU8T 163 1.00 (13)

DIsP

( 3).HOOP 1.00 (Il) 8UST 163 1.00 (13).DiSP

( 3)

HOOP 1.00 (11)

SUST 358 1.00 (13) DISP (13)

( 3) HOOP 1.00 (11) BUST

.358 1.00 (13) DISP (13)

( 3) HOOP 1.00 (11) BUST 359 1.00 (13) DISP (13) 1 3) HOOP 1.00 (11)

BUST 359 1.00 (13)

DI8P (13)

13)

HOOP 1.00 (11)

BUST 313 1.00 (13) DISP (13) 1 3) HOOP 1.00 (11)

BUST 313 1.00 (13) DSSP (13)

3) HOOP 1.00 (11)

BUST

311 1.00 (13) DISP (13) 0 1

10062 0

0 20269 0

1 44604 44604 0

1 44707 44707 0

1 38981 38981 0

1 38981

38981 0

1 38728 38728 18800 18800 28200 18800

'18800 28200 18800 18800 28200 18800 18800 28200*4 46999 18800 18800 28200k 46999 18800 18800 28200k 46999 18800 18800 28200**

46999 18800 18800 28200*

46999 18800 18800 28200 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 Point Load Ma Mb Ic Eq. I name combination (Bus.)

(Occ.)

(Exp.)

S.I.F no. t

Stream in p.l

,oad Code type Stress I---

25 N* Max P GR + Maxc P O

Cold to T1 with Bus. load margin

( 3) HOOP 0

1.00 (11)

WUST 1

311 1.00 (13)

DISP 38728 (13) 38728 Code Milow.

18800 18800 28200"*

46999 25 F-max P

¢R + Max P Cold to Ti 2S F+ Sax P OR + Max P Cold to T1 0

0 1 3)

HOOP 1.00 (11)

BUST 32 1.00 (13) DISP

( 3)

HOOP 1.00 (11)

WUST 32 1.00 (13)

DI8P 0

18800 1

18800 3935 28200 0

18800 1

18800 3935 28200 30 N-Max P 6R + Max P Cold to Ti 30 N+ MaX P OR + Max P Cold to Ti 0

( 3) 2 1.00 (11) 27 1.00 (13)

C 3) 1.00 (11) 27 1.00 (13)

HOOP BUST DISP HOOP WUST DIP 0

30

- max P OR + M P

0 Cold to Ti with Bus. load margin 30 F+ Max.P GR + MaxP 0

Cold to T1 with Sus, load margin 40 Max P GR +

ax P 0

Cold to Ti with Bus. load margin 43 Max P GR + Max P 0

Cold to Ti with Sus. load margin 44 Max P GR + MaxP 0

Cold to Ti with Su.

load margin 45 N"

P GR + Max P 0

Cold to T1

( 3) HOOP 1.00 (11)

WUST 444 1.00 (13) DIBP (13)

( 3)

HOOP 1;00 (11)

BUST 444 1.00 (13) DXBP (13)

( 3)

HOOP 1.00 (11) BUST 411 1.00 (13) DISP (13)

( 3)

HOOP 1.00 (11)

BUST 378 1.00 (13) DISP (13) 1 3) HOOP 1.00 (11)

BUST 345 1.00 (13) DISP (13) 1 3)

HOOP 1.30 (11) BUST 312 1.30 (13)

DISP 0

1 3416 0

I 3416 0

0 55385 55385 0

.0 55385 55385 0

1 51216 51216 0

1 47098 47098 0

. 1 42980 42980 0

2 50521 18800 18800 28200 18800 18800 28200 18800 18800 28200**

47000**

18800 18800 28200**

47000**

18800.

18800 28200^^

46999**

18800 18800 28200**

46999**

18800 18800 28200*"

46999 18800 18800 28200"*

fiv.

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

.Attachment A Page A28 of 34 CONDUIT REBIS 05/19/2005 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 Code combination (Bus.)

(occ.)

(zxp.)

8.1.Y no. type Stress Allow.

with Bum.

load margin (13) 50521 46998**

50 Xax P GRxP M0x P O

Cold to Ti with Bus. load margin 55 xax P GR + Max P 0

Cold to TI with Bus.

load margin

( 3)

HOOP 1.00 (11) S8ST 279 1.00 (13) DISP (13) 0 2

34744 34744 18800 18800 28200k*

46998

( 3) 1.00 (11) 246 1.00 (13)

(13)

HOOP SUS DISP:

0 2

30626 30626 0

2 26508 18800 18800 28200k*

46998 18800 18800 28200 57 aIZ P CR + Max P Cold to 5I 58 Max.P CR.+ Max P Cold to TS 60 Max P GR '+ Max P Cold to T1 65 Max P GRi + Max P Cold to Ti 67 Max P GR + Max P Cold to TI 0

1.00 213 1.00

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

( 3) HOOP 1.00 (11) SUBT 180 1.00 (13) DIST

( 3)

HOOP 1.30 (11) BUSU 147 1.30 (13) DISP 0

18800 2

18800 22390 28200 0

0 0

18800 2

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)

HOOP SUS DISP HOOP SUWS DISP 0

2 14155 0

1 10037 18800 18800 28200 18800 18800 28200 70 Max P GR

+ Max P Cold to Ti 73 Maz P GR + Max P Cold to TI C

HOOP SUST DISP HOOP SUBT DISP 0

1 7695 0

1 1801 18800 18800 28200 18800 18800 28200 0

75 Max P GR + Max P Cold to Ti 85 N-Max P GR + Max P Cold to TI 0

( 3) HOOP 1.00 (11) SUST 19 1.00 (13) DISP

( 3) HOOP 1.30 (11) SUST.

