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HomeMy WebLinkAbout021-010-047+atcln he Se d oCs ozi0 o i o. o � � IWashingt PROJECT TITLE • 011 CALCULATION SUMMARY & CONTROL SHEET Page 1 of 2 =D GOOSE EXPANSION CALCULATION SET NO. 1308000-1 PRELIM. FINAL VOID REVISION DISCIPLINE Structural J•O• 24135-001 STRUCTURE OR SYSTEM Compressor DESIGN CLASSIFICATION + SUBJECT Compressor Foundation COMPLETED By Anthony Thomsen DATE 9/18/2002 CHECKED BY EKI C. TlilROc>tS DATE ' 9 ielc APPROVED BY leEx DATE /O • 00 • D SDE OR MGR OF. STAFF GROUP DISTRIBUTION REASON FOR REVISION: TOTAL NUMBER OF SHEETS IN THIS ISSUE ' SHEETS REVISED, ADDED, OR DELETED PROBLEM STATEMENT: Design foundation for compressor SUMMARY CONCLUSIONS: Compressor foundation is adequate OQ�OfESS/p;�y lF 0 �F2 Foundation size 43' -0"x17' -0"x7'-8 7/8" -1 63-D7 ;2- BUTTE. COUNTY sT C/ V1 �P 'jFOFCA'\FORS BUILDING DIVISION �x� rz�s x-30-03 APPROVED P� c5rv., .. , ".1, -� 0APetro-Chem\IP ttruc\wildgoose 2\COVERSHEETS\1308000-1-2.DOC Fv` ` CALCULATION SET NO. Washington CALCULATION SUMMARY 1308000-1 & CONTROL SHEET PRELIM. FINAL VOID REVISION Page 2 of 2 V/ DISCIPLINE Structural PROJECT TITLE WILD GOOSE EXPANSION J•0• 24135-001 DESIGN BASIS: UBC 1997 Seismic zone 3 Foundation information from compressor vendor UNVERIFIED ASSUMPTIONS/OPEN ITEMS: REFERENCES: (SPECIFICATIONS, DRAWINGS, CODES, COMPUTER DATA, FSAR, ETC.) ULATIONS, TEXTS, REPORTS, COMPUTER PROGRAM DISCLOSURE INFORMATION: PROGRAM USED: (NAME) Damf REV. TREV. DATE PROGRAM TYPE RE&. C V�$JFIED S 0 NO ANALYSIS DESCRIPTION RUN NO. RESULT The attached computer output has been reviewed, the input data checked, and the results approved for release.. INPUT CRITERIA BY DATE CHECKED BY DATE %HOZ RUN BY DATE APPROVED BY DATE 0APetro-Chem\IP Struc\wildgoose 2\COVERSHEETS\1308000-1-2.DOC Sheet No. Washington CALCULATION Calculation No. SHEET Project No. PROJECT TITLE )d//1- 24(IJ16, Calc. By Date/ Rev. SUBJECTNEATURE —Vzze�� 0 Checked By D e AZ 421 o 12 j.),4 r4oW aoc- TNI IQ 4V zorl-erf or Im m Sheet No. Washington ALCULATION Calculation No. Z SHEET e00 Project No. PROJECT TITLE it/S/O.c/ Calc. By Date Rev. SUBJECT/FEATUREC�M��� _�S9�t' %D/1�/ DL Checked By rz to 0 a D FirVis,�1 Sheet No. Washington CALCULATION Calculation No. SHEET o Project No. PROJECT TITLE �/�Gl� �DO S� �xf�,�J/✓.S/D/�I !-�S " �d� Calc. By D#/ Rev. SUBJECT/FEATURE COM���S.S�J/� ���� Checked ByDaad�e (� -C rS 9/�'1��� W� /�zNTS , �oi2c�s 3a'�t, o /< E/�/G /�✓� (/.�/,C��G �,�/G � � D,e ��s .fir✓1� /` �O � �l� �✓Ts ) 0Ile C'S Z-wl-IlAle vew Yaez /-/ O eZ ,cr e13 V E,eT 11o1ez //o/ZZ 1::,r zZ3 I� Li Z13 ZS/7_ /.3 a ZZ 700 .3284 / q7S' 4¢ ZO Bea 789 ¢�'.3 �57 2� 900 /4201 S60 7S 3.3 p4 D /45¢ 1� y2 90 qZ Fi0 iF o ;z_ -lo 2 s o �lo���-�✓r's ANG- CCt T 1:-r z 1-3 /-/ O eZ ,cr e13 vle�-/zr 6 //o/ZZ 1::,r zZ3 Ido ZS/7_ /S/z / ZZ goo .3284 / q7S' 017 Zq ©Mi',��sso.�' l�i�r�F�L,q�vGcv /=o,�'c�.s i��✓o 1�foM�-1r5 Sheet No. CALCULATION Washington calculation No. SHEET Project No. PROJECT TITLE �✓/� �� Ct�D Sc' �xP<1c/S/oic/ ' Calc. By SUBJECT/FEATURE G'4i`����s So,�.. f'�i✓ Checked By E -.I DzF s,1G .c/ o"A- ,IA/0 two/� TAzgGc 4 -Z PW4�' 6`9 7 x 43 = /S, ZS40 z- A- I n (IS UO/ Date Rev. Az 3 4a/ a/'1 /,=> Z 3Z79 Sheet No. Washington CALCULATION SHEET calculation No. � o� — Project No. PROJECT TITLE Calc.. By Date Rev. DZ SUBJECT/FEATURE 2/`f/�.f'�SSo�C i-'O�/�1/Dr4l/0La,/ Checked B D e = 4 43X. /7 ' _ / Z, zssl = / f i z (2 f� IA14 /7 M, 4 ( l 3 � y � / Washington PROJECT TITLE CALCULATION SHEET SUBJECT/FEATURE 454/`60.ees SDS /`7'JIV Sheet No. Calculation No. Z— Project No. ,?;41015— Calc. By ` DateL Rev. Checked By ( �' ae R�17 �� Z S/`'/Z/i✓G.. /90D/�/C,�Tio�/S fo,P E��,C��Oiy��/T ��F�cTS Ax = 41- 3sJ9 /Zoc /� i/✓G- ��3 � �T � �x/s /<" CVx = /, 34SO 6. X 2 DG 6 970o = 2eg 536 tl, /S Z 2 7 9 x o o® 9'79'? = �8�sz i 99 1,f4_r- DYNAMIC ANALYSIS OF MACHINE FOUNDATIONS=/`�J,c3� d /1fe /✓r S/`�� /it/G�. Gdi✓STr��i/T$ File Name For Reading Input Data c:\act\rdo File Name For Saving Input Data c:\act\rdo Client WILD GOOSE STORAGE Job No. 24.135-001 Project WILD GOOSE EXP. Subject COMPRESSOR FDN. Analyst A. C. THOMSEN J0 IT -L FT - 'No. Of Foundation Blocks 1 No. Of Equipment Loads 1 Foundation Support.Type_ 0 No. Of Support Springs 0 No..Of Dynamic Load Points 1 No. Of Output Displ. Points 7 Acceleration Of.Gravity 32.20 Unit Weight Of Foundation 0.15 Unit Weight Of Soil 0'.10 Poisson's Ratio Of Soil 0.35 Dynamic Shear Modulus Of,Soil 2600.00 Mat'l Damping Ratio Of Soil 0.05 Geometric Damping Factor 0.50 EQUIPMENT LOCATION AND INERTIA PROPERTIES Equip No. Centroidal Coordinates Weight Moments Of Inertia X Y Z W Ixx Iyy Izz. 1 21.83 8.50 13.07 364 0 0 0 DYNAMIC LOADS FOR FORCING FREQUENCY = 16.670 Cps Point 1 ._-Coordinate 12.50 Y -Coordinate 8.50 .Z -Coordinate 16.66 Fx 0.00 Fy 0.69 Fz 1.24 Mx 0.00 My 5.14 Mz 3.08 Phase Angles Fx 0.00 Fy 0.00 Fz 90.00 Mx 0.00 My 90.00 Mz 0.00 OUTPUT LOCATIONS FOR DYNAMIC DISPLACEMENTS Point No. C o o r d i n a .t e s -X Y Z 1 26.00 8.50 15.63 2 21.83 8.50 15.63 3 12.50 8.50 15.63 4 0.00 0.00 7.74 5 43.00 0.00 7.74 6 0.00 17..00 7.74 7 43.00 17.00 7.74 Weight And Center Of Gravity Of Foundation & Equipment Weight = 1.212691E+03 i Xcg = 2.159905E+01 Ycg = 8.500000E+00 Zcg = 6.631462E+00 l Moments Of Inertia About Centroidal Axes Ixx - 4.623760E+04 Iyy = 1.565952E+05- Izz = 1.512362E+05 Ixy = 0.000000E+00 Iyz _ 0.000000E+00 Izx = 7.733972E+02 Moments Of Inertia About Axes Thru Base Of Foundation Ixx = 9.956725E+04 Iyy = 2.099367E+05 Izz = 1.512481E+05 Soil Springs And Damping In X -Direction Translational Spring = 1.985965E+05 Geometric Damping Ratio = 1.733684E-01 Mat'l Plus Geom. Damping Ratio = 2.233684E-01 Damping Constant = 1.221757E+03 Rocking Spring (About Y Axis) = 8.009789E+07 Geometric Damping Ratio = 1.480105E-01 Mat'l Plus Geom. Damping Ratio = 1.980105E-01 Damping Constant = 2.861837E+05 Soil Springs And Damping In Y -Direction Translational Spring = 1.812251E+05 Geometric Damping Ratio = 1.733684E-01 Mat'l Plus Geom. Damping Ratio = 2.233684E-01 Damping Constant = 1.167100E+03 Rocking Spring (About X Axis) = 2.066972E+07 Geometric Damping Ratio = 4.229983E-02 Mat'l Plus Geom. Damping Ratio = 9.229983E-02 Damping Constant = 4.666900E+04 Soil Springs And Damping In Z -Direction Translational Spring = 2.405364E+05 Geometric Damping Ratio 2.851890E-01 Mat'l Plus Geom. Damping Ratio = 3.351890E-01 Damping Constant 2.017703E+03 Torsion Spring (About Z Axis) 6.775480E+07 Geometric Damping Ratio = 7.936489E-02 Mat'l Plus Geom. Damping Ratio = 1.293649E-01 Damping Constant 1.459599E+05 Natural Frequencies And Mode Shapes Uy Mode Frequency -1.969348E-02 Rx No. (cps) -3.913576.E-0.1 Rz 1 9.024840E+00 2 1.077231E+01 3 1.271915E+01 4 1.911574E+01 5 2.191415E+01 6 2.336028E+01- Mode Shape No. 1 Mode Shape No. 2 Dof Amplitude Dof Amplitude Ux 0.000000E+00 Ux 1.000000E+00 Uy 1.000000E+00 Uy 0.000000E+00 Uz 0.000000E+00 Uz -6.933786E-03 Rx -5.002780E-02 Rx 0.000000E+00 Ry 0.000000E+00 Ry. 1.979052E-02 Rz 3.011925E-04 Rz 0.000000E+00 Mode Shape No. 3, Mode Shape No. 4 Dof Amplitude Dof Amplitude Ux 7.547971E-03 Ux 0.000000E+00 Uy 0.000000E+00 Uy -9.634724E-02 Uz' 1.000000E+00 Uz 0.000000E+00 Rx 0.000000E+00 Rx -1.409046E-02 Ry -2..403331E-04 Ry 0.000000E+00 Rz 0.000000E+00 Rz 1.000000E+00 Mode Shape No. 5 Dof Amplitude Ux 1.000000E+00 Uy 0.000000E+00 Uz -1.969348E-02 Rx 0.000000E+00 Ry -3.913576.E-0.1 Rz 0.000000E+00 Mode Shape No. 6 Dof Amplitude Ux 0.000000E+00 Uy 1..000000E+00 Uz 0.000000E+00 Rx 5.244112E-01 Ry 0.000000E+00 Rz 5.713012E-03 Composite Modal Damping And Resonant Frequencies Mode Composite * * Resonant Frequencies (cps) No. Damping Ratio Const. Ampl.. Rotating Mass 1 1.722515E-01 8.752972E+00. 9.305151E+00 2 2.189835E-01 1.024271E+01. 1.132928E+01 3 3.351787E-01 1.119943E+01 1.444509E+01 4 1.2938.36E-01 1.879302E+01 1.944401E+01 5 2.024058E-01 2.099719E+01 2.287116E+01 6 1.433981E-01 2.287488E+01 2.385598E+01 Dynamic Displacements At System Centroid Dof Amplitude Phase Angle Ux 1.808622E-06 2.812658E+02 Uy 3.717309E-06 1.878184E+02 Uz 4.511213E-06 3.208377E+02 Rx 2.790350E-07 9.050700E+01 Ry 2.884073E-07 3.765821E+01 Rz 1.471802E-07 1.383543E+02 Dynamic Displacements At User Specified Output Points Point No. 1 Dof Amplitude Phase Angle Ux Uy Uz Rx Ry Rz Point No. Dof Ux Uy Uz Rx Ry Rz Point No. Dof Ux Uy Uz Rx Ry Rz Point No. Dof Ux Uy Uz Rx Ry Rz E 3 4 2.415253E-06 4.885193E-06 4.398979E-06 2.790350E-07 2.884073E-07 1.471802E-07 Amplitude 2.415253E-06 4.748638E-06 4.496494E-06 2.790350E-07 2.884073E-07 1.471802E-07 Amplitude 2.415253E-06 4.725949E-06 5.712797E-06 2.790350E-07 2.884073E-07 1.471802E-07 Amplitude 8.161052E-07 3.204962E-06 8.567989E-06 2.790350E-07 2.884073E-07 1.471802E-07 3.555307E+02 2.119627E+02 3.045216E+02 9.050700E+01 3.765821E+01 1.383543E+02 Phase Angle 3.555307E+02 2.190852E+02 3.200113E+02 9.050700E+01 3.765821E+01 1.383543E+02 Phase Angle 3.555307E+02 2.357499E+02 3.474058E+02 9.050700E+01 3.765821E+01 1.383543E+02 Phase Angle 2.462703E+02 2.459822E+02 3.504953E+02 9.050700E+01 3.765821E+01 1.383543E+02 Dynamic Displacements At User Specified Output Points Point No. 5 Dof Amplitude Phase Angle Ux 8.161052E-07 2.462703E+02 Uy 6.167646E-06 1.680399E+02 Uz 9.094917E-06 2.613521E+02 Rx 2..790350E-07 9.050700E+01 Ry 2.884073E-07 3.765821E+01 Rz 1.471802E-07 1.383543E+02 Point No. 6 Dof Amplitude Phase Angle Ux 2.860533E-06 3.026029E+02 Uy 3.204962E-06 2.459822E+02 Uz 9.043264E-06 2.159690E+01 Rx 2:7.90350E-07 9.0.50700E+01 Ry 2.884073E-07 3.765821E+01 