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公开(公告)号：US10730645B2
公开(公告)日：2020-08-04
申请号：US15494315
申请日：2017-04-21
Applicant: THE BOEING COMPANY
Inventor： Eric S. Mindock , James H. Mabe , Frederick Theodore Calkins , Abraham Naroll Gissen , Miguel A. Estevez
IPC: H05K7/20 , F28F13/00 , F28F21/00 , B64G1/50 , F28D21/00 , H01L23/427 , H01L23/42 , H01L23/373
Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.
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公开(公告)号：US11718424B2
公开(公告)日：2023-08-08
申请号：US16387204
申请日：2019-04-17
Applicant: The Boeing Company
CPC classification number: B64G1/58 , H05B3/0014 , H05B3/145 , H05B3/34 , H05B2203/011 , H05B2214/04
Abstract: Protective blankets comprise a flexible blanket body and a voltage supply. The flexible blanket body comprises a plurality of sheets of material operatively coupled together to define the flexible blanket body. The plurality of sheets comprises one or more sheets composed at least in part of a carbon nanotube material and at least one sheet composed of a different material. The voltage supply is electrically coupled at least to a first sheet of the one or more sheets composed at least in part of the carbon nanotube material, such that the first sheet defines a resistive heater.
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公开(公告)号：US20200331639A1
公开(公告)日：2020-10-22
申请号：US16913855
申请日：2020-06-26
Applicant: THE BOEING COMPANY
Inventor： Eric S. Mindock , James H. Mabe , Frederick Theodore Calkins , Abraham NaroII Gissen , Miguel A. Estevez
IPC: B64G1/50 , F28D21/00 , H05K7/20 , H01L23/427 , H01L23/42 , F28F13/00 , H01L23/373
Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.
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Patent Agency Ranking
公开(公告)号：US20180305043A1
公开(公告)日：2018-10-25
申请号：US15494315
申请日：2017-04-21
Applicant: THE BOEING COMPANY
Inventor： Eric S. Mindock , James H. Mabe , Frederick Theodore Calkins , Abraham NaroII Gissen , Miguel A. Estevez
Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.
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公开(公告)号：US11225339B2
公开(公告)日：2022-01-18
申请号：US16913855
申请日：2020-06-26
Applicant: THE BOEING COMPANY
Inventor： Eric S. Mindock , James H. Mabe , Frederick Theodore Calkins , Abraham Naroll Gissen , Miguel A. Estevez
IPC: H05K7/20 , B64G1/50 , F28D21/00 , H01L23/427 , H01L23/42 , F28F13/00 , H01L23/373
Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.
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公开(公告)号：US20200331640A1
公开(公告)日：2020-10-22
申请号：US16387204
申请日：2019-04-17
Applicant: The Boeing Company
Abstract: Protective blankets comprise a flexible blanket body and a voltage supply. The flexible blanket body comprises a plurality of sheets of material operatively coupled together to define the flexible blanket body. The plurality of sheets comprises one or more sheets composed at least in part of a carbon nanotube material and at least one sheet composed of a different material. The voltage supply is electrically coupled at least to a first sheet of the one or more sheets composed at least in part of the carbon nanotube material, such that the first sheet defines a resistive heater.
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公开(公告)号：US10265930B2
公开(公告)日：2019-04-23
申请号：US14595019
申请日：2015-01-12
Applicant: The Boeing Company
Inventor： Richard W. Aston , Anna Maria Tomzynska , Eric S. Mindock
IPC: B32B5/00 , B32B5/26 , B32B37/16 , B32B5/02 , B32B5/06 , B32B15/14 , B64G1/52 , B64G1/54 , B64G1/56
Abstract: Protective blankets include a plurality of sheets of material operatively coupled together to define the protective blanket. The plurality of sheets includes at least one sheet composed of carbon nanotube reinforced composite material and at least one sheet composed of a different material. Methods of assembling protective blankets include layering the plurality of sheets and operatively coupling together the plurality of sheets. Spacecraft include a body and a protective blanket operatively coupled to the body. Methods of assembling spacecraft include coupling a protective blanket to the body of a spacecraft.
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公开(公告)号：US20160200460A1
公开(公告)日：2016-07-14
申请号：US14595019
申请日：2015-01-12
Applicant: The Boeing Company
Inventor： Richard W. Aston , Anna Maria Tomzynska , Eric S. Mindock
CPC classification number: B32B5/26 , B32B5/024 , B32B5/028 , B32B5/06 , B32B15/14 , B32B37/16 , B32B2260/021 , B32B2260/023 , B32B2260/046 , B32B2262/02 , B32B2262/0269 , B32B2262/106 , B32B2264/108 , B32B2307/212 , B32B2307/304 , B32B2307/558 , B32B2571/00 , B64G1/52 , B64G1/546 , B64G1/56
Abstract: Protective blankets include a plurality of sheets of material operatively coupled together to define the protective blanket. The plurality of sheets includes at least one sheet composed of carbon nanotube reinforced composite material and at least one sheet composed of a different material. Methods of assembling protective blankets include layering the plurality of sheets and operatively coupling together the plurality of sheets. Spacecraft include a body and a protective blanket operatively coupled to the body. Methods of assembling spacecraft include coupling a protective blanket to the body of a spacecraft.
Abstract translation: 保护毯包括多个可操作地联接在一起以限定保护毯的材料。 多个片材包括由碳纳米管增强复合材料构成的至少一个片材和由不同材料构成的至少一个片材。 组装保护性毯子的方法包括层叠多个片材并且可操作地将多个片材组合在一起。 航天器包括可操作地耦合到身体的身体和保护毯。 组装航天器的方法包括将保护毯连接到航天器的身体。
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