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公开(公告)号：US20230040229A1
公开(公告)日：2023-02-09
申请号：US17788578
申请日：2020-12-23
发明人： Andrew WALKER
摘要： A support structure for a spacecraft is disclosed having a first side wall, a second side wall which is parallel to and opposite the first side wall, a third side wall attached to at least the first side wall, and a fourth side wall which is parallel to and opposite the third side wall; at least one interior panel attached between and perpendicular to the first side wall and to the second side wall, at least one first thermal coupling device bearing against the second side wall and attached to the interior panel, electronic devices arranged on and in direct thermal contact with at least a portion of the first thermal coupling device.
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公开(公告)号：US20180237168A1
公开(公告)日：2018-08-23
申请号：US15750980
申请日：2016-08-10
发明人： Philippe CAEL , Andrew WALKER , Fabrice MENA
CPC分类号： B64G1/1007 , B64G1/10 , B64G1/226 , B64G1/44 , B64G1/503 , B64G2001/1092
摘要： Disclosed is an artificial satellite including one face from the North face and the South face supporting at least one main radiator having an outer face turned towards space and an inner face opposite the outer face. The satellite includes a bearing structure carrying the North face, the South face, the East face and the West face. At least one part of the at least one main radiator protrudes from at least one face from the East face and the West face. The inner face of the at least one protruding part is covered with a high infrared emissivity material. The value of the dimension of the at least one protruding part is between 19% and 50% of the value of the distance between the East and West faces.
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3.发明申请公开(公告)号：US20180320983A1
公开(公告)日：2018-11-08
申请号：US15772444
申请日：2016-11-16
摘要： Disclosed is a heat exchange device for effecting a heat exchange between a heat transfer fluid of a first network of capillary heat pipes and a heat transfer fluid of a second network of capillary heat pipes. The heat exchange device includes a solid block provided with a first channel and a second channel which are independent of one another, the first channel having at least one opening intended to be connected to a capillary heat pipe of the first network, the second channel having at least one opening intended to be connected to a capillary heat pipe of the second network, the first channel having a portion which lies near a portion of the second channel such that the heat transfer fluid of the first network is able to exchange heat with the heat transfer fluid of the second network via the heat exchanging portions.
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公开(公告)号：US20230050562A1
公开(公告)日：2023-02-16
申请号：US17785628
申请日：2020-12-09
摘要： 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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公开(公告)号：US20200232716A1
公开(公告)日：2020-07-23
申请号：US16486853
申请日：2018-03-13
发明人： Andrew WALKER
摘要： A heat transfer device is disclosed having a housing including a first main wall and a second main wall, the housing having a sealed internal cavity, a liquid contained in the internal cavity, and a mixer able to set the liquid in motion, the heat transfer device being able to be switched between a first state and a second state in which the liquid is in motion and transfers heat by convection between the first main wall and the second main wall, the thermal conductance between the first main wall and the second main wall in the first state being four times less than the thermal conductance between the first main wall and the second main wall in the second state.
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公开(公告)号：US20180079534A1
公开(公告)日：2018-03-22
申请号：US15565703
申请日：2016-06-01
发明人： Andrew WALKER
摘要： Disclosed is an artificial satellite including a battery pack capable of dissipating heat, at least one radiator capable of conveying the heat dissipated by the battery pack into space, and a low-dissipation equipment item having an individual power flux density of less than 250 watts/m2. The satellite includes a thermally insulating cover delimiting, together with the radiator, an interior isothermal zone in which thermal control takes place by radiation, the battery pack and the low-dissipation equipment being arranged in thermally insulating cover. The battery pack has an operating range of between 0° C. and 50° C. and preferably of between 10° C. and 30° C.
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