Rz 1.471802E-07 1.383543E+02 Point No. 7 Dof Amplitude Phase Angle Ux 2.860533E-06 3.026029E+02 Uy 6.167646E-06 1.680399E+02 Uz 4.475838E=06 2.516444E+02 Rx 2.790350E-07 9.050700E+01 Ry 2.884073E-07 3.765821E+01 -Rz 1.471802E707 1.383543E+02 t Nx L DYNAMIC ANALYSIS OF MACHINE FOUNDATIONS File Name For Reading Input Data c:\act\rdl File Name For Saving Input Data c:\act\rdl,. Client WILD GOOSE STORAGE Job No. 24135-001 Project, WILD GOOSE EXP, Subject COMPRESSOR FDN. Analyst A. C. THOMSEN No. Of Foundation Blocks 1 No. Of Equipment Loads 1 Foundation Support Type,- 1 No. Of Support Springs - 1 No. Of Dynamic Load Points 1 No. Of Output Displ. Points 7 Acceleration Of Gravity 32.20 Unit Weight Of Foundation 0.15 FOUNDATION BLOCK DIMENSIONS Block No. C o o r ds O f C o r n e r S i d e L .e n g t h e X Y Z. Lx Ly Lz 1 0.00 0.00 0.00 43.00 17.00 7.74 EQUIPMENT LOCATION AND INERTIA PROPERTIES veuip No. 'Centroidal Coordinates Weight Moments Of Inertia X Y Z W Ixx Iyy I<z�z . 1 0 21'. 8.3 8 .50 13.07 364 0 0 :_ :: USER INPUT STIFFNESS (K) AND DAMPING (C) VALUES Point 1 ..-Coordinate 21.50 Y -Coordinate 8.50 Z -Coordinate 0.00 Kx 263538 Ky 240486 Kz 274,356 Krx 28536615 Kry 98352199 Krz 67754800 Kxry 0 Kyrx 0 Cx 1222 . Cy 1167 Cz 2018 Crx 46670 Cry 286184 Crz 145960" Cxry ' 0 Cyrx 0 DYNAMIC LOADS FOR FORCING FREQUENCY = 16.670 Cps Point 1 ..-Coordinate 12.50 . Y -Coordinate 8.50 Z -Coordinate 16.66 Fx 0.00 Fy 0.69 Fz 1.24 Mx 0.00 My 5.14 Mz 3.08 Phase Angles Fx 0.00 Fy. 0.00 Fz 90.00 Mx 0.00 My 90.00 Mz 0.00 OUTPUT LOCATIONS FOR DYNAMIC DISPLACEMENTS Point No. C o o r d i n a t e s X Y z 1 26.00 8.50, 15.63 2 '21.83 8.50 15.63 3 12.50 8.50 15.63 4 0.00 0.00 7.74 5 43.00 0.00 7.74 6 0.00 17.00 7.74 7 .43.00 17.00 7.74 Weight -And Center Of Gravity Of Foundation &Equipment Weight = 1.212691E+03 Xcg = 2.159905E+01 Ycg = 8.500000E+00 zcg 6.631462E+00 Moments Of Inertia About Centroidal Axes Ixx = 4.623760E+04 Iyy = 1.565952E+05 Izz 1.512362E+05 Ixy = O.000000E+00 Iyz = 0.000000E+0.0 Izx = 7.733972E+02 Natural Frequencies And Mode Shapes Mode Frequency No. (cps) 1 1.047539E+01 2 1.232158E+01 3 1.358403E+01 4 1.911628E+01 /. /S 5 2.445573E+01 6 2.723986E+01 Mode Shape No. 1 Mode Shape No. 2 Dof Amplitude Dof Amplitude.. Ux 0.000000E+00 Ux 1.000000E+00 Uy 1.000000E+00 Uy 0.000000E+00 Uz 0.000000E+00 Uz -1.209053E-02 Rx -4.848502E-02 Rx 0.000000E+00 Ry 0.000000E+00 Ry 2.163440E-02 Rz 4.473015E-04 Rz 0.000000E+00 Mode Shape No. 3 Mode Shape No. 4 Dof Amplitude Dof Amplitude Ux 1.230324E-02 Ux 0.000000E+00 Uy 0.000000E+00 Uy -9.105917E-02 Uz 1.000000E+00 Uz 0.000000E+00 Rx 0.000000E+00 Rx -2.354978E-03 Ry -7:613968E-05 Ry 0.000000E+00 Rz 0.000000E+00 Rz 1.000000E+00 Mode Shape No. 5 Mode Shape No. 6 Dof Amplitude Dof Amplitude Ux 1.000000E+00 Ux 0.000000E+.00 Uy 0.000000E+00 Uy 1.000000E+00 Uz -1.582329E-02 Uz 0.000000E+00 Rx 0.000000E+00 Rx 5.410365E-01 Ry -3.580222E-01 Ry 0..000000E+00 Rz 0.000000E+00 Rz 3.886426E-03 Dynamic Displacements At System Centroid Dof Amplitude, Phase Angle Ux 2.071095E-06 2.925722E+02 Uy 4.074673E-06 1.933421E+02 Uz 4.875361E-06 3.267425E+02 Rx 1.914891E-07 8.238561E+01 Ry 2.099003E-07 4.612377E+01 Rz 1.480193E-07 1.382456E+02 Dynamic Displacements At User Specified Output Points Point No. 1 Dof Amplitude Phase Angle . Ux 2.175043E-06 3.453275E+02 Uy 5.176535E-06 2.053266E+02 Uz 4.791939E-06' 3.158205E+02 Rx _ 1.914891E-07 8.238561E+01 Ry 2.099003E-07 .4.612377E+01 Rz 1.480193E-07. 1.382456E+02 Point No. 2 Dof Amplitude Phase Angle Ux 2.175043E-06 3.453275E+02 Uy 4.968794E-06 2.118966E+02 Uz 4.866661E-06. 3.261815E+02 Rx 1.914891E-07 8.238561E+01 Ry 2.099003E-07 4.612377E+01 Rz 1.480193E-07 1.382456E+02 Point No. 3 4::�r A14, SI4AF% C Dof, Amplitude Phase Angle Ux 2.175043E-06 3.453275E+02 Uy 4.767914E-06 2.280337E+02 Uz 5.55'4143E-06, 3.464963E+02 Rx 1.914891E-07_ 8.238561E+01 Ry 2.099003E-07 4.612377E+01 Rz 1.480193E-07 1.382456E+02 Point No. 4 Dof Amplitude Phase Angle Ux 9.070265E-07 2.711156E+02 Uy 3.652632E-06 2.438851E+02 Uz 7.077191E-06 3.517221E+02 Rx 1.914891E-07 8.238561E+01 Ry 2.099003E-07 4.612377E+01 Rz 1.480193E-07 1.382456E+02 Dynamic Displacements At User Specified Output Points Point No 5 Dof Amplitude Phase Angle. Ux 9.070265E-07 2.711156E+02 Uy 6.427903E-06 1.714212E+02 Uz 7.562079E-06 2.756745E+02 Rx 1.914891E-07 8.238561E+01 Ry 2.099003E-07 4.612377E+01 Rz 1.480193E-07 1.382456E+02 Point No. 6 Dof Amplitude Phase Angle Ux 3.203151E-06 3.062678E+02 Uy 3.652632E-06 2.438851E+02 Uz 7.755649E-06 1.653811E+01 Rx 1.914891E=07 8.238561E+01 Ry 2.099003E-07 ' 4.612377E+01 Rz 1.480193E-07 1.382456E+02 Point No. 7 Dof Amplitude. Ux 3.203151E-06 Uy 6.427903E-06 Uz .4.457188E-06 Rx 1.914891E-07 Ry 2.099003E-07 Rz 1.480193E-07 Phase Angle 3.062678E+02 1.7.14212E+02 2.853390E+02 8.238561E+01 4.612377E+01 1.382456E+02 Washington CALCULATION SHEET PROJECT TITLE W11- D L2,2 O 64 EX SUBJECTNEATURE /?ES' t lz- /OdD 1,epr% CJy = ;po0oo5. /.7G.5.3�fT Calculation No. o - P oject No. Calc. By Rev. D Checked By Da e �J (S I w ),7 .D0000s�7Gs� X/Z = 0000��/Zi.