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公开(公告)号:US20180208333A1
公开(公告)日:2018-07-26
申请号:US15743223
申请日:2016-07-07
Applicant: AIRBUS DEFENCE AND SPACE SAS
Inventor: Philippe Cesari , Jacques Cottier , Vincent Claudet
CPC classification number: B64G1/58 , B64G1/428 , B64G1/50 , H01R13/04 , H01R13/18 , H01R13/6277 , H01R13/64
Abstract: A device for electrical connection intended to connect a super-insulating mattress to a structural panel of a spacecraft, said connection device comprising: a conducting sleeve having an axis extending in a first direction, said sleeve comprising a device for axial fastening of the insulating mattress and a support, a conductive pin suitable for being arranged in said sleeve, an elastic element carried by said support, said elastic element being suitable for exerting a force on the pin in a direction substantially perpendicular to the first direction in order to press the pin against the sleeve. A method for assembling a female portion of a device for electrical connection to a super-insulating mattress, a super-insulating mattress and a spacecraft.
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公开(公告)号:US10450093B2
公开(公告)日:2019-10-22
申请号:US15743223
申请日:2016-07-07
Applicant: AIRBUS DEFENCE AND SPACE SAS
Inventor: Philippe Cesari , Jacques Cottier , Vincent Claudet
Abstract: A device for electrical connection intended to connect a super-insulating mattress to a structural panel of a spacecraft, said connection device comprising: a conducting sleeve having an axis extending in a first direction, said sleeve comprising a device for axial fastening of the insulating mattress and a support, a conductive pin suitable for being arranged in said sleeve, an elastic element carried by said support, said elastic element being suitable for exerting a force on the pin in a direction substantially perpendicular to the first direction in order to press the pin against the sleeve. A method for assembling a female portion of a device for electrical connection to a super-insulating mattress, a super-insulating mattress and a spacecraft.
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公开(公告)号:US12077324B2
公开(公告)日:2024-09-03
申请号:US17785628
申请日:2020-12-09
Applicant: AIRBUS DEFENCE AND SPACE SAS
Inventor: Catherine Berthomieu , Carole Chossiere , Andrew Walker , Franck Levallois , Vincent Claudet
Abstract: A method for assembling devices on a satellite structure is disclosed including attaching the devices to a first face of a plate drilled with a through-hole provided with a fluid connector, on a second face of the plate, depositing a continuous peripheral bead of polymerisable adhesive composition and depositing a plurality of discontinuous and disjointed inner beads of polymerisable adhesive composition, pressing the second face of the plate against a continuous face of the structure, performing suction so as to create a pressure differential between the plate and the structure, at least partially polymerising the polymerisable adhesive compositions so as to form adhesive joints between the plate and the structure, and interrupting the suction.
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