Calculation 1400287.301, Rev. 0, 'Pilgrim Salt Service Water … · 2014. 4. 9. · ATTACHMENT 9.2...

23
ATTACHMENT 3 TO ENTERGY LETTER 2.14.032 PILGRIM RELIEF REQUEST PRR-25, Rev 1 Calculation Cover Page EC # 49514 Pilgrim Salt Service Water Discharge Piping Elbow (JF29-8-4) Wall Thinning Stress Analysis Structural Integrity Associates Calculation No. 1400287.301, Rev. 0 (22 Pages)

Transcript of Calculation 1400287.301, Rev. 0, 'Pilgrim Salt Service Water … · 2014. 4. 9. · ATTACHMENT 9.2...

  • ATTACHMENT 3

    TO ENTERGY LETTER 2.14.032

    PILGRIM RELIEF REQUEST PRR-25, Rev 1

    Calculation Cover Page EC # 49514

    Pilgrim Salt Service Water Discharge Piping Elbow (JF29-8-4) Wall Thinning Stress

    Analysis

    Structural Integrity Associates Calculation No. 1400287.301, Rev. 0

    (22 Pages)

  • ATTACHMENT 9.2 ENGINEERING CALCULATION COVER PAGE

    Sheet 1 of 2

    [] ANO-1 13 ANO-2 LI GGNS 13 IP-2 13 IP-3 E] PLP

    E7 JAF Z PNPS [] RBS El VY W3

    E[ NP-GGNS-3 E] NP-RBS-3CALCULATION 11) EC # 49514 (2)Page I of 2_22

    COVER PAGE

    (3) Design Basis Calc. Ej YES Z• NO (4) Z• CALCULATION - EC Markup

    Calculation No: M1397 Revision: 0

    (7) Title: Pilgrim Salt Service Water Discharge Piping Elbow (' Editorial(JF29-8-4) Wall Thinning Stress Analysis EL YES Z NO(9) System(s): 29 (10) Review Org (Department):

    (11) Safety Class: (12) Component/Equipment/StructureType/Number:

    Z Safety / Quality Related PIpe/Number:

    PIPE /JF29-8-4

    r- Augmented Quality Program

    LI Non-Safety Related

    (13) Document Type: CALC

    (14) Keywords (Description/Topical

    Codes):

    JF29-8-4, spool, SIA, Structural IntegrityAssociates, flaw, leak, rubber lining,1400287.301, 1400287

    REVIEWS

    (15) Name/Signature/Date (16) Name/Signature/Date (17) Name/Signature/Date

    Structural Integirity Assoc. John A. Tucker;O,• 3-,-ly See IAS

    Responsible Engineer L- Design Verifier Supervisor/ApprovalZ Reviewer__ Comments Attached LI Comments Attached

    EN-DC-126 R005

  • ATTACHMENT 9.3 CALCULATION REFERENCE SHEETSheet 1 of 3

    CALCULATION CALCULATION NO: M1397REFERENCE SHEET REVISION: 0

    I. EC Markups Incorporated (N/A to NP calculations)1.N/A2.3.4.5.I1I. Relationships: Sht Rev Input Output Impact Tracking

    Doc Doc Y/N No.1. Specification M300 2-12 109 x 0 N2. M100-7250 - 5 x [] N3. 0 04. _ _ __5. 11 11

    III. CROSS REFERENCES:

    1.PNPS Dwg M100-72502.ASME Code Case N-513-33.Flow of Fluids Through valves, Fittings and Pipe, Crane Co.., Technical Paper No.

    4104.5.

    IV. SOFTWARE USED:

    Title: ANSYS Mechanical APDL and PrepPost Version/Release: 12.1x64, Nov2009 Disk/CD No. --

    V. DISKJCDS INCLUDED:

    Title: N/A Version/Release Disk/CD No.