�./ /�Mf'G/r�o�t ,04900oS)149s-3 S ui AGT'o� Z, o I./L G OG/T / ZX• �� GS4 � = D/gyp ��"/.��� �G Uz =. BD0007755G5" x DODO 9 3 Z /.c/ Ovc'/�s/G- SG=�vic � G'o�tivirio,c/ i�v�f=�lo�' zea /�� /� Soi�/�G G ,(.j�i�EG � /✓4T/CC �.CYG GG O/G /A14G AIUAI DYNAMIC ANALYSIS OF MACHINE FOUNDATIONS File Name For Reading Input Data c:\act\rd2 File Name For Saving Input Data c:\act\rd2 C �► �`'� E 1 c� `q f I�/� Client WILD GOOSE STORAGE Job No. 24135-001 :Project WILD GOOSE EXP. •Subject COMPRESSOR FDN. Analyst A. C. THOMSEN No. Of Foundation Blocks 1 No. Of Equipment Loads 1 Foundation Support Type 1 No. Of Support Springs 1 No. Of Dynamic Load Points 1 No. Of Output Displ. Points 7 Acceleration Of Gravity 32.20 Unit Weight Of Foundation 0.15 i FOUNDATION BLOCK DIMENSIONS Block No. C o o r d s 0 f C o r n_ e r S, i de L e n g t h e X Y z Lx Ly Lz 1 0.00 0.00 0.00 43.00 17.00 7.74 EQUIPMENT LOCATION AND-.INERTIA.PROPERTIES Equip No. Centroidal Coordinates Weight Moments Of Inertia X Y z W Ixx. Iyy Izz 1 21.83 8.50 13.07 364 0 0 0 USER.INPUT STIFFNESS (K) AND DAMPING (C) VALUES Point 1. &-Coordinate 21.50 Y -Coordinate 8.50 Z -Coordinate 0..00 Kx 263538 Ky 240486 Kz 274356 Krx 28536615 Kry 98352199 Krz 67754800 Kxry 0 Kyrx 0 Cx 1222 Cy 1167 Cz 20.18 Crx 46670 Cry 286184 Crz 145960 Cxry . 0 Cyrx 0 DYNAMIC LOADS FOR FORCING FREQUENCY _ 15.000 Cps Point. 1 k -Coordinate:' 12.50 Y -Coordinate 8.50 Z -Coordinate 16.66 - Fx 0.00 Fy, 0.56 Fz 1.00 Mx 0.00 My 4.16 Mz 2.50 Phase Angles Fx 0.00 Fy 0.00 Fz 90.00 Mx 0.00 My 90.00 Mz 0.00 OUTPUT LOCATIONS FOR DYNAMIC DISPLACEMENTS ,Point No. C o o .r d i n,a t e s X Y Z 1 26.00 8.50 15.63 - 2 21.83 8.50 15.63 3 12.50 8.50 15.63 ' 4 0.00 0.00 7.74 ' 5 43.00 '0.00 7.74 6 0.00 17.00 7.74 7 43.00 17.00 7.74 Weight And Center Of Gravity Of Foundation & Equipment Weight 1.212691E+03 Xcg = 2.159905E+01 Ycg = 8.500000E+00 Zcg = 6.631462E+00 Moments Of Inertia About Centroidal Axes Ixx 4.623760E+04 Iyy = 1.565952E+05 I Izz = 1..512362E+05 Ixy = 0.000000E+00 Iyz = 0.000000E+00 Izx = 7.733972E+02 Natural Frequencies And Mode Shapes Mode Frequency No. (cps) 1 1.047539E+01 2 1.232158E+01 3 1.358403E+01 .9 4 1.911628E+01 / , Z7 5 2.445573E+01 .6 2.723986E+01 Mode Shape No. 1 Mode Shape No. .2 Dof Amplitude Dof Amplitude Ux 0.000000E+00 Ux 1.000000E+00 Uy 1.000000E+0.0 Uy 0.000000E+00 Uz 0.000000E+00 Uz -1.209053E-02 Rx -4.848502E-02 Rx 0.000000E+00 Ry 0.000000E+00 Ry 2.163440E-02 Rz 4.473015E-04 Rz 0.000000E+00 Mode Shape No., 3 Mode Shape No.. 4 Dof Amplitude Dof- Amplitude Ux 1.230324E-02 Ux 0.000000E+00 Uy 0.000000E+00 Uy -9.105917E-02 Uz 1.000000E+00 Uz O.000000E+00 Rx 0.000000E+00 Rx -2.354978E-03 Ry -7.613968E-05 Ry 0.000000E+00 Rz 0.000000E+00 Rz 1.000000E+00 Mode Shape No. 5 Mode Shape No. 6 Dof Amplitude Dof Amplitude Ux 1.000000E+00 Ux 0.000000E+00 Uy 0.000000E+00 Uy 1.000000E+00 Uz -1.582329E-02 Uz 0.000000E+00 Rx 0:000000E+00 Rx 5.410365E-01 Ry -3.580222E-01 Ry 0.000000E+00 Rz 0.000000E+00 Rz 3.886426E-03 Dynamic Displacements At System Centroid Dof Amplitude Phase Angle Ux 2.241857E-06 3.084160E+02 Uy 4.60519.2E-06 1.983091E+02 Uz 4.98687.3E-06 3.424895E+02 Rx 1.967951E-07 6.753027E+01 Ry 1.590301E-07 4.646021E+01 Rz 9.177213E-08 1.539882E+02 Dynamic Displacements At User Specified Output Points Point No. 1 Dof Amplitude Phase Angle Ux 2.485137E-06 3.431783E+02 Uy 6.142708E-06* 2.082344E+02 Uz 4.721812E-06 3.348355E+02 Rx 1.967951E-07 6.753027E+01 Ry 1.590301E-07 4.646021E+01 Rz 9.177213E-08 1.539882E+02 Point No. 2 Dof Amplitude Phase Angle Ux 2.4.85137E-06 3.431783E+02 Uy 5.927243E-06 2.112378E+02 Uz 4.970866E-06 3:421091E+02 Rx 1.967951E-07 .6.753027E+01 Ry 1.590301E-07 4.646021E+01 Rz 9.177213E-08 1.539882E+02 Point No. 3 Dof Ux Uy Uz Rx Ry Rz Point No. 4 Dof Ux Uy Uz Rx Ry Rz. Amplitude 2.485137E-06 5.511286E-06 5.770275E-06 1.967951E-07 1.590301E-07 9.177213E-08 Amplitude 1.522199E-06 3.672692E=06 6.506451E-06 1.967951E-07 1.590301E-07 9.177213E-08 Phase Angle 3.431783E+02 2.187458E+02 3.555121E+02 6.753027E+01 4.646021E+01 1.539882E+02 Phase Angle 3.023009E+02 2.232739E+02 3.550954E+02 6.753027E+01 4.646021E+01 1.539882E+02 Dynamic Displacements At User Specified Output Points Point No. 5 Dof Amplitude Phase Angle Ux 1.522199E-06 -3.023009E+02 Uy 6.270080E--06 1.872101E+02 Uz 5.791099E-06 2.878177E+02 Rx 1.967951E-07 6.753027E+01 Ry 1.590301E-07 4.646021E+01 Rz 9.177213E-08 1.539882E+02 Point No. 6 Dof Amplitude Phase Angle Ux 2.965246E-06 3.183446E+02 Uy 3.672692E-06 2.232739E+02 