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TTCB Progress Structural Analysis. Presented by XM QI. SYSU mechanical group: Structural Analysis: XH Diao, XM Qi, GY Chen Mechanical Design: SS Zheng, XM Qi work with Corrado , . April. 22, 2006, Cern, Geneva. FEM Model. Valves. Heat Exchange. Start up radiator plate. Pump. - PowerPoint PPT Presentation
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Tracker Thermal Control System
TTCB ProgressTTCB ProgressStructural Analysis Structural Analysis
April. 22, 2006, Cern, Geneva
SYSU mechanical group:
Structural Analysis: XH Diao, XM Qi, GY ChenMechanical Design: SS Zheng, XM Qi work with Corrado ,
Presented by XM QI
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Tracker Thermal Control System
FEM ModelFEM Model
Start up radiator plate
Side plate
Base plate Accumulator
Heat Exchange
Pump
Valves
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Tracker Thermal Control System
TTCB FEM ModelsTTCB FEM Models
components element Connection Element connecting to related massAccunulator shell rigid bars Accu Brackets nonstructural massAccu Brackets shell coupled degree of freedom Main plate
rigid bars Accumualtor
Heat Exchanger beam with lumped mass nonstructural massHX Brackets Down solid elements coupled degree of freedom Main plateHX Brackets up shell elements coupled degree of freedom HX Brackets DownPump beam with lumped mass nonstructural massPump Brackets shell coupled degree of freedom start up radiatormain Plate shell elements coupled degree of freedom start up radiator
constrains USSSide plate shell elements coupled degree of freedom start up radiator
constrains USSstart up Radiator shell elements coupled degree of freedom Main and Side plateValves lumped masses on start up radiatorsendors lumped masses on main paltePelteir sadle solid connector elements Accumulator
Others nonstructural mass distributed uniformaly on top of the main palte
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Tracker Thermal Control System
Mass modeling In FEM Models Mass modeling In FEM Models (Based on document (Based on document TTCSMassBudget03112005.xlsTTCSMassBudget03112005.xls by Johanes) by Johanes)
Heat Exchanegr 0. 14 1. 6 1.6-0.14 lumped mass on HX beamPump 0. 029 1. 69 1.69+0.1-0.029 lumped mass on pump beamvalves 0.1*4 4 lumped masses on main platemain Plate 2. 99start up radiator 0. 94side plate 0. 78Pump Brackets 0.01*2*2Accu Brackets 0.255+0.211HX Brackets 0.0464*2pelier sadle 0.016*2
total mass in above model : 15.337ttcb budget: 36.786rest mass: 36.786-15.337=21.449 are distributed uniformly on the top of main plate as nonstructural mass
result is conservative: 36.786 is the mass including condensor(6.12kg)
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Tracker Thermal Control System
FEM Model Elements SummeryFEM Model Elements Summery
Shell(quadrilateral): 50851 Shell(quadrilateral): 50851
Solid(linear brick): 5984Solid(linear brick): 5984
Rigid bar: 120Rigid bar: 120
Connector: 6Connector: 6
Lumped mass: 15Lumped mass: 15
Constrained elements: 630 Constrained elements: 630
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Tracker Thermal Control System
For FEM Structural Analysis DetailFor FEM Structural Analysis Detail
See following reference documents:See following reference documents:
TTCB_Structure Analysis_SYSU_I-deasV11_result_Jan2006.docTTCB_Structure Analysis_SYSU_I-deasV11_result_Jan2006.doc
progress on January, 2006progress on January, 2006
TTCB_Structure modification proposal_SYSU_I-deasV11_result_Mar2006.docTTCB_Structure modification proposal_SYSU_I-deasV11_result_Mar2006.doc
Section 5.8 Main plate layout optimization, progress on March, 2006 Section 5.8 Main plate layout optimization, progress on March, 2006
TTCB_Structure Analysis_SYSU_I-deasV11_result_April2006.docTTCB_Structure Analysis_SYSU_I-deasV11_result_April2006.doc
Section 7, Main plate thickness optimization, progress on April, 2006 Section 7, Main plate thickness optimization, progress on April, 2006
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Tracker Thermal Control System
General Analysis ResultGeneral Analysis Result
See document See document
TTCB_Structure Analysis_SYSU_I-deasV11_result_Jan2006.doc TTCB_Structure Analysis_SYSU_I-deasV11_result_Jan2006.doc
Table 5.1: main/startup/side plate and Acc Brackets/HX Bracket/Pump Bracket Table 5.1: main/startup/side plate and Acc Brackets/HX Bracket/Pump Bracket
sturctural stress and margin of safetysturctural stress and margin of safety
Table 5.2: USS/TTCB connection bolts calculation;Table 5.2: USS/TTCB connection bolts calculation;
Side plate/USS connection bolts calculation;Side plate/USS connection bolts calculation;
StartUp Radiator/Side&Main Plate connection bolts calculation;StartUp Radiator/Side&Main Plate connection bolts calculation;
Acc Bracket/main Plate connection bolts calculation;Acc Bracket/main Plate connection bolts calculation;
HX Bracket/main Plate connection bolts calculation;HX Bracket/main Plate connection bolts calculation;
Pump Bracket/main plate connection bolts calculation.Pump Bracket/main plate connection bolts calculation.
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Tracker Thermal Control System
Different Ribs layouts Different Ribs layouts
38 different layout are tried38 different layout are tried
( see ( see 060316ttcb-sysu-fem-model-facies.rar 060316ttcb-sysu-fem-model-facies.rar
ttcb-sysu-reaction-thirty-eight-modification-060319.rarttcb-sysu-reaction-thirty-eight-modification-060319.rar for detail) for detail)
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Tracker Thermal Control System
Main plates reaction force with above designMain plates reaction force with above design
Load
Case
(N) (N) (N) (N) ( l bf ) ( l bf ) ( i n. l bf . )
1 316. 6 513 602.83 845. 1 188.52 134.48
2 248. 9 - 51. 9 254.25 561. 9 125.35 56.72
3 - 206. 2 366. 8 420.79 931. 4 207.78 93.87
4 - 316. 6 - 513 602.83 0 0 134.48
5 - 951. 1 465 1058.69 560. 3 124.99 236.17
Shear Bending force
MofS
Main Plate Bolt Reaction Force and MofSafety Calculation
y Z Shear Tension Tension
Maximum reaction force 1064.6N 931.4N
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Tracker Thermal Control System
Optimization on Thickness of main pate Optimization on Thickness of main pate
Model change: Accu Slide end as moving along axis Model change: Accu Slide end as moving along axis
Three thickness 3mm,4mm,5mm were calculatedThree thickness 3mm,4mm,5mm were calculated
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Tracker Thermal Control System
Result 1 on Different Thickness of main pateResult 1 on Different Thickness of main pate
Top plate
Thickness
Case x y z (mm) Von Mises Max Principal (mm) Yield Ultimate