    VI. OTHER CHANGES:

    EN-DC-126 R005

  • Structural Integrity Associates, Inc! File No.: 1400287.301Project No.: 1400287

    CALCULATION PACKAGE Quality Program: Z Nuclear E] Commercial

    PROJECT NAME:

    Pilgrim Leaking Elbow Evaluation Support

    CONTRACT NO.:

    10404807, Change Order No. 001

    CLIENT: PLANT:Entergy Nuclear Pilgrim Nuclear Power Station

    CALCULATION TITLE:Pilgrim Salt Service Water Discharge Piping Elbow (JF29-8-4 Spool) Wall Thinning Stress Analysis

    Document Affected Project Manager Preparer(s) &Revision Pages Revision Description Approval Checker(s)

    Signature & Date Signatures & Date

    0 1-16 Initial IssueA-I - A-2B-I - B-2

    Eric Houston Richard BaxEJH 3/3/14 RLB 3/3/14

    Jim WuJW 3/3/14

    Page 1 of 16F0306-01 R1

  • CStructural Integrity Associates, Inc.!

    Table of Contents

    1.0 O B JE C T IV E ........................................................................................................... . . 4

    2.0 TECHNICAL APPROACH ..................................................................................... 4

    3.0 ASSUMPTIONS / DESIGN INPUTS ..................................................................... 4

    4.0 900 ELBOW FINITE ELEMENT MODEL DEVELOPMENT .............................. 4

    4.1 Geometry and Element Selection ............................................................... 4

    4.2 Boundary Conditions ................................................................................... 5

    5.0 RESULTS OF ANALYSIS ..................................................................................... 5

    6.0 REFEREN C E S ........................................................................................................ 6

    APPENDIX A COMPUTER FILES .................................................................................... A-I

    APPENDIX B JF29-8-4 SPOOL UT DATA .................................................................. B-i

    File No.: 1400287.301Revision: 0

    Page 2 of 16

    F0306-OIRI

  • rStructural Integrity Associates, Inc!'

    List of Tables

    Table 1: Membrane Stresses along the Elbow through the Leak Location ........................ 7

    List of Figures

    Figure 1:

    Figure 2:

    Figure 3:

    Figure 4:

    Figure 5:

    Figure 6:

    Figure 7:

    Figure 8:

    Figure 9:

    Photo of U T G rid ................................................................................................. 8

    L eak L ocation ..................................................................................................... . . 9

    Model Geometry, Global View .......................................................................... 10

    Model Geometry, Thinning View ...................................................................... II

    Finite Elem ent M odel ........................................................................................ 12

    Loads and Boundary Condition Application for Global-Z Moment ................... 13

    Total Hoop Stress Results due to [n-Plane (Global-Z) Unit Moment ................. 14

    Total Hoop Stress Results due to Out-of-Plane (Global-Y) Unit Moment ........ 15

    Linearized Path Locations ................................................................................. 16

    File No.: 1400287.301Revision: 0

    Page 3 of 16

    F0306-01 RI

  • rStructural Integrity Associates, Inc.!

    1.0 OBJECTIVEA weeping flaw was identified in a 900 elbow at Pilgrim Nuclear Power Station. The leakage wasidentified in the Salt Service Water system, JF29-8-4 Spool [1]. Structural Integrity Associates (SI) wascontracted to demonstrate the suitability for continued operation of the leaking elbow using methodsconsistent with an upcoming revision of Code Case N-513-3 [2]. The objective of this calculation is todevelop a finite element model of the thinned elbow and determine the local stresses due to appliedbending loads.

    2.0 TECHNICAL APPROACH

    A finite element model (FEM) of the leaking elbow will be developed using the ANSYS finite elementsoftware program [3]. Unit moment loads will then be applied to the model and stresses in the localregion of the leak will be extracted for use in an evaluation of allowable through-wall flaw lengths,which will be documented in a later calculation.

    3.0 ASSUMPTIONS / DESIGN INPUTSThe evaluated local thinning is from Reference [4] and is shown in Appendix B. The grid spacing is0.75 inch [4]. The thinning data point locations for the Reference [4] values are shown in Figure 1.

    Design input for the 900 elbow is taken from Reference [1] unless noted otherwise.

    * Elbow Type: long radius (R) = 1.5.(Nominal Pipe Size) = 27 inches* Outside diameter (OD): 18 inches* Nominal wall thickness (t): Schedule 20 pipe = 0.312 inches [5]* Elbow material: ASTM A-234, Grade WPB.