Uz 8.164851E-06 1.808986E+01 Rx 1.967951E-07 6.753027E+01 Ry- 1.590301E-07 4.646021E+01 Rz 9.177213E-08 1.539882E+02 Point No. 7 Dof Amplitude Phase Angle Ux 2.965246E-06 3.183446E+02 Uy 6.270080E-06 1.872101E+02 Uz 3.895074E-06 3.215553E+02 Rx 1.967951E-07 6.753027E+01 Ry 1.590301E-07 4.646021E+01 Rz 9.177213E-08 1.539882E+02- Sheet No. Washington CALCULATION calculation No 8 SHEET / p oGto Project No. PROJECT TITLE W�G1� �floSC �X��I�✓Sioi�/ Calc. By D Rev. SUBJECT/FEATURE CD��i,c' L".SSD' `1�/✓/1 �Z Checked By Da C) r --AK q 7/0Z l/v 0A 84D �E'iv/�'I DYNAMIC ANALYSIS OF MACHINE FOUNDATIONS File Name For Reading Input Data c:\act\rd3 File Name For Saving Input Data c:\act\rd3 Client WILD GOOSE STORAGE Job No. 24135-001 Project. WILD GOOSE EXP. Subject COMPRESSOR FDN. Analyst A. C. THOMSEN No. Of Foundation Blocks 1 No. Of Equipment Loads 1 Foundation Support Type 1 No. Of Support Springs 1 No. Of Dynamic Load Points 1 No. Of Output Displ. Points 7 Acceleration Of Gravity 32.20 Unit Weight Of Foundation 0.15 USER INPUT STIFFNESS (K)'AND DAMPING (C) VALUES Point 1 -a-Coordinate 21.50 Y -Coordinate 8.50 Z -Coordinate 0.00 Kx 263538 Ky 240486. Kz 274356 Krx 28536615 Kry 98352199 Krz 67754800 Kxry 0 Kyrx 0 Cx 122-2 Cy 1167 Cz 2018 Crx 4667.0 : Cry 286184 Crz 145960 Cxry 0 Cyrx 0 DYNAMIC LOADS FOR FORCING FREQUENCY =" 13.330 Cps Point 1 :&-Coordinate 12.50 Y -Coordinate 8.50 " Z -Coordinate 16.66 FX 0.00 Fy 0.00 Fz 0.79 Mx 0.00 My 3.28 Mz 1.98 Phase Angles Fx 0.00 Fy 0.00 Fz 90.00 . Mx 0.00 . My 90.00 Mz 0.00 OUTPUT LOCATIONS FOR DYNAMIC DISPLACEMENTS _ Point No. C o o r d i n a t e" s X Y Z 1 26.00 8.50 15.63 2 21.83 8.50 15.63' 3 12.50 8:50 15.63 4 0.00 0.00 7.74 5 43.00 0.00 7'.74 6 0.00 17.00 7.74 7 43.00 17.00 7.74 Weight And Center Of.Gravity Of Foundation & Equipment Weight = 1.212691E+03 Xcg 2.159905E+01 Ycg 8.500000E+00 Zcg = 6.631462E+00 Moments Of Inertia About Centroidal.Axes Ixx 4.623760E+04 Iyy = 1.565952E+05 Izz = 1.512362E+05 Ixy = 0.000'O00E+00 Iyz = 0.000000E+00 Izx = 7.733972E+02 Natural Frequencies And.Mode Shapes Mode Frequency 1.000000E+00 No. (cps) Rx 1 1.047539E+01 0.000000E+00 2 3 1.232158E+01 1.358403E+01 A r 13,.33 - 4 1.911628E+01 5 2.445573E+01 6 2.723986E+01 Mode Shape No. 1 Dof Amplitude Ux 0.000000E+00 Uy 1.000000E+00 Uz 0.000000E+00 Rx -4.848502E-02 Ry 0.000000E+00 Rz 4.473015E-04 Mode Shape No. 3 Dof Amplitude Ux 1.230324E-02 Uy 0.000000E+00 Uz 1.000000E+00 4 Rx 0.000000E+00 Ry -7.613968E-05 Rz 0.000000E+00 Mode Shape No. 5 Dof Amplitude Ux 1.000000E+00 Uy 0.000000E+00 Uz -1.582329E-02 Rx 0.000000E+00 Ry -3.580222E-01 Rz 0.000000E+00 Mode Shape No. 2 Dof Amplitude Ux 1.000000E+00-% Uy 0.000000E+00 Uz -1.209053E-02 Rx 0.000000E+00 Ry2.163440E-02 1.000000E+00 Rz 0.000000E+00 Mode Shape No. 4 Dof Amplitude Ux 0.000000E+00 Uy -9.105917E-02 Uz .0.000000E+00 Rx -2.354978E-03 Ry 0.000000E+00 Rz 1.000000E+00 Mode Shape No. 6 Dof Amplitude Ux 0.000000E+00 Uy 1.000000E+00 Uz 0.000000E+00 Rx 5.410365E-01 Ry 0.000000E+00 Rz 3.886426E-03 Dynamic Displacements At System Centroid Dof Amplitude Phase Angle Ux 2..519140E-06 3.359132E+02 Uy 1.131125E-08 1.993120E+02 Uz 4.640419E-06 3.516185E+00 Rx 7.392938E-10 3.124167E+01 Ry 1.375260E-07 4.505316E+01 Rz 5.365993E-08 3.406433E+02 Dynamic Displacements At User Specified Output Points Point No. 1 Dof Amplitude Phase Angle Ux 3.177698E-06 3.572541E+02 Uy 2.234340E-07 3.375113E+02 Uz 3.580414E+02 Rx 114.206566E-06 7.392938E-10 3.124167E+01 Ry 1.375260E-07 4.505316E+01 Rz 5.365993E-08 3.40643.3E+02 Point No. 2 Dof Amplitude Phase Angle Ux .3.177698E-06 3..5725.41E+02 Uy 1.222590E-08 2.475412E+02 Uz 4.616693E-06 3.254805E+00 Rx 7.392938E-10 3.124167E+01 Ry 1.375260E-07 4.505316E+01 Rz 5.365993E-08 3.406433E+02 Point No. 3 Dof Ux Uy Uz. Rx Ry Rz Point No. 4 Dof Ux Uy Uz Rx Ry Rz Amplitude 3.177698E-06 5.014573E-07 5.638485E-06 7.392938E-10 1.375260E-07 5.365993E-08 Amplitude 3.033332E-06 1.168381E-06 7.134747E-06 7.392938E-10 1.375260E-07 5.365993E-08 .Phase Angle 3.572541E+02 1.620383E+02 1.197876E+01 3.124167E+01 4.505316E+01 3.406433E+02 Phase Angle 3.393165E+02 1.610210E+02 1.951766E+01 3.124167E+01 4.505316E+01 3.406433E+02 Dynamic Displacements At User Specified�Output Points Point No. 5 Dof Amplitude Phase Angle Ux 3.033332E-06 3.393165E+02 Uy 1.139048E-06 3.402560E+02 tiz 3.119928E-06 3.247256E+02' Rx 7.392938E-10. 3:124167E+01 Ry 1.375260E-07 4.505316E+01 Rz 5.365993E-'08 3.406433E+02 Point No. 6 Dof Amplitude Phase Angle Ux 2.121463E-06 3.387461E+02 Uy 1.168381E-06 1.610210E+02 Uz 7.147053E-06 1.953814E+01 .Rx 7.392938E-10 3.124167E+01 Ry 1.375260E-07 4.505316E+01 Rz 5.365993E-0.8" 3..406433E+02 Point No. 7 Dof Amplitude Phase Angle Ux 2.121463E-06 3.387461E+02 Uy 1.139048E-06 3.402560E+02 Uz 3.124958E-06 3.249369E+02. Rx 7.392938E-10 3.124167E+01 Ry 1.375260E-07 4.505316E+01 Rz 5.365993E=08 3.406433E+02 Sheet No. CALCULATION CAL Washington SHEET Calculation No. Project No. PROJECT TITLE_W IL V �� sE &::K Calc. By SUBJECT/FEATURE e5S6�ft DA/zo Checked By TS CO, C'o11flile E55 a.cP 6' 6z IAv A -,0491 Date Rev. e-711MOZ Dat "t%1`7IDZ ��`�!'