52 1.30 (13) DZSP 0

18800 0

18800 2317 28200 0

18800 0

18800 8365 28200 0

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 Point Load Ka Mab Mc EZq.

I name coabination (Sus.)

(Occ.)

(Exp.)

8.1.F no. t

[stress in ]Pi Load Code Y"e Stress 85 N

1Max P.

( 3) HOOP OR + Max P 0

1.30 (11) BUST Cold to TI 52 1.30 (13) DISP 0

0 8365 Code Allow.

18800 18800 28200 85 P-Mxx P GR + Max P Cold to T1 85 F+ Max P OR + Max P Cold to Ti 0

0 90 Max P R + MaxP 0

Cold to Ti with Bus. load margin 95 Max P GR + MaxP 0

Cold to TI with Bus. load margin

' ( 3) HOOP 1.00 (11) OUST 63 1.00 (13) DISP

( 3) HOOP 1.00 (11) BUST 63 1.00 (13) DISP

( 3) HOOP 1.00 (11)

BUST 361 1.00 (13) DISP (13)

( 3)

HOOP 1.30 (11) BUST 249 1.30 (13) DISP (13) 0 0

7878 0

0 7878 0

2 44995 44995 0

1 40301 40301 18800 18800 28200 18800 18800 28200 18800

.18800 28200**

46998 18800 18800 28200**

46999 100 Max P GR + Max P Cold to Ti 105 Max P OR + KaIP Cold to Ti 110

)ax P OR + Max P Cold to Ti 0

0 0

115 Max P GR + Max P Cold.to Ti 120 max P OR + Max P Cold to Ti 122 Max P GR + Max P Cold to Ti 123 Max P CR + Max P Cold to Ti 0

0.

0 0

3) HOOP 1.00 (11)

BUST 152 1.00 (13) DISP

( 3) HOOP 1.00 (11) SUST 56 1.00 (13)

DISP

( 3)

HOOP 1.00 (11)

BUST 62 1.00 (13) DISP

( 3)

HOOP 1.00 (11) 8UST 52 1.00 (13) DISP

3) HOOP 1.00 (11)

BUST 31 1.00 (13) D08P

( 3)

HOOP 1.00 (11)

BUST 11 1.00 (13) DXSP

3)

HOOP 1.00 (11) 8UST 10 1.00 (13) DISP 0

18800 1

18800 19006 28200 0

18800 0

18800 7011 282 00 0

18800 0

18800 7731 28200 0

0 6498 0

0 3907

. 0

.0 1316 0

0 1275 18800 18800 282 00 18800 18800 282 00 18800 18800 28200 18800 18800 28200

%LLY..

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

.Attachment A Page A30 of 34 CONDUIT REBIS 05/19/2005 AutoPIPE+6.00 RESULT PAGE 16 point name 130 Load combination Ma P OR + Max P Cold 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

18800 0

1.30 (11) BUST 0

18800 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 Maximum Y s Max. totals 14.446

-23.000 23.000 Point : 30 Point : S Point I S r

Load Comb.: TI Load Comb.: TI Load Comb.: Ti Maximum rotations (dog)

Maximum Z Max.

totals 16.365 16.365 Point s 30 K Point s 30 N

Load Comb.s TI Load Comb.: TI Maximum restraint forces (lb)

Maximum Maximum Y :

Max. total:

147 Point : 90

-208 Point

30 208 Point t 30 rF r

Load Ccmb.s Ti Load Comb.l TI Load Comb.: Ti Maximum restraint moments (ft-lb) axi4u-Z :

62 Max. total:

.62 Point a 5 Point s 5 Load Comb.: Ti 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 Maxiji Y t Max. totals 99 Point s 20

-175 Point r 20 201 Point -

5 N

F MSaxi4m pipe ah=ntx (ft-lb)

M3aximua Z t 444 Max. totals

.444 Load Coub. s Ti Load Ccmb.,t T1 Load Caonb.: TiS Load Comnb.s TS Load Ccomb.: TI Point s 30 r Point s 30 r

I

,age~

L

-: ?rldy",:

Caic. No. M-1 1165-048-1 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 Stress psi Allowable psi Ratio Load combination t 57 i2 a 18800 2 0.00 r GR + Max P Maximum displacement stress; Point Stress psi Allowable psi Ratio Load combination

30 F

55385 t 47000 S 1.18 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

M axizmm sustained stress ratio Point stress psi Allowable psi Ratio Load cobination s 57 t2 2 18800 8 0.00

R

+ Max P Maximum displacement stress ratio point stress psi Allowable psi Ratio Load combination i 30 F

55385 a 47000 2 1.18 a Cold to TI

*

The system does not satisfy ASZE B31.1 code requirements * *

^

for the selected options

C.s

~

..o

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

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

c~an~si~resnnmco

'rJYESHANTOLIACsarqenimdycm S~~et abdown kifo2u,:i2 DU 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,Seia 3571. !',(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 ifromto 0'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

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v t e Letter Sequence Request
TAC:MC6729, (Approved, Closed)
Initiation Request, Request, Request, Request, Request, Request, Request, Request Acceptance... Administration Questions 15 April 2005 3 June 2005 Answers 1 June 2005 Results Approval, Approval Other: ML051470299, ML060120079, ML060240029, ML060300043, ML060530454
MONTHYEAR2005-06-24 [Table View]

ML051580337

Text

SUMMARY

SUMMARY

1.0 Purpose and Scope

7.0 REFERENCES

SUMMARY

SUMMARY

SUMMARY

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