    4.0 900 ELBOW FINITE ELEMENT MODEL DEVELOPMENTA three-dimensional (3-D) FEM of the 900 elbow is developed with the ANSYS finite element analysissoftware package [3].

    4.1 Geometry and Element Selection

    The three-dimensional finite element model is constructed using ANSYS 8-node SOLID45 structuralsolid elements. The region of ultrasonic (UT) measurement consists of eight (8) axial grid blocks bysixty-one (61) circumferential grid blocks [4]. Reference [4b] indicates that the axial grid is centeredacross the axial position of the leak (see Figure 1). The axial position of the hole, relative to the elbow isprovided in Reference [6] and shown in Figure 2. The remaining elbow region, which was not UTexamined is assumed to have a wall thickness equal to the nominal wall thickness of the pipe,0.312 inch.

    File No.: 1400287.301 Page 4 of 16Revision: 0

    F0306-01 RI

  • jSlructural Integrity Associates, Inc.0

    An additional length of straight pipe is added to either end of the elbow in order to remove boundarycondition end effects from the areas of interest. The wall thicknesses of the additional lengths of pipeare modeled using nominal wall thickness, 0.312 inch.

    The leak location that is shown in Figure 2 is modeled as a square hole that is approximately 0.674inches long axially by 0.464 inches long circumferentially. The elements originally modeled in the holeregion are deactivated via the ANSYS EKILL command. The deactivated elements have near-zerostiffness contribution to the structure. The hole center axially between the Row 4, Column AO andRow 5 Column AO UT data points [4b) (see Appendix B).

    Figure 3 shows a global view of the FEM solid model geometry. Figure 4 shows a view of the thinningin the solid model geometry with a detailed view of the leak region. Figure 5 shows a global view of thefinal finite element model mesh. The ANSYS input files that generate the FEM are listed in Appendix A.

    4.2 Boundary Conditions

    Two separate moment loads are applied to the FEM; an arbitrary unit 10,000 in-lb moment in the plane(moment about the global-z) of the elbow and an arbitrary unit 10,000 in-lb moment out of the plane(moment about the global-y) of the elbow (torsion loading is not evaluated). For the evaluations, oneend of the attached piping is fixed in the axial and circumferential directions, and the CONTA175 andTARGE170 ANSYS elements are used in the application of a pilot node to apply the moment loading tothe other free end of the attached piping. An example of the applied boundary conditions is shown inFigure 6.

    The resulting peak hoop stresses in the elbow are shown in Figures 7 and 8 for the in-plane and out-of-plane moment loads, respectively. The resulting stresses from these moment evaluations will be scaledto the appropriate load combination piping resultant moments in a later calculation. The input files forthe moment evaluation are listed in Appendix A.

    5.0 RESULTS OF ANALYSISLinearized stresses are extracted at each of the grid locations provided in Reference [4] along the axialpath of the elbow and through the leak location as shown in Figure 9. The extracted hoop membranestress due to two moment loads are stored in the Excel spreadsheet, Pilgrim-Results.xlsx, and the resultsare shown in Table 1.

    The input files for the post-processing as well as the output files are listed in Appendix A.

    File No.: 1400287.301 Page 5 of 16Revision: 0

    F0306-OI RI

  • rStructural Integrity Associates, lnc.0

    6.0 REFERENCES

    1. Entergy Drawing No. M100-7250, Rev. E5, "Service Water System, E209N SSW BackwashDrain Piping," SI File No. 1400287.20 1.

    2. ASME Code Case N-513-3, "Evaluation Criteria for Temporary Acceptance of Flaws inModerate Energy Class 2 or 3 Piping Section XI, Division 1," Cases of ASME Boiler andPressure Vessel Code, January 26, 2006.