� iTvv� , ocx��o�2��SG �r _ , oo aooSoS/.✓ V6� Z 2784 /�If�G /TV�Gr = D�DIOb //✓ 4r ,5,r,4A r �iJ 70� �2f'M DYNAMIC ANALYSIS OF-.MACHINE FOUNDATIONS File Name For Reading Input Data c:\act\rd4 File Name For Saving Input Data.. c:\act\rd4 CN►c.��� c.1�� 9IM(�� Client WILD GOOSE STORAGE Job No., 24135-001 Project WILD GOOSE EXP.. Subject COMPRESSOR FDN. Analyst A. C. THOMSEN No. Of Foundation Blocks 1 No. Of Equipment Loads 1 Foundation Support Type 1 No. Of Support Springs 1 No. Of Dynamic Load Points 1 No. Of Output Displ. Points 7 Acceleration Of Gravity 32.20 Unit Weight Of Foundation 0.15 EQUIPMENT LOCATION AND.INERTIA PROPERTIES ' Equip No. Centroidal Coordinates Weight Moments Of Inertia X Y z W Ixx Iyy Izz 1 21.83 8.50 13'.07 364 0 0 0 USER. INPUT STIFFNESS (K) AND DAMPING (C) VALUES Point 1 &-Coordinate 21.50 Y -Coordinate 8.50 Z -Coordinate 0.00 Kx 263538 Ky 240486 Kz 274356 Krx 28536615 Kry _ 98352199 Krz 67754800 Kxry 0 Kyrx 0 Cx 1222 .Cy 1167 Cz 2018 Crx 46670 Cry 286184 Crz 145960 Cxry 0 , Cyrx 0 tL'L 00'LT 00'U, L T7L'L 00' LT 00'0 9 fL'L 00'0 00'£% S fL'L_ 00'0 00'0 t £9'ST O9'8 OS'ZT £ £9'ST OS'8 £8'TZ Z £9'ST OS'8 00'9Z T Z X s a e u i p a. o O O -ON 4uiod SSdQaWaDVgdSIQ OiwvxAQ uoa SNOIIVDOq SndInO 00'0 zw 00'06 AN 00'0 X 00'06 z 00' 0 ,fid. 00'0 Xd saTBUV 9s2tid TS'T Z14 Z S ' Z 0 0 ' 0 XN 09'0 zd V£' 0 Ad 00'0 Xd 99' 9T agsuipa003-Z OS' 8 . a-41euipaOOD-x OS' ZT ageuipaOOo-- T :tuiod sd0 OL9'TT = XoNanosud fmio iod HOd SCIVOU 0'IXVN7La Weight And Center Of Gravity Of Foundation & Equipment Weight = 1.212691E+03 Xcg = 2.159905E+01 Ycg _ 8.50000"0E+00 Zcg = 6.631462E+00 Moments Of Inertia About Centroidal Axes Ixx = 4.623760E+04 Iyy = 1.565952E+05. Izz = 1.512362E+05 Ixy = .0.000000E+00 -Iyz = O.O000OOE+00 Izx 7.733972E+02 Natural Frequencies And Mode Shapes Mode Frequency No. (cps) 1 1.047539E+01 2 1. 232158E+01 -/,,O 3 1.358403E+01 4 1.911628E+01 5 2.445573E+01 6 2.723986E+01 Mode Shape No. 1 Dof Amplitude Ux 0.000000E+00 Uy 1.000000E+00 �- Uz 0.000000E+00 Rx -4.848502E-02 Ry 0.000000E+00 Rz 4.473015E-04 Mode Shape No. 3 Dof Amplitude Ux 1.230324E-02 Uy 0.000000E+00 Uz 1.000000E+00 Rx 0.000000E+00 Ry -7.613968E-05 Rz 0.000000E+00 Mode Shape No. 5 Dof Amplitude Ux 1.000000E+00 Uy 0.000000E+00 Uz -1.582329E-02 Rx. 0.00`0000E+00 Ry -3.580222E-01 Rz 0.000000E+00 Mode Shape No. 2 Dof Amplitude Ux 1.000000E+00 -1 -- Uy 0.000000E+00 Uz -1.209053E-02 Rx 0.000000E+00 Ry 2.163440E-02 Rz 0.000000E+00 Mode .Shape No. 4 Dof Amplitude Ux 0.000000E+00 Uy -9.105917E-02 Uz 0.000000E+00 Rx -2.354978E-03 Ry 0.000000E+00 Rz 1.000000E+00 Mode Shape No. 6 Dof Amplitude Ux 0.000000E+00 Uy 1.000000E+00 Uz 0.000000E+00 Rx 5.410365E-01 Ry 0.000000E+00 Rz 3.88642.6E-03 Dynamic Displacements At System Centroid Dof Amplitude Phase Angle Ux 2.093525E-06 2.074634E+01 Uy 8.311200E-06 2.301662E+02 Uz 3.624395E-06 2.593134E+01 Rx 4.122979E-07 7.080530E+01 Ry. .1.229705E-07 5.769943E+01 Rz 3.841612E-08 -1.719446E+02 Dynamic Displacements At User Specified Output Points Point No. 1 Dof Amplitude Phase Angle -Ux 3.051202E-06 3.333899E+01 Uy 1.192913E-05 2.357659E+02 Uz, . 3.177088E-06 2.078607E+01 Rx 4.122979E-07 7.080530E+01 Ry 1.229705E-07 5.769943E+01 Rz 3.841612E-08 1.719446E+02 Point No. 2 Phase Angle Dof Amplitude Phase Angle Ux 3.051202E-06 3.333899E+01 Uy 1.185932E-05- 2.364604E+02 Uz 3.600281E-06 2.569339E+01 Rx 4.122979E-07 .7.080530E+01 Ry 1.229705E-07 5.769943E+01 Rz 3.841612E-08 1.719446E+02 Point No. 3 Dof Amplitude Phase Angle Ux 3.051202E-06 3.333899E+01 Uy 1.17095.8E-05_ 2.380438E+02 .Uz 4.613446E-06 3.326744E+01 Rx 4.122979E-07 7.080530E+01 Ry 1.229705E-07 5.769943E+01 Rz 3.841612E-08 1.719446E+02 Point No. 4 Dof Amplitude Phase Angle Ux 1.931198E-06 2.786334E+01 Uy 8.347031E-06 2.361245E+02 Uz 3..564725E-06 8.392130E+00 Rx 4.122979E-07 7.'080530E+01 Ry 1.229705E-07 5.769943E+01 -Rz 3.841612E-08 1.719446E+02 Dynamic Displacements At.User Specified Output Points Point No. 5 Dof Amplitude Phase Angle Ux 1.931198E-06 2.786334E+01 Uy 9.187636E-06 2.268105E+02 Uz 4.010960E-06 2.800653E+02 Rx 4.122979E-07 7.080530E+01 Ry .1.229705E-07 5.769943E+01 Rz 3.841612E-08 1.719446E+02 Point No. 6 Dof Amplitude Phase Angle Ux 2.489743E-06 1.901160E+01 Uy 8,.347031E-06 2.361245E+02 Uz 9.218206E-06 5.076138E+01 Rx 4.122979E-07 7.080530E+01 Ry 1.229705E-07 5.769943E+01 Rz 3.841612E-08 1.719446E+02 Point No. 7 Dof Amplitude. Phase Angle Ux 2.489743E-06 1.901160E+01 Uy 9.187636E-06 2.268105E+02 Uz 4.020261E-06 4.161951E+01 Rx 4.122979E-07 7.080530E+01 Ry 1.229705E-07 5.769943E+01 Rz 3.841612E-08 1.719446E+02 Sheet No. Washington CALCULATION SHEET Calculation No.. Project No. PROJECT TITLE W/� !