1 Status of the 11T cryo-assembly design and integration Presented at ColUSM #34, February 21, 2014

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Presentation transcript:

1 Status of the 11T cryo-assembly design and integration Presented at ColUSM #34, February 21, 2014

Outline  Recall from last talk (January 2013)  What are we looking for in the new solution  The 11 T cryo-assembly  Main integration issues  Status of the cold mass and cryostat design 2

MB From last talk (Jan. 2013)  Cold collimator discarded. The baseline is a room temperature vacuum baked collimator.  Remove one MB cryo-magnet and replace it with a new cryo- assembly of equal length, integrating:  2x 11T short magnets  1 collimator  Longitudinal integration benefits from placing the collimator in the middle  Fitting within the mm length of a standard MB is a challenge 3 11 T Collimator 15660

Aim for full interchangeability with a standard dipole (no changes to neighbouring cryomagnets) 4 K2 QRL side M2 V2 W Y M1 M3 E C’ V1 K1 X N  No changes to cryo, electrical or mechanical interfaces (different jack’s position is inevitable)  mm long, interc. included  Inside the 11 T cryostat:  X-line remains straight  He II free cross section: 60 cm 2  Pressure drop of He II circuit: 4.3 kPa/m (50 mm smooth pipe)  Pressures and temperatures acording to LHC-Q-ES-0001 (edms 90032)

Operation and maintenance  Mechanical decoupling from cryostat and collimator for removal and alignment of collimator without warming up the arc  bellows between collimator tank and cryostat, independent supports to the floor, compatible integration  One collimator design fits beam 1 and beam 2  Minimise exposure to residual radiation  simplify removal/installation of collimator, ex. quick CF flanges, pre- aligned collimator support system, “rapid” electrical and hydraulic connections (but not remote handling), permanent bakeout insulation  Ports for “RF-ball” test of new sectors  Transport constraints: Stay in the “shadow” of the existing arc cryostat 5

Vacuum  Room temperature (bakeable) collimator vacuum operated and maintained independently from cold beam vacuum  sector valves on both lines  Beam screens (K-line cooling) with same reliability and performance as rest or the arcs (no helium to beam vacuum welds, testing, etc.)  No demountable vacuum tight joints in cryogenic system (all welded)  Ensure pressure safety of each new beam vacuum “subsectors”  rupture disks on SSS ports  Ensure pressure safety of insulation vacuum (DN 200’s)  Respect current RF-impedance requirements: ex. shielded sector valves, shielded bellows, max 15º taper angle 6

Thermo-mechanical  Busbar flexibility must take into account adjacent magnets  Temperature offset between cold mass and beam screen during transient  Temperature variation between two cold masses during transient  Cold to warm transitions on the beam lines 7

Before the 11 T magnet development: QTC (2010)  Main drawback: extensive machine layout changes to create space m m interc. = 4.5 m installation length

Could the QTC cryostat concept be “extended”?  Can only be finished after cryostating  Dealing with welding distortions is a major issue  Distortions amplified with length  Adjustment of cold supports posts is required  Complicated assembly procedure 9 Longitudinal butt-welds Cover closure w/ fillet welds New approach needed

The 11 T cryo-assembly concept  Independently cryostated and handled cold masses, linked through two short transfer lines  Transfer lines with expansion joints mechanically decouple cryostats A and B  Splice and piping interconnect in the tunnel, all other work prior to installation  Can use the existing TCLD collimator design with modified the supports 10 Collimator Lines M, E, N, K, C’ Reinforced jacks to widstand vacuum forces 11 T cold mass A11 T cold mass B Line X Independently supported collimator Busbar splice and interconnect done in the tunnel Flexible S-shaped busbar stabiliser Busbar lyra

Access for in-situ repair  Once the collimator removed, the vacuum vessel cover can slide open  Good to have in-situ access for repair of «fragile» components:  Expansion joints  Flexible hoses  Diode  Instrumentation feedthrough (IFS)  Current leads (?) 11 Collimator Cold mass ACold mass B