1 22 5. 5 5. 5 5 72. 4 62. 6 0. 365 3. 266 2. 63422 5. 5 5. 5 4 80. 5 98 0. 415 2. 837 1. 32122 5. 5 5. 5 3 147 110 0. 491 1. 101 1. 068
2 5. 5 22 5. 5 5 70. 2 62. 1 0. 115 3. 4 2. 6635. 5 22 5. 5 4 72. 1 63. 4 0. 124 3. 284 2. 5885. 5 22 5. 5 3 74. 7 65 0. 14 3. 135 2. 5
3 5. 5 5. 5 22 5 60. 8 65. 5 0. 226 4. 08 2. 4735. 5 5. 5 22 4 61. 9 66. 5 0. 25 3. 99 2. 4215. 5 5. 5 22 3 91 68. 2 0. 291 2. 394 2. 336
4 - 22 - 5. 5 - 5. 5 5 72. 4 66. 6 0. 365 3. 266 2. 416- 22 - 5. 5 - 5. 5 4 80. 5 81. 8 0. 415 2. 837 1. 781- 22 - 5. 5 - 5. 5 3 132 152 0. 491 1. 34 0. 497
5 - 5. 5 - 22 - 5. 5 5 70. 2 74. 5 0. 115 3. 4 2. 054- 5. 5 - 22 - 5. 5 4 72. 1 76. 5 0. 124 3. 284 1. 974- 5. 5 - 22 - 5. 5 3 74. 7 79. 1 0. 14 3. 135 1. 876
6 - 5. 5 - 5. 5 - 22 5 60. 8 52. 8 0. 226 4. 08 3. 309- 5. 5 - 5. 5 - 22 4 61. 9 55. 2 0. 25 3. 99 3. 121- 5. 5 - 5. 5 - 22 3 91 104 0. 262 2. 394 1. 1875
Loads Cases: Base Plate
Load Acceleration (g) Limit Stress [N/mm2] Displacement Margin of Safety
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Tracker Thermal Control System
Result 2 on Different Thickness of main pateResult 2 on Different Thickness of main pate Load Top Plate y Z Shear Tension Tension Shear Bending force
CaseThickness
(mm) (N) (N) (N) (N) ( l bf ) ( l bf ) ( i n. l bf . )
1 5 0. 5 40. 6 40.6 833. 4 185.91 9.06
4 1. 2 34. 3 34.32 863. 9 192.72 7.66
3 7. 2 20. 2 21.44 909. 9 202.98 4.78
2 5 312 - 50. 6 316.08 597. 9 133.38 70.51
4 313. 3 - 57. 7 318.57 590. 8 131.8 71.07
3 315. 1 - 67. 6 322.27 588. 1 131.19 71.89
3 5 - 294. 9 485. 3 567.88 1044. 6 233.03 126.68
4 - 293 478. 7 561.25 1051. 9 234.67 125.2
3 - 283. 4 464. 5 544.13 1062. 8 237.09 121.38
4 5 19. 8 107. 3 109.11 24.34
4 20. 6 110 111.91 24.97
3 23. 6 113. 5 115.93 25.86
5 5 - 346. 3 19. 9 346.87 383. 4 85.53 77.38
4 - 333. 6 14. 9 333.93 405 90.35 74.49
3 - 320. 9 9. 5 321.04 426. 8 95.21 71.62
6 5 58. 1 - 373. 3 377.79 656. 6 146.47 84.28
4 56 - 367. 3 371.54 558. 3 124.55 82.88
3 52. 8 - 357. 3 361.18 549. 9 122.67 80.57
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Tracker Thermal Control System
Result 3 on Different Thickness of main pateResult 3 on Different Thickness of main pate
Thickness 1 2 3 4 5 6 7 8 9 10
249 272 2815mm 150 162 182 291 330 361
4mm 147 155 171 200 231
209
258 268 272 285
184 197 211 2403mm 136 149 155 258 265 273
349
First Ten Natural Frequencies
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Tracker Thermal Control System
Following TBC for Further ProgressingFollowing TBC for Further Progressing
1.1. This version can be a final document with This version can be a final document with neccesary modification on bolts calculation? neccesary modification on bolts calculation? Or should be in more detailling; Or should be in more detailling;
2.2. Mass Budget Table Updated;Mass Budget Table Updated;3.3. Pump Controller Mass listed separately with Pump Controller Mass listed separately with
pump;pump;4.4. TTCB Design close(until no big modification TTCB Design close(until no big modification
expected);expected);5.5. Components Material Frozen; Components Material Frozen; 6.6. Bolts Connection Tables frozen;Bolts Connection Tables frozen;7.7. Modified Template for Bolts calculation. Modified Template for Bolts calculation.
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Tracker Thermal Control System