� CzDoS� F/'f��/S /D.✓ ' oo/ Calc. By ftD41 SUBJECT/FEATURE Go/`�f'�cSsa� /:DA/ Checked By , � Rev. LZ 0z C-7. V6 J-ociry , p ! L9 'Off 3 ��✓/sem c w s 1±7 ,e v is i= ��ra�� z, o Tvoc ,000286.3 I�L�o�iry ,o2m?q27' i1VI/see- ST/G G / !/�•e y' Coo v- ,c Iv? -e J T/1/S /s .4 Gon/D ilia �. ,�o�.✓D,QT�o.c/ �S C�a�/, J/ 54 Design of Structures and Foundations for Vibrating Machines Table 3-2 General Machinery -Vibration -Severity Data* Horizontal Peak Velocity (in./sec.) Machine Operation <0.005 Extremely smooth 0.005-0.010 Very smooth 0.010-0.020 Smooth 0.020-0.040 Very good 0.040-0.080 Good 0.080-0.160 Fair 0.160-0.315 Slightly rough 0.315-0.630 Rough > 0.630 Very rough 'After Baxter and.Bernhard (ref. 8). safety (service factor) have been proposed. These factors are applied to the computed maximum amplitude of vibration to obtain an effective vibration amplitude. Use of a service factor* (or additional factor of safety) has been proposed to account for the relative importance of the machine to overall plant operation. The actual vibration amplitude is multiplied by the service factor to obtain an effective vibration amplitude. The effective vibration amplitude (rather than the actual vibration amplitude) is then used to determine the adequacy of the installation. Single -stage centrifugal pump, electric motor, fan.. 1.0 Typical chemical processing equipment; noncritical ...................... 1.0 "Turbine, turbogenerator; centrifugal compressor... 1.6 Centrifuge, stiff-shaftt; multistage centrifugal pump ..........................2.0 Miscellaneous equipment, characteristics unknown ....................2.0 Centrifuge, shaft -suspended, on shaft near basket. .0.5 Centrifuge, link -suspended, slung ...............0.3 Effective vibration = measured single amplitude vibra- tion, inches multiplied by the service factor. Machine tools are excluded. Values are for bolted - down equipment; .when not bolted, multiply the ser- vice factor by 0.4 and use the product as a service factor. Caution: Vibration is measured on the bearin_ hous- ing, exce t as stated. The design checklist and design procedure may be summarized as follows. Note that most of the steps listed in the design checklist are implicitly considered in a computer analysis (see chapter 7). The checklist is appropriate for analysis of block -type foundations. Design Checklist Design Conditions Procedures Static Conditions Static Bearing Capacity Proportion footing area for 5050 of allowable soil pressure. Static Settlement Settlement must be uniform; center of gravity of footing and machine loads should be within 5 % of any linear dimension. Bearing capacity: Static plus Dynamic The sum of static plus modified dynamic load should not create a bearing Loads pressure greater than 75% of the allowable soil pressure given in the soil report. The combined center of gravity of the dynamic loads and the static loads Settlement: Static plus Repeated Dv- should be within 5% of the linear dimension from the center of gravity namic Loads of footing. In the case of rocking motion; the axis of rocking should coincide with principal axis of the footing. The magnitude of the resulting settlement should be less than the permissible deflecting capability of the connected piping system. Limiting Dynamic Conditions Vibration Amplitude at Operating The ma_eirrium single amplitude of motion of the foundation system as Frequency calculated from Table 14'_should .lie in zone A or B of Figure 3-3 for the given acting frequency. Where unbalanced .forces are caused by • From Blake (ref. 9). t Horizontal displacement on basket housing. 52 Design of Structures and Foundations for Vibrating Machines 0.10 0 0.01 v N d y 2L I C N � • v o ,= 'E o a 2 a c 0.001 nM E .r: Q p am 0 m Z 0.0001 100 1000 10,000 Frequency, cpm A EXPLANATION OF CASES E DANGEROUS. SHUT IT' DOWN NOW TO AVOID DANGER. D FAILURE 13 NEAR. CORRECT WITHIN TWO DAYS TO AVOID BREAKDOWN. r C FAULTY. CORRECT WITHIN 10 DAYS TO SAVE MAINTENANCE DOLLARS. B MINOR FAULTS. CORRECTION WASTES DOLLARS. A NO FAULTS. TYPICAL NEW EQUIPMENT. Figure 3-3. Vibration performance of rotating machines (see ref. 9). + FROM REIHER AND MEISTER (1931)—(STEADY STATE VIBRATIONS) o FROM RAUSH (1943) -(STEADY STATE VIBRATIONS) FROM CRANDELL (1949) (DUE TO. BLASTING ) a 0.1 0.05 0.02 a • 0.01 W 0 0.005 J a a 0.002 0.001 W U 0.0005 CL 0 0.0002 0.0001 \C, 9GrgO,CF O y'p0 yFs � G�yG9 Gd! U,9yo \RFs Fs . AF Fs �L N V 9 A sQy X O 4 'Ipy pG , F!y 9! 