3D Integration 12

13 Diode ? Splices Line M (6 busbars + splools) Line N Line E Lines C’ and K (not shown) Collimator Line X C’ and K lines not shown

14 Interconnect sleeve (rigid) Expansion joints or flexible hoses on all lines Expansion joints RF-shielded bellows

Elements defining the design in the transverse plane  Line X insulation  RF-shield module of gate valve 15 N E M X QRL sideTransport side

Main features  Seen by neighbouring magnets as standard MB cryo-assembly: Staightforward replacement in case of major problem  Can be cold tested as a single unit in a dipole test bench and split in two for handling and transport  Standard alignment procedures  Completely independent operation of collimator and cryogenic systems  Access for some in-situ repairs  Simplified construction  Non-compromised functionality wrt existing arcs  Passed a first iteration with simplified CAD model  Minimised impact on the collimator design (assuming 800 mm long TCLD) 16

Will it fit in mm? (Layout of beam line equipped with collimator) 17 New: 800 mm Estimated potential for optimisation, design work will start now...

Main integration topics 18 TopicIssueStatus Sizing of cold beam linesStandard 50 mm cold bore tubes and beam screens Approved PoweringCurrent baseline: In series with MB magnets Trim circuit required 2x 300 A current leads integration In-work Magnet protectionDifficult integration of diode stack in cryo-assembly B Starting soon SpoolsOne pair integrated in cold mass B, downstream end cover To be confirmed Longitudinal integrationRe-design vacuum components to optimise length Starting soon (TE-VSC) Electromagnetic interferenceInterference between busbar magnetic field and collimator LVDT’s? To be discussed Over pressure safety devicesInsulation vacuum: number and placement of DN 200’s Beam vacuum: rupture disks To be discussed Done: All SSS equipped with rupture disks during LS1 (TE- VSC) InterfacesPrepare and approve interface specification On-going

Current boundary conditions Designation Current L [mm] Optimized L [mm] End cover154 Shrinking cylinder extension (w.r.t. end plate)56 End plate (longitudinal limit of the active part of the magnet)7570 Collared coil assembly5622 End plate (longitudinal limit of the active part of the magnet)7570 Shrinking cylinder extension (w.r.t. end plate)56 End cover154 Cold mass length “C-plane” to “L-plane” (not including IC) /11/2013 Cold mass integration status and plans19 One pair of spool pieces needed; any of the four magnet ends of a complete assembly (2 x 11T dipoles and 1 collimator) is acceptable, will be likely on the far right end A cryo-magnet assembly (1 x 11T dipole in its cryostat) shall be exchangeable (the collimator, and the other cryo-magnet assembly to remain in place) Frederic Savary

Two concepts under study A. Integrated bus bars, all (M1, M2, and M3) inside the cold mass assembly B. Externally routed bus bars, for the lines M1 and M2 (quadrupoles, and spools) The integration of the bus bars is a challenge, and a detail design study is needed to confirm the conceptual design. There are good indications today that it will be possible In both cases, apply the solutions known from the past experience, as much as possible The integration of a second diode stack, should it be needed for the protection, is also extremely challenging, in particular to make possible maintenance or repair work in situ. A preliminary study will be initiated in the next 2 weeks. 6/11/2013 Cold mass integration status and plans20 Frederic Savary

Possible bus bar routing – left of collimator 6/11/2013 Cold mass integration status and plans21 “Lyra side” Courtesy Ch.Y. Mucher Frederic Savary

Another solution … 6/11/2013 Cold mass integration status and plans22 Courtesy Ch.Y. Mucher Frederic Savary

Vacuum vessel design  Engineering design of vacuum vessel cover on-going  Driven by the displacements at the beam lines  Stress analysis according to EN (European code for vacuum insulated cryostats)  Detailed design starting now, since busbar routing seems feasible 23

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