    3. ANSYS Mechanical APDL and PrepPost, Release 12.1 x64, ANSYS, Inc., November 2009.

    4. Email from John Tucker (Entergy) to Eric Houston (SI), "Subject: FW: JF29-4-8," dated 2/25/14,with attached files, SI File No. 1400287.20 1.

    a) JF29-4-8 spool.JPG

    b) Spool JF29 4 8 012.xls

    5. Flow of Fluids Through Valves, Fittings and Pipe, Crane Co., Technical Paper No. 410, 1976.

    6. Email from Roger Metthe (Entergy) to Eric Houston (SI), "Subject: Pilgrim Hole LocationSketch," dated 2/25/14, with attached file, SI File No. 1400287.201.

    a) Pilgrim Hole Location Sketch.pdf

    File No.: 1400287.301Revision: 0

    Page 6 of 16

    F0306-01 RI

  • $Structural Integrity Associates, Inc."

    Table 1: Membrane Stresses along the Elbow through the Leak Location

    UT Data Thickness Membrane Hoop Stress, psi)Point•° Inches(2) In-Plane (Global-Z) ] Out-of-Plane (Global-Y)Nominal 0.312 16 2

    1, AO 0.352 17 252, AO 0.353 25 213, AO 0.361 21 61

    4, AO(41 0.051 352 1655, AO 4' 0.064 281 526, AO 0.362 21 397, AO 0.343 36 238, AO 0.366 41 42

    Nominal 0.312 16 3NotNotes:

    1) See Figure 9 for layout of UT Data Points and Figure 4 for relative location on the elbow.2) UT data per Reference 4b and nominal thickness for 18 inch, Schedule 20 pipe.3) The unit moment loadings where applied in arbitrary directions and thus the stress reported here

    are in terms of absolute values.4) The modeled hole is centered between these two data points.

    File No.: 1400287.301Revision: 0

    Page 7 of 16

    F0306-01 R1

  • rStructural Integrity Associates, Inc.®

    Figure 1: Photo of UT Grid

    (From Reference 4a)

    File No.: 1400287.301Revision: 0

    Page 8 of 16

    F0306-01 R I

  • VStructural Integrity Associates, Inc!

    ý- ký V4- 1%

    ,ýECV104 t\-N

    Figure 2: Leak Location

    (From Reference 6a)

    File No.: 1400287.301Revision: 0

    Page 9 of 16

    F0306-01 RI

  • rStructural Integrity Associates, Inc!

    VOLUMES

    MAT NUM

    ANFEB 26 2014

    15:26:57KiO NO. 1

    "• ~Region of UT Data

    Figure 3: Model Geometry, Global View

    File No.: 1400287.301Revision: 0

    Page 10 of 16

    F0366-01R I

  • rStructural Integrity Associates, Inc.0

    ANFEB 26 2014

    15:36:55PI/r NO. 1

    11.5 inches~

    Figure 4: Model Geometry, Thinning View

    File No.: 1400287.301Revision: 0

    Page 11 of 16

    F0306-01 R I

  • rStructural Integrity Associates, Inc.!

    PEAL NUM

    ANFEB 26 2014

    16:26:36PLOT NO. 1

    Figure 5: Finite Element Model

    File No.: 1400287.301Revision: 0

    Page 12 of 16

    F0306-01 R I

  • rStructural Integrity Associates, Inc.®

    ANET =S FEB 26 2014

    REAL NUM 16:28:04PLOT NO. 1

    AppliedMoment about

    Global-Z

    Circumferentialand Axial DOF

    Constraints

    Figure 6: Loads and Boundary Condition Application for Global-Z Moment

    File No.: 1400287.301Revision: 0

    Page 13 of 16

    F0306-01 RI

  • rStructural Integrity Associates, Inc.0

    NCDAL SOLUTICTSTEP=-2SUB =1TIME-=2Sz (AVG)RSYS=12

    IX =. 009007SHN =-1169SMX =891.661

    ANFEB 27 2014

    16:33:51PLOT NO. 1

    ------ [Modeled Hole

    -1169 _Tqqs-711.041 -4203-253.126 -418204.789 4376662.704Figre39Totl9oo S4tress Reut uoI-24.16e

    43lba-Z.746Moen 891.661

    Figure 7: Total Hoop Stress Results due to In-Plane (Global-Z) Unit Moment

    (Units are in terms of psi)

    File No.: 1400287.301Revision: 0

    Page 14 of 16

    F0306-OI RI

  • Structural Integrity Associates, Inc.!