0y?1% F Z yOr Fy0r, ro No l0 .o�y/CO %�949Z AF9yr0 �lopo � n I'llCSX - 100 200 500 1000 2000 5000 10,000 FREQUENCY, CPM Figure 3-4. General limits of vibration amplitude for a particular frequency (see ref. 10). CA�'ER P1 LLAR8 12/21/2000 Maximum Unbalanced Forces and Moments for G3612 Engine Due to Manufacturing Tolerances Primary Force (kg) Secondary Force (kg) Engine rpm Vertical Horizontal Vertical Horizontal 700 2747,04,0 7 154 3'39.5/ 20 4 4, -Ol 9 / % $ ¢- 800 358 789, 2.S 2014 43, IJ 26$7, .3Z 12 2 G , � S 900 454/000.96 254559. 97 34 74.14 1533, a7 1000 560/234-593146 72.ZS 41170,3'1 194 /, 8y Primary Couple (kg -m) Secondary Couple (kg -m) Engine rpm Vertical Horizontal Vertical Horizontal 700 34825/7 / 209 1-,51170 23 /; (-• 3 2 800 4543283, 78 273/g74,G/ 30 2/7, D 4 28, i_3 900 5754/!�*, 79 34524116.39 38 Z7 9�5_ 1000 71 05-12547 4263-08/, Zs-4733�% '5�6 117? G Note : 2x30" Narrow Dampers (7C-2122) are used in the estimation. This data is based on the assumption that engine components may be machined to a maximum/minimum permissible weight tolerance and assembled in such a manner that produces maximum unbalanced forces and couples. An unbalanced assembly that produces a maximum unbalanced force tends to produce a minimum unbalanced couple and vice -versa. It is to be noted that these are maximum calculated values and standard assembly procedures rarely produce such extreme conditions. 7 23S k� • = Fac �-` OPERATING JOB #KC-1076A/B DATE: 9/3/02 BY: BG ITEM WEIGHT X Y Z MX MY MZ 1D 101712 21 1.5 0 2135952 152568 0 ENG/COMP BOX 18583 23.3 4.5 0 432984 83624 0 ENGINE 55300 30.5 8.8 0 1686650 486640 0 COMP FRAME 22500 17 7.7 0 382500 173250 0 COUPLING 1180 23.8 7.7 0 28084 9086 0 DST PC SUPPORT 1000 17 6.2 0 17000 6200 0 THR #1, 7.25' 2520 21.1 7.7 5.22 53172 19404 13154 THR #2, 7.25' 2520 20.4 7.7 -5.22 51408 19404 -13154 THR #3, 7.25' 2520 17.3 7.7 5.22 43596 19404 13154 THR #4, 7.25' 2520 16.6 7.7 -5.22 41832 19404 . -13154 THR #5, 7.25' 2520 13.6 7.7 5.22 34272 19404 13154 THR #6, 7.25' 2520 12.9 7.7 -5.22 32508 19404 -13154 SCRUBBER, 0900 10000 2.1 11 -5.22 21000 110000 -52200 SCRUBBER, 1000 10000 2.1 11 5.22 21000 110000 52200 BOTTLE, 1600 5633 16.6 11 -5.22 93508 61963 -29404 BOTTLE, 1700 12661 12.9 4.7 -5.22 163327 59507 -66090 BOTTLE, 1800 5633 17.3 11 5.22 97451 61963 29404 BOTTLE, 1900 12661 13.6 4.7 5.22 172190 59507 66090 COMP OIL FILTER 220 7.5 .4.6 3 1650 1012 660 ENG PLATFORMS 1795 30.3 9.3 0 54389 16694 0 EXHAUST/AIR SUPPORTS 2905 34.1 9.4 0 99061 27307 0 EXHAUST/AIR PIPING 7500 34.1 19.2 0 255750 144000 0 SENT OIL 16828 7.4 1.5 0 124527 25242 0 __YCOL/WATER 8228 17 1.5 -5.4 139876 12342 -44431 GLYCOL/WATER 3315 24.2 1.5 -4.5 80223 4973 -14918 LUBRICATOR OIL 5994 17 1.5 -5.4 101898 8991 -32368 FRESH OIL 18082 32.75. 1.5 - 0 592186 27123 0 FRESH OIL 7566 39.7 1.5 0 300370 11349 0 OIL IN ENGINE 2000 32.6 6.7 0 65200 -13400 0 OIL IN COMPRESSOR FRAM 702 17 6.5 0 11934 4563 0 COOLANT IN ENG AND PIPIP 2865 35 8.5 0. 100275 24353 0 PUMPS 550 0 0 0 SPINNERS 100 38.1 5.5 -7.2 3810 550 -720 OIL TANK HEATERS 200 0 0 0 PROCESS PIPE SPOOLS 828 0 0 0 TOTAL 351661 7439581 1812628 -91776 CGX 21.15555 FT FROM COMP. END OF SKID TOWARD ENGINE CGY 5.154477 FT FROM BOTTOM OF SKID UP CGZ -0.26098 FT FROM CL OF UNIT TOWARD THROW #1 TOTAL OPERATING WEIGHT= 364,000# ".7 T'.. Smumq OM - Qa 71 3 Pon T02075A0, tt Prcqec! .13 �J0 Rec-:n Oic,:q'i! Install weigtIts- Toicy Bole, a C; B,!: m.- mioct� 71 Ibs R 43E A250 7 lw'4CU 7 ;, � C, T 14 N 147 it not 1, 10 4 %: 3 7-1MCU 725U 161DO M 4 DMN w 1mcu 7 250 15g qu 3 9 A I,!- i 2, �u WOO SIP 81 Ey wq2 0720 &�4m Qto us 7, 7 CU 7.2 1691C lap 8P D-191 14720 E W35 My opp-tming 'I are. N()T SOLD - Gauuo;) IP "Afc-i Hjht cadt Q=aed max agau wygm snami DYNAkUC ROD LOAD SUMMARY In Ear.: Fomey X'Pin..Svk X VI: -1,3 1 Dy mu Deg Tmal Man Deg Max Deg Deg ---------------- C 3 9 5,'.38 267 TVN 3 74 W2Q Cang jjg URN`' 07 6 S 2 EC 2V T27"3 74 BU32 GA"O 2P TWO 73 1% to 3 C, 3 Q 08 267 T= 3 74 655 COM WZ T2W9D 72 17 w 4 C-3958�. 237 TVU3 74 P232 73 is 5 5 CNOT 20 MR3 74 6742 THNO ?I 5 8 "' 267 V27M3 74 67232 COW 21M Tako 73 ma, I. E ENaz - &M Rewm-Jj r.leg 30, :?r UNBALANCED FORCES & COUPLES KHP KIP , 'ViNiv::21 U, C, Sheet No. CALCULATION Washington SHEET Calculation No. Project No. PROJECT TITLE In//L D �$/�OS�= r x�s�/✓s/a�� Calc. By SUBJECTNEATURE 1512,/ Checked By J/Ir� ate Rev. WT per' /���T /7X ¢..3X 7, �S ;�. /S 8So k /Z/4 k _ /Z/4e //7-.e o/ l�S� /�/i� , DO/s�� • (ACI Z�7.Z2 —9S �t=cr (�, 4� �s ec s -- , o o �S �/ 2)03) /, 5/A✓ SAI / r } /, 61,E/ z/= r Sheet No. CALCULATION Washington calculation No. SHEET joom Project No. PROJECT TITLE Iil/�L �� �ooS� CXiJA�S/O.t� Z -3 -epd Calc. ByDate Rev. Zge SUBJECT/FEATURE l'2�1 i�,c'L'��s�Z i` D.L� Checked By Dat /S o 0d X 6 XJ To 1,4 rc1-o' A19 F,47- 1"714 4 ,47" 1 1GG IL-- /d doll G6z S5 .. •"kiln L `