cryomodule for crab cavity tests with sps
DESCRIPTION
Cryomodule for Crab Cavity Tests with SPS. Shrikant Pattalwar Accelerator Science and Technology C entre STFC Daresbury Laboratory, UK. 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013, Daresbury. Acknowledgements. This presentation is on behalf of the members of the Global WP4 team . - PowerPoint PPT PresentationTRANSCRIPT
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The HiLumi LHC Design Study (a sub-system of HL-LHC) is co-funded by the European Commission within the Framework Programme 7 Capacities Specific Programme, Grant Agreement 284404.
Cryomodule for Crab Cavity Tests with SPSShrikant Pattalwar
Accelerator Science and Technology CentreSTFC Daresbury Laboratory, UK
3rd Annual Hi-Lumi Meeting Nov 11-15, 2013, Daresbury
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Acknowledgements
STFC ASTeC, Technology, University of LancasterCERN Various DepartmentsLARP ODU+SLAC, BNL, FNAL
This presentation is on behalf of the members of the Global WP4 team
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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Contents • Factors Influencing Design Requirements
• Achievements so far … Concept designs for Helium Vessel and Cryomodule
• Work in Progress
• Future Plans
• Conclusion
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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Requirements
• Operating Temperature • Magnetic shielding• Helium Vessel • Couplers and Interfaces• Tuner mechanism• Dynamic Heat Load• ….
1. Cavity
• Two beam pipes• Heat load due to beams• Helium Vessel Geometry • Internal Layout• ….
2. LHC
• External Geometry• Third beam pipe ( SPS
Bypass)• Coupler Orientations • Integration with
Infrastructure• Operation
3. SPS Layout
Requirements for the cryomodule are influenced by various Factors
Talk # 92 by Rama Calaga and # 95 Alex Ratti
Talk # 100 by Alick Mcpherson# 106 by Ofelia Capatina
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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Requirements continued
• Cooling Capacity at various temperatures
• Cooling Processes• Ports and Interfaces• Operating modes
4. Cryogenic Services
• Mechanical Design • Safety and Pressure Relief • Volumes, pipe sizes• Methods of QC/QA
5. Regulations and directives
6. Other
• Intermediate Tests (SM18) • Assembly Procedures• Instrumentation• Cost• R&D needs Talk # 102 by Laurent Tavian Talk # 105 by Ofelia Capatina
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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Helium Vessel UK 4-Rod Cavity Cavity in He Vessel Parts of the Vessel
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Courtesy : Graeme Burt and Ben Hall, ULAN Saclay-II type tuner
SPS beam pipe
LHC (dummy) beam pipe
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Cryoperm magnetic shields
OVC to coupler ISO K 500 spool pieces
Tuners
2 Phase He line
Top fill LHe line
Bottom fill LHe line
Motor magnetic shield
LHe level probes
Pipework for liquid nitrogen connections
Thermometry and wiring for entire string
Fully Assembled Cavity String (4R)
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Courtesy : Tom Jones (STFC)
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Helium Vessel ODU Dipole cavity BNL Double QW cavity
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Courtesy : HyeKyoung Park (ODU) Courtesy : Ofelia capatina (CERN)
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Cryomodule Schematic (P&ID) Courtesy : Andy May (ASTeC)
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2150mm 800mm
1520mmCryogenics interface
Additional ports for LOM extraction/instrumentation
2mm thick MuMetal Magnetic shield
Module positioning system
1050 AluminiumThermal shield (80K) Cooling loop TBD
Cryomodule Concept
More details in - Conceptual design of a Cryomodule for Crab Cavities for HiLumi-LHC S. Pattalwar, et al, MOP 087, SRF 2013, Paris
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Design features• simplifies the assembly
procedures• provides sufficient access to
internal components during assembly and after installation
• FPC is used as the main support for the cavity string.
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Compatibility with SPS InfrastructureRequirements Concept Design
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1 Clean Room Operations• Assemble cavity string • Couplers assembled at 90o
• Beam pipe closed with gate Valves
2 Outside the clean Room• Load the cavity String from Side
3 Align the string with the vacuum chamber
4. Lift and assemble with top plate of the vacuum chamber
Assembly Sequence – Proposal 1 (Side Loading)
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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ISO K clamp
80K300K
Mu Metal magnetic shield (blue).
