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公开(公告)号：US11414220B2
公开(公告)日：2022-08-16
申请号：US16080213
申请日：2017-02-01
发明人： Hiroki Izu , Yuichi Ogura , Takehide Nomura , Kengo Hayashi , Shintaro Yamashita , Shiro Sakata , Tetsuya Kitagawa
摘要： Inner panels including at least one built-in heat pipe connected in a circumferential direction are provided. In a heat pipe panel including the built-in heat pipe, apparatuses are mounted on the outer side of the plural inner panels connected in the circumferential direction to diffuse generated heat of the apparatuses to the circumferential direction of the inner panels. Webbed panels including a built-in heat pipe horizontally arranged and having heat radiation surfaces are radially arranged at corners of the inner panels as well as a heat pipe is horizontally built in and heat radiation surfaces are arranged also on outer panels facing the inner panels to thermally connect the heat pipes to one another.
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公开(公告)号：US20220127021A1
公开(公告)日：2022-04-28
申请号：US17471138
申请日：2021-09-09
申请人： L'Garde, Inc.
摘要： A solar sail includes a bus and a plurality of separate movable vanes coupled to the bus. Each movable vane includes a reflective surface for generating solar radiation pressure and propel the solar sail in space. Each vane may be movable relative to the bus in a fully deployed configuration such that an amount of thrust generated by solar radiation pressure on each vane is controllable.
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113.发明授权公开(公告)号：US11273900B2
公开(公告)日：2022-03-15
申请号：US16905008
申请日：2020-06-18
申请人： The Boeing Company
发明人： Edward V. White
IPC分类号： B64C1/40 , B64C3/18 , B64C3/36 , B32B5/24 , B64G1/50 , B64D13/00 , F28F13/14 , B64C1/00 , B64C3/26 , B64C13/50 , B64C9/00 , B32B5/02 , B64C1/38 , F28F13/00
摘要： A thermal management system for transferring heat from a heat load includes a composite structural member that supports a heat load source and a heat transfer member in thermal contact with the composite structural member, and in thermal contact with a heat sink. The system further includes at least one thermally-conductive first fastener that is in thermal contact with the heat transfer member, couples the heat load source to the composite structural member, and conducts heat from the heat load source into the heat transfer member. The heat transfer member conducts heat from the thermally-conductive first fastener to the heat sink.
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公开(公告)号：US20220073217A1
公开(公告)日：2022-03-10
申请号：US17447358
申请日：2021-09-10
IPC分类号： B64G1/50
摘要： A method includes coupling a radiator panel assembly to a component, and conducting heat from the component via a thermally conductive hinge into at least one base radiator panel in the radiator panel assembly. The method further includes placing the at least one base radiator panel in a position to radiate a fraction of the heat into space through a surface of the at least one base radiator panel, and dynamically varying the position of the at least one base radiator panel to vary an amount of heat loss through the at least one base radiator panel to regulate a temperature of the component.
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公开(公告)号：US11254452B2
公开(公告)日：2022-02-22
申请号：US16448215
申请日：2019-06-21
发明人： Fabrice Mena , Bruin Benthem
摘要： A radiative fin for a spacecraft is disclosed having an end fitting of heat conductive material, configured to be mounted on the spacecraft, a flexible radiative laminate, connected to the end fitting at one end and having an opposite free end, at least one pyrolytic graphite sheet, and at least one heat emission layer in contact with the pyrolythic graphite sheet on at least part of the surface of the pyrolythic graphite sheet, and a flexible rod, extending from the end fitting along at least part of a side of the flexible radiative laminate and being affixed to the latter. The flexible rod is adapted to occupy a folded position and a deployed position and to exert, while in the folded position, a deployment torque adapted to bring the flexible rod back to the deployed position.
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公开(公告)号：US11142348B2
公开(公告)日：2021-10-12
申请号：US16095939
申请日：2017-05-05
申请人： L'Garde, Inc.
摘要： A solar sail includes a bus and a plurality of separate movable vanes coupled to the bus. Each movable vane includes a reflective surface for generating solar radiation pressure and propel the solar sail in space. Each vane may be movable relative to the bus in a fully deployed configuration such that an amount of thrust generated by solar radiation pressure on each vane is controllable.
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公开(公告)号：US11009297B2
公开(公告)日：2021-05-18
申请号：US14687640
申请日：2015-04-15
摘要： A passive thermal system for use in aerospace vehicles includes a plurality of core-bearing radiator panels having at least one heat pipe embedded therein. The portion of the heat pipe embedded in each panel is fluidically coupled to the portions of the heat pipe in the other core-bearing radiator panels.
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公开(公告)号：US10899477B2
公开(公告)日：2021-01-26
申请号：US15227630
申请日：2016-08-03
申请人： MADE IN SPACE, INC.
发明人： Michael Snyder
IPC分类号： H01Q17/00 , B64G1/10 , B33Y40/00 , B33Y10/00 , B33Y30/00 , B33Y80/00 , B33Y50/02 , B33Y70/00 , B22F3/105 , B23K5/18 , B23K9/04 , B23K11/00 , B29C64/386 , B23K15/00 , B23K26/342 , B23K37/04 , B29C64/106 , B23K10/02 , B64G1/66 , B64G1/52 , B64G1/26 , B64G1/50 , B64G4/00 , B64G99/00 , B29L31/30
摘要： A system for producing an object is disclosed including a build device having a build area and a material bonding component to receive portions of a material that are used to produce the object, at least one gripper within the build area to contact the object to provide support and to provide for at least one of a heat sink for the object, a cold sink for the object, and electrical dissipation path from the object, and a movement mechanism to move the build device relative to the object to position the build device at a position to further produce the object. Another system and methods are also disclosed.
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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：US20200062428A1
公开(公告)日：2020-02-27
申请号：US16111052
申请日：2018-08-23
申请人： The Boeing Company
摘要： Systems, methods, and devices are disclosed for implementing habitation support appliances. Devices may include a housing defining an internal volume, the housing having an inner surface and an outer surface, the inner surface including a helical groove. Devices may also include a front plate coupled to a first end of the housing, an end plate coupled to a second end of the housing, the front plate and the end plate being configured to seal the internal volume, a thermal loop coupled to the outer surface of the housing, the thermal loop configured to transfer thermal energy with the housing and the internal volume, and a mixing device configured to be positioned within the internal volume, and configured to be moved along the helical groove of the inner surface.
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