Magnetic shielding and thermal shielding

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Presentation transcript:

Magnetic shielding and thermal shielding Sébastien ROUSSELOT Patxi DUTHIL Philippe DAMBRE Patricia DUCHESNE Denis REYNET Sylvain BRAULT Unité mixte de recherche CNRS-IN2P3 Université Paris-Sud 11 91406 Orsay cedex Tél. : +33 1 69 15 73 40 Fax : +33 1 69 15 64 70 http://ipnweb.in2p3.fr November 4th 2011

Magnetic shield Thermal shield Conclusion Overview contents lundi 5 août 2019 Magnetic shield Overview Warm magnetic shield Cold magnetic shield Thermal shield Thermal shielding concept Conclusion

Magnetic shielding concept Overview Surface resistance of superconducting cavities can be deteriorated by the trapped DC magnetic field in Nb. The magnetic shielding for pure Nb cavity is one of the major parameter that affects the performance of the cavity and also the cryogenic loss.  Double shielding: Warm magnetic shield (@ room T°) Cold magnetic shield (@ cryogenic T°) Warm magnetic shield Cold magnetic shield

Magnetic shielding concept Overview Access for maintenance (tuner, HOM) (Possibly) Access to the inter-cavity connections during the (pre-)alignment phase

Magnetic shielding concept Warm magnetic shield Replaced by the use of low-carbon steel for the vacuum vessel Warm magnetic shield

Magnetic shielding concept Cold magnetic shield Material: Cryoperm, A4K (TBD) Required magnetic properties (permeability) obtained Below a critical T° If the material is annealed Avoid apertures and sharp angles Use of simple shapes No mechanical modification possible after annealing

Magnetic shielding concept Cold magnetic shield 2 possible solutions: Discontinuous shielding: one shield per cavity Continuous shield: one shield for the string of cavity

Magnetic shielding concept Cold magnetic shield One shield per cavity Main advantages Permanent access to the cavity interconnections Mounted before the alignment procedure (no alteration of the alignment) Related problematic Assembly procedure  need to be mounted before the tuner End cap closures: Lack of space (presence of the tuner, cavity interconnections…) Needs of several apertures (tuner supports) → solution abandoned Alternative studied solution (CERN) : magnetic shield inside the cavity LHe tank → difficulty to manufacture the tank

Magnetic shielding concept Cold magnetic shield One shield for the string of cavities Main advantages Simpler geometry (and construction) Available space Related problematic Maintenance access (tuner, HOM) Access to the cavity interconnections for the alignment procedure  Solution proposed

Magnetic shielding concept Cold magnetic shield One shield for the string of cavities Half part-sleeve 1 Sliding pods half-part shield 1 Knob Stopper Half-part sleeve 2 half-part shield 2 Fixation screws

Magnetic shielding concept Cold magnetic shield One shield for the string of cavities 1- Positionning of the half screens 2- Fixation with screws on the tank interface 3- Positionning of the half sleeves 4,5 & 6- Positionning of the half sleeves

THERMAL shielding concept Overview Thermal radiation from the ambient T° vacuum vessel to the 2K cold mass must be reduced in order to lower the static losses. Thermal shield aim at reducing the radiant heat. The attenuation factor depends on: The number of shields (the highest, the better) The temperature difference between cold mass and its closest shield (the lower the better) → also related to the temperature homogeneity of the shield The emissivity of the shields (the lower the better) The area of the shield (the lower the better) The shape of the shields (the view factor)

THERMAL shielding concept Number of thermal shield: 1 T°: 50 -75K Emissivity: the shield will be covered with a reflective MLI (20-30 layers) having a low emissivity Material: high thermal conductivity allowing for: An effective cooling of the shield during the cool down phase; A good homogeneity of the shield temperature (reducing the thermal losses);

THERMAL shielding concept Thermal conductivity for different materials Estimated losses on the thermal shield : 240W (full length cryomodule) For 2mm thickness, T < 4K for materials having a thermal conductivity above 100W/m/K Material of the thermal shield will be proposed based on construction consideration

THERMAL shielding concept Shield inserted within the vacuum vessel (before cryostating) Larger area (larger diameter) Shape: larger view factor Top cover NB1: Needs of a dedicated tooling for its insertion within the vessel NB2: Needs of an opening for the insertion of the string of cavities. The cover must be actively cooled (large area)

THERMAL shielding concept Shield positioned around the string of cavities before cryostating Smaller area Shape: smaller view factor Mounted on the string of cavities during the dressing phase  inserted within the vacuum vessel with the string of cavities during the cryostating (same tooling)  Solution proposed

THERMAL shielding concept End cap top cover (passively cooled) Thermal shielding concept Half part thermal shield Half part thermal shield Maintenance access ports top covers End cap with C/W transition (actively cooled)

THERMAL shielding concept Half part thermal shield Maintenance access ports top covers Half part thermal shield End cap top cover (passively cooled) End cap with C/W transition (actively cooled)

THERMAL shielding concept Cooling line Fixed point of the thermal shield is positionned on the third coupler  25mm of max thermal displacement (at extremities)

THERMAL shielding concept 50K 300K Support The thermal shield is not interfaced on the cold mass to limit the thermal losses @ 2K → interface on the coupler flange @ 300K Support material: composite (epoxy glass) Thermal compensation (30mm max.)

THERMAL shielding concept Cold/Warm transition The thermal shield is not interfaced with the cold Cooling line Interface To Be Define (Flexibility required) End cap (actively cooled) C/W transition welded on the screen

THERMAL shielding concept Cold/Warm transition The thermal shield is not interfaced with the cold Cooling line Interface To Be Define (Flexibility required) End cap (actively cooled) C/W transition welded on the screen

Continuous magnetic shield (covering the string of cavities) proposed CONclusion Magnetic shield Continuous magnetic shield (covering the string of cavities) proposed Simple geometry Movable sleeves to keep a (small) maintenance access to the tuner and HOM  Needs of magnetic computations to validate the geometry → CERN Thermal shield Small thermal shield around the string of cavities proposed Supported on the coupler flange Movable top covers for maintenance access required

Thank you for your attention Unité mixte de recherche CNRS-IN2P3 Université Paris-Sud 11 91406 Orsay cedex Tél. : +33 1 69 15 73 40 Fax : +33 1 69 15 64 70 http://ipnweb.in2p3.fr