80K thermal shield (green). 20mm allocated for MLI
Final Assembly
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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1 Clean room OperationsCavity, Coupler and Beam pipe
2 Outside the clean RoomMounting on the top plate
3 Outside the clean RoomAssembly of the cold parts
4 Load from the top into the vacuum chamber
Assembly Sequence – Proposal 2 (Top Loading
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Courtesy : Ofelia capatina (CERN)
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Final Assembly (Top Loading )
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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RF Input
Cryo services
Sliding support table
Cryomodule in SPS
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Conclusion First level constraints defined by SPS layout have been successfully overcome
The design appraocah• simplifies the assembly
procedures• provides sufficient access to
internal components during assembly and after installtion
• reduces overall manufacturing cost
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Common Design Approach UK 4-Rod
US Dipole
US Double QW
Conclusion – A common design approach to accommodate all the 3 cavity designs has been successfully developed.
• External Envelope• Cryogenic Interface• Cryogenic Process• Alignment (external and Internal) • …….
Challenges – Couplers and Tuners and their locations for the three designs are different.
For illustration only
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Work In Progress
• Coupler designs for HOMs and LOMs and their integration with Infrastructure• Magnetic Shielding • Alignment • Integration with Cryogenics and heat load management• Switch over with the SPS BY-PASS or with other cryomodule• Safety , Pressure Vessel Regulations etc.• Tests at SM-18• ........................• ........................
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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HL per cryomodule HL @2 K [W] HL @ 80 K
(TS) Comment
Dynamic
Deflecting mode 5.0 - Confirmed? Other Order
Modes TBD TBD
RF Coupler TBD TBD Beam Current 0.5 Tentative
Static
Radiation (cavity +Phase Sep. Cold surface + Thermal
Shield
0.2 6.8
Rescaling from LHC o W/ m2 @ cold mass
o 1.7 W/ m2 @ Thermal shield
CWT
0.557(rad) + 0.892(cond) =
1.5W x 2 = 3.0
0.625(rad) + 5.926 (cond) =
6.6W x 2 = 12.6
1 heat intercept @ 80K in the middle
Supporting System 1.0 3.3 6 tie rods/cavity
RF Coupler
0.501(rad) + 0.853(cond) =
1.4W x 2 = 2.7
0.587(rad) + 5.662 (cond) =
6.3W x2 = 12.6
1heat intercept @ 80K in the middle
Cables & Instrumentation 1.0 - Tentative
Other order modes TBD TBD Design dependent
Totals ~13.4 + TBD ~34.9 +TBD
Heat Load Budget
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Compliance with Regulations - PED
Maximum LHe volume < 100 LMaximum Operating Pressure 0.8 barG
Max He pressure0.43 barG
Max pipe diameter (ID) < 25 mm
Max Pressure 5 bar??
Category 0 for LHC Category 1 for SPS tests
CC in LHC Pmax 0.5 bar
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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Manufacturing Final testsDesign Acceptance TestsQ1 (M3) Q2 (M6) Q3 (M9) Q4(M12) Q5(M15) Q6(M18) Q7 (M21) Q8 (M24) Q8 (M24) Q8 (M24)
Cavity Development and Performance tests Couplers Manufacture Tests
C1 in manufacturing
C1 Bare cavity tests
Dressed C1 test
SM-18 RF test
C2 Bare cavity tests
Dressed C2 test
Install and Commsioning at SPS
Interim FAT Final FAT
He vessel design V1 in ManufacturingCryomodule Engineering V2 in Manufacturing
Design Ancillary systemsManufacturing of Ancillary systems
Design OVC
Manufacturing of OVC
Define Instrumentation System AssemblyDevelop QA/ PED/Assembly/Test procedures
Design performance Tests Manufacturing and Assembly
Install and Commsioning
at SPS
C2 in manufacturing
Concept Design Engineering DesignManufacturing
Acceptance Tests
March 2014 Commissioning
Future Plan (Expectations)
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
Jan 2016
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Conclusion
1. First level constraints defined by SPS layout have been successfully overcome
2. A common design approach to accommodate any of the 3 cavity designs has been successfully developed
3. Overall design process is at an advance stage .
4. Most of the remaining issues are well understood and solutions are being worked out through collaborative efforts
5. WP4 Global collaboration is working well and advancing in a right direction
Shrikant Pattalwar 3rd Annual Hi-Lumi Meeting Nov 11-15, 2013 Daresbury
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Thank You
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