SPL RF coupler: integration aspects

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SPL RF coupler: integration aspects V.Parma, TE-MSC with contributions from WG3 members: Th.Renaglia, U.Wagner, P.Coelho, N.Bourcey, A.Vandecraen Review of SPL coupler, CERN 16th-17th March 2010

description

SPL RF coupler: integration aspects. V.Parma, TE-MSC with contributions from WG3 members: Th.Renaglia, U.Wagner, P.Coelho, N.Bourcey, A.Vandecraen . Review of SPL coupler, CERN 16th-17th March 2010. β =1 cryo -module in SPL layout ( drwg SPLLJL__0014). - PowerPoint PPT Presentation

Transcript of SPL RF coupler: integration aspects

Page 1: SPL RF coupler:  integration aspects

SPL RF coupler: integration aspects

V.Parma, TE-MSC

with contributions from WG3 members:Th.Renaglia, U.Wagner, P.Coelho, N.Bourcey, A.Vandecraen

Review of SPL coupler, CERN 16th-17th March 2010

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β=1 cryo-module in SPL layout(drwg SPLLJL__0014)

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Cryogenic scheme (under discussion)

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Cavity/coupler assy

Part of interest

Doub

le-w

alle

d-tu

be

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Coupler integration functionalities (non-exhaustive list)

Functionality Requirement CommentRT/atm. to 2K/vacuum penetrations

-minimise static HL;- leak-tight penetration (o-ring);- mechanical decoupling from vacuum vessel (if not a support);

- Optimise thermal design

Isolation between coupler and beam vacua

- leak tight window- vacuum gauge outside cryostat

- Single ceramic window for HP RF

Gas cooling of double-walled tube (5 K-300 K)

- minimise static HL;- cryostat feedthrough of cooling line:

- leak-tight- avoid atm. moisture (T>dew

point)

- externally-mounted manual valves (presetting);- Heater for control (Ofelia’s talk)

Coupler maintenance Maintenance-free No in-situ intervention

Coupler as support (option under study)

-support/position cavities;- coupler flange mechanically fixed to vacuum vessel;- fix longitudinal position of cavities;- mechanical support of thermal shield

- impact of gas cooling on position (Ofelia’s talk);- Vacuum vessel as mechanical reference

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Transversal position of cavities inside cryostatBUDGET OF TOLERANCE (preliminary)

Step Sub-step Tolerances (3σ) Total envelopes

Cryo-module assembly

Cavity and He vessel assembly ± 0.1 mm (TBD)Positioning of the cavity

w.r.t. beam axis ± 0.5 mm

Supporting system assembly ± 0.2 mm (TBD)

Vacuum vessel construction ± 0.2 mm (TBD)

Transport and handling (± 0.5 g any

direction)N.A. ± 0.1 mm (TBD)

Stability of the cavity w.r.t. beam axis

± 0.3 mmTesting/operation

Vacuum pumping

± 0.2 mm (TBD)

Cool-down

RF tests

Warm-up

Thermal cycles

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Fixed support

Sliding support

Inertia beam

Invar longitudinal positioner

External supports (jacks)

RF coupler

Possible supporting schemes“standard” supporting scheme

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Fixed support

Sliding support

Inertia beam

Invar longitudinal positioner

External supports (jacks)

RF coupler

Possible supporting schemes“standard” supporting scheme

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External supports (jacks)

RF coupler + longitudinal positioner + vertical support

Intercavity support structure

Possible supporting schemesCoupler supporting scheme

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Coupler position: top ...?Contras:• Interferes with bi-phase tube move

sideways• Waveguides/coupler more exposed to

personnel/handling (damage, breaking window?)

Pros:• Easier connection of waveguides• Easier access (needed?)

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Coupler position: ...or bottom?Contras:• Space needs for waveguides under

cryostat• If coupler not a support (bellows)

support on top, i.e. centered tube not possible

Pros:• Centered bi-phase tube symmetry• Waveguides/coupler protected

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• Defines minimum diameter of “pipeline” type vessel:– Lenght of double-walled tube– Integration of thermal shield

RF coupler assembly constraints

Note: drwgs for information only (concept not final)

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Mid plane symmetry

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Need guiding?

l

2l

- If sag small enough- If strenght OK- isostatic

- couple cavities- hyperstatic

mid cavities most critical: sag reduces only to ½

No

Yes

Equivalent sketchLayout

inter-cavity guides

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Mass loads on internal supports(preliminary)

Description Load Comment

Cavity/he vessel/tuner ~2.0 kN per assembly (x 8 per cryomodule)

Piping/thermal shield/MLI 0.8 kN equally shared on coupler tube

Transport accelerations ± 0.5 g each direction

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Max sag: “to guide or not to guide?”

Stiffening of coupler/cavity assembly necessary Guiding between cavities is most probably necessary

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“standard” supporting

Max. sag minimized at a/L=0.20.

A 3rd central support seems mandatory

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comparing solutionsA) Coupler supporting scheme B) “standard” supporting scheme

Pros ContrasDesign simplicity Vacuum vessel:

- Stiffness (thickness, stiffeners)- Dim. stability- Precision machining- Cost

Single cavity adjustment at assy

Positioning stability (thermal, weld relieving...)

Inter-cavity guiding

Mid cavities guiding sufficient?

Pros ContrasCavities mechanical isolation from external perturbations: dim. changes (thermal, weld relieving), vibrations...

Design complexity

Vacuum vessel simplicity:-Reduced machining precision- reduced thickness

Central support needed (?)

Complex cavity adjustment at assy

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Summary• Coupler length (double-walled tube) sets

minimum diameter of cryo-module• Coupler could be used as cavity support and is an

interesting option• Vacuum vessel become of paramount importance

for mechanical positioning/stability• Guiding between cavities probably needed

(relieve cantilever)• In case of “standard” supporting solutions,

coupler design considerations still valid mechanical decoupling with bellows