    1NUDAL SOLUTICN

    STEP=-1SUB =1TIME=ISZ (AVG)RSYS=12DMX =. 00522SMN =-642.857SMX =658.506

    ANFEB 27 2014

    16:34:16PLOT I)O. 1

    •'-• Modeled Hole

    -642.857 -353.665 -64.474 224.718 513.91-498.261 -209. 069 80. 122 369.314 658.506

    Figure 8: Total Hoop Stress Results due to Out-of-Plane (Global-Y) Unit Moment

    (Units are in terms of psi)

    File No.: 1400287.301Revision: 0

    Page 15 of 16

    F0306-01 RI

  • rStructural Integrity Associates, Inc:

    LDTES

    REAL NUMNomnal: 0.312

    Location (8, AO): 0.366"

    Location (7, AO): 0.343"

    Location (6, AO): 0.362"

    Location (5, AO): 0.064"

    Hole Region Location (4, AO): 0.05 1"

    Location (3, AO): 0.36 1"

    Location (2, AO): 0.353"

    FLocation (1, AO): 0.352"

    N ominal: 0.312"

    FEB 26 201416:44:08

    .=DT NO. 1

    Figure 9: Linearized Path Locations

    File No.: 1400287.301Revision: 0

    Page 16 of 16

    F0306-01 RI

  • Structural Integrity Associates, Inc0

    APPENDIX A

    COMPUTER FILES

    File No.: 1400287.301Revision: 0

    Page A- I of A-2

    F0306-01 RI

  • rStructural Integrity Associates, Inc!

    FILENAME DESCRIPTIONgeom-pil.inp ANSYS input file to generate finite element model.pilgrim.prn ASCI file called by geom-pil.inp containing UT data. Generated in

    Excel spreadsheet Thickness Data.xls.

    load-pil-M.inp ANSYS input file to run two 10,000 in-lb moment evaluations.post-pil-M.inp ANSYS input file to extract linearized stress results for two

    10,000 in-lb moment evaluations.

    Pilgrim-Unit-In.out Output file containing linearized stress results for 10,000 in-lbin-plane moment (about Global-Z) evaluation.

    Pi lgrim-Unit-Out.out Output file containing linearized stress results for 10,000 in-lbout-of-plane moment (about Global-Y) evaluation.

    Thickness Data.xls Excel file with final UT data.Pilgrim-Results.xlsx Compilation of the linearized stress results.

    File No.: 1400287.301Revision: 0

    Page A-2 of A-2

    F0306-01 RI

  • rStructural Integrity Associates, Inc.!

    APPENDIX B

    JF29-8-4 SPOOL UT DATA

    File No.: 1400287.301Revision: 0

    Page B- 1 of B-2

    F0306-01 R1

  • j Slructural Integrity Associates, Inc!

    WKl' e 29 0 rM30

    ýre"man J)a JVA -YJ I L:: F I-At 'Ame-

    'I .. I .T M Er 2 Iicw, mý,.'N J- 00 2 1'--119

    401p LCjjAs3-V! :0000" Ua/ItAr aim w4i YC0 cdI

    RES PW C R ESEWE) ..

    ... .... .

    ~-Iz

    J : .

    U.4UfI. F MIS r JeIcyn minAI21n J ~ ~ rTVI C 3F0 3tId.ti .I :iA'b LII .00-i

    ;vlnh~rm TV1Ii rr m .1 ,i1!YxirnU- V5 Le V0

    vylmi.... ....71 ~

    ----- -- -i

    tR' P 01 F 11 11 IA* N'

    L Loi UJbFj L Jf.b L U I L L/2 J.*- /L J.L tj J.J i I J.- it J.'- U.JFji U.j jý UJO.4 U.J-b

    C 3,18 0 3ý8- C SO ý6 C E73 3.E79 3.E75 3.3117 I.E7E 3.37 M 0.363 0.387 0363 0.338

    K I C 3,111 03,18 C M I.E72 C .74 3.27-- Jý-/7 3.37E IM, D.334 0.361 0.3&1 030 0.32

    C Ktj 0392) C M F9 C z7lý 3DS IM UE 3.ý E 3.33C 0.372 0.387 0366 0.383r "Aq n inA r ,wt; i arR r -7r) I c7F I F7R 1347 1 =FT I 1V n 377 n 37ý miwi n 17?3.332 3.331 0.375 03'3 0.32

