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公开(公告)号:US12073955B2
公开(公告)日:2024-08-27
申请号:US16883629
申请日:2020-05-26
Applicant: THE BOEING COMPANY
Inventor: Patrick J. Kinlen , Daniel A. Charles
IPC: H01B1/12 , B32B27/08 , B64D45/02 , C09D5/24 , C09D7/40 , C09D7/61 , C09D7/62 , C09D125/18 , C09D133/00 , C09D153/00 , C09D163/00 , C09D165/00 , C09D175/04 , C09D179/02 , H01B1/04
CPC classification number: H01B1/124 , B32B27/08 , B64D45/02 , C09D5/24 , C09D7/61 , C09D7/62 , C09D7/70 , C09D125/18 , C09D133/00 , C09D153/00 , C09D163/00 , C09D165/00 , C09D175/04 , C09D179/02 , H01B1/04 , H01B1/127 , H01B1/128 , B32B2264/108 , B32B2307/302 , B32B2313/04
Abstract: Methods of forming an electrically conductive carbon allotrope material comprise depositing a first material comprising a polymer and a sulfonic acid onto a carbon allotrope material to form a second material. The methods comprise curing the second material. Methods of heating a surface of a vehicle component comprise applying a voltage to a material comprising a carbon allotrope material, a polymer, and a sulfonic acid. The material is disposed on a surface of a vehicle component. Electrically conductive materials comprise at least one polymer, at least one sulfonic acid, and a carbon allotrope material.
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公开(公告)号:US11117336B2
公开(公告)日:2021-09-14
申请号:US16837226
申请日:2020-04-01
Applicant: The Boeing Company
Inventor: Alex X. Zhu , Daniel A. Charles
IPC: B29C73/10 , B29C73/12 , B29C35/16 , B29C73/24 , B29C65/24 , B32B27/00 , B32B37/06 , F28F7/02 , B29C73/34 , B29K101/10 , B29K105/24 , B29K105/00 , B29L9/00 , B29L31/30
Abstract: A method is provided for managing the temperature of heat sensitive material located near a repair patch being thermally cured on a composite skin using a heating blanket. The method comprises configuring an assembly of thermally conductive cooling blocks to fit within a space between the heating blanket and the heat sensitive material. The assembly of thermally conductive cooling blocks is then installed against the skin within the space, forming a heat sink that conducts a portion of heat out of the composite skin away from the heat sensitive material.
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公开(公告)号:US10685761B2
公开(公告)日:2020-06-16
申请号:US15252072
申请日:2016-08-30
Applicant: THE BOEING COMPANY
Inventor: Patrick J. Kinlen , Daniel A. Charles
IPC: H01B1/12 , B32B27/08 , C09D7/61 , C09D7/40 , C09D7/62 , B64D45/02 , C09D5/24 , C09D125/18 , C09D133/00 , C09D153/00 , C09D163/00 , C09D165/00 , C09D175/04 , C09D179/02 , H01B1/04
Abstract: Methods of forming an electrically conductive carbon allotrope material comprise depositing a first material comprising a polymer and a sulfonic acid onto a carbon allotrope material to form a second material. The methods comprise curing the second material. Methods of heating a surface of a vehicle component comprise applying a voltage to a material comprising a carbon allotrope material, a polymer, and a sulfonic acid. The material is disposed on a surface of a vehicle component. Electrically conductive materials comprise at least one polymer, at least one sulfonic acid, and a carbon allotrope material.
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公开(公告)号:US20200223163A1
公开(公告)日:2020-07-16
申请号:US16837226
申请日:2020-04-01
Applicant: The Boeing Company
Inventor: Alex X. Zhu , Daniel A. Charles
Abstract: A method is provided for managing the temperature of heat sensitive material located near a repair patch being thermally cured on a composite skin using a heating blanket. The method comprises configuring an assembly of thermally conductive cooling blocks to fit within a space between the heating blanket and the heat sensitive material. The assembly of thermally conductive cooling blocks is then installed against the skin within the space, forming a heat sink that conducts a portion of heat out of the composite skin away from the heat sensitive material.
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公开(公告)号:US20180147800A1
公开(公告)日:2018-05-31
申请号:US15365215
申请日:2016-11-30
Applicant: The Boeing Company
Inventor: Alex X. Zhu , Daniel A. Charles
CPC classification number: B29C73/12 , B29C35/16 , B29C65/242 , B29C73/24 , B29C73/34 , B29K2101/10 , B29K2105/246 , B29K2105/253 , B29L2009/00 , B29L2031/3076 , B32B27/00 , B32B37/06 , B32B2305/77 , B32B2309/02 , B32B2398/10 , B32B2605/18 , F28F7/02
Abstract: An assembly of thermally conductive cooling blocks is configured to be placed against a composite skin between a heating blanket used to thermally cure a composite repair patch and a structure formed of a heat sensitive material. The cooling block assembly conducts heat away from the skin to prevent overheating of the heat sensitive material.
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