    3M 0357 C 3(4 I.H7 C Z78 lz7E IcEl 0.372L Jb4 u lib! L UU) J.- A L ý /5 L A J.U1 JJ Jz: E. L I ljfý U.J.13 U.Jil UJ!" U.J.11

    nlen -- -- -- r- ---- T- -- -- 7- --- -F -ni7 7 7- -n---n.ir, 1 77(3 -7 7c74 I`F73 1.z,= 773 r 7-57 1 Fr i 17 5 1 f775

    ------------- . .-.. -S..... ......... .....

    .... ....... i.... ......... .... .... ...... ..... ..... ....... ........... ...... I . .....

    . i ..7.. •.... . . .. f Fo++ ~ ~ ~ ~ ~ --- ----... .. . i . .. . .. !... . . . . .i ... .. .... . ..... ......... .. . ......... ..... ......... ..... . . . ... . . . ...... . D r t o f F l w i. .. . . . . .......... ....•,.I.

    f '

    U~J:h U:J!J U!JZ. .L.U'. IulAu L4LI I~SL4CL 0.1" J

    S4CC5 C409 C,(113 I.-MI~ 0.107 3), -S I I 2/21 )AIE 0.11i 0A.4I• I : -

    419 34-S~

    Al,--

    A'A A!,

    C 3,18 3U .J9 UJýLt u aumi. UUWU L UI V L JUU LL/I I LrJ4 U.':U L .12/ J., 4 J.JLt J.I -! U.JJ/ J.Jlf

    v), 1 039' 029) 0289 10 38? 3 93 C22 39 C 9I zE C 30 .ElI.Cs am17 ]oI 1.3Y 1E ).3 0.327~ U.320.33 0391 0.381 1 0383 0383 0387 1C 380 C 389 C ME C 11.0 C -1- E.E26 0.327 ).33EnLI1r' n 371 ni3Rm nAn nfAi N.qFk, r ,3 r _C4 r If'. 141 1 17F NU3F "111f.I

    I IFS ZC 3.334 g3.g9 :L1 -W L JW IU.-4U 1.42 J. I J.J-" J.-AgL

    4N1 17 57 . I nt , m n N3R9 r 3FI " rTr r",7-Fr rW3 nfl ;7C r i-fl N .i .; 1 d "1 ;.. nI. ... .!. ..II .t. . . .. ..... .. ,...._ _ I ... .. _ _ _ _ . . .. ... ... .... . . t ... .. _ .. ...

    A'; AW A A" .AC RA" RR =in tP 'F RP R.1 RI- RI

    0.323 033. 0.311 0346 0343 0339 033 C (330 C (8 C 333 0.M2 C 328 3..1it CU 8U.mJi u:rJ; U.J41 ULJ44 U4Ig U j4' UUU L ULLt L 2U L JJ U.:LU L iLLI J.-.I L.'.•0.323 0332 0338 0343 0348 0339 0237 C 327 ( 0225 C 331 0.%6 C 3!6 3.29 U-1-10.3'3 0323 0.333 0344 0343 0339 033' C 336 C (-6 C 331 0.E E6 C 3m6 3. U-10 (19nl',1 n 33.1 0133- N 34,3 N ,r f 4'I r,4" 1 q3.31 -, I- r 3M.' ,- ra-3 6- i r0.323 0333 0.341 0347 0343 0349 0.345 C 333 ( (339 0.043 (346 3.-9 (..40u.J1J ujui u.J4i ULJtU UUUJ UL=4I U14. L U.I L L'b L U44 U.L4U L J'Ii J.L41 L..

    7i ,r =1- nui ' , '35 3 fl3:. 1 5 5 1 r" -.," r %m I..- r u-4, I ,,-i I rv" i,-9 l I, r ci ... . ..... I. ... .......I.. . . . . . . . . . -..... . .......... , . . .... . . . ...... . ... + .. ...

    File No.: 1400287.301Revision: 0

    Page B-2 of B-2

    F0306-01R I