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1.
公开(公告)号:US20230365274A1
公开(公告)日:2023-11-16
申请号:US18348900
申请日:2023-07-07
Applicant: The Boeing Company
Inventor: Keith Daniel Humfeld , Joseph Andrew Bolton
IPC: B64F5/10 , B29C70/54 , B64C3/26 , B29L31/30 , B29K307/04 , B29K63/00 , B23K101/00
CPC classification number: B64F5/10 , B29C70/545 , B64C3/26 , B29L2031/3085 , B29K2307/04 , B29K2063/00 , B23K2101/006 , B29C2793/0009
Abstract: Methods for machining a composite material substrate are discloses comprising integrating a predetermined pattern area having a disbond material for the purpose of creating a disbond region into the composite material substrate at a predetermined thickness, detecting the disbond region and forming a plurality of recesses in the composite material substrate by removing a machined plug from the composite material substrate to form recesses positioned at locations corresponding to the predetermined pattern area, and composite components comprising the recesses machined according to such methods.
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2.
公开(公告)号:US11724823B2
公开(公告)日:2023-08-15
申请号:US16658459
申请日:2019-10-21
Applicant: The Boeing Company
Inventor: Keith Daniel Humfeld , Joseph Andrew Bolton
IPC: B64F5/00 , B29C70/00 , B64F5/10 , B29C70/54 , B64C3/26 , B23K101/00 , B29K63/00 , B29K307/04 , B29L31/30
CPC classification number: B64F5/10 , B29C70/545 , B64C3/26 , B23K2101/006 , B29C2793/0009 , B29K2063/00 , B29K2307/04 , B29L2031/3085
Abstract: Methods for machining a composite material substrate are discloses comprising integrating a predetermined pattern area having a disbond material for the purpose of creating a disbond region into the composite material substrate at a predetermined thickness, detecting the disbond region and forming a plurality of recesses in the composite material substrate by removing a machined plug from the composite material substrate to form recesses positioned at locations corresponding to the predetermined pattern area, and composite components comprising the recesses machined according to such methods.
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公开(公告)号:US10782481B1
公开(公告)日:2020-09-22
申请号:US16351928
申请日:2019-03-13
Applicant: THE BOEING COMPANY
Inventor: Joseph Andrew Bolton , Keith Daniel Humfeld
Abstract: A fastener includes a head that is configured to be engaged by a tool, and a shaft extending from the head. The shaft includes a distal end that is opposite from the head. At least one optical component is coupled to one or both of the head or the shaft. The optical component(s) is configured to allow light to pass through the fastener. A window system includes a panel that includes an exterior surface and an interior surface, and the fastener extending between the exterior surface and the interior surface of the panel. A screen is coupled to the interior surface. The screen receives light from the optical component(s) of the fastener.
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公开(公告)号:US20200292760A1
公开(公告)日:2020-09-17
申请号:US16351928
申请日:2019-03-13
Applicant: THE BOEING COMPANY
Inventor: Joseph Andrew Bolton , Keith Daniel Humfeld
Abstract: A fastener includes a head that is configured to be engaged by a tool, and a shaft extending from the head. The shaft includes a distal end that is opposite from the head. At least one optical component is coupled to one or both of the head or the shaft. The optical component(s) is configured to allow light to pass through the fastener. A window system includes a panel that includes an exterior surface and an interior surface, and the fastener extending between the exterior surface and the interior surface of the panel. A screen is coupled to the interior surface. The screen receives light from the optical component(s) of the fastener.
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5.
公开(公告)号:US20200218861A1
公开(公告)日:2020-07-09
申请号:US16239096
申请日:2019-01-03
Applicant: THE BOEING COMPANY
Inventor: Joseph Andrew Bolton , Keith Daniel Humfeld
IPC: G06K7/10 , H01Q1/22 , H01Q9/06 , G06K19/077
Abstract: A radio-frequency identification (“RFID”) device includes a substrate and a load formed in the substrate, where the load includes at least one microchannel and at least one body of fusible metal contained within the at least one microchannel. The RFID device also includes an antenna electrically connected to the load, and a protective layer covering at least a portion of the substrate.
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公开(公告)号:US20200061947A1
公开(公告)日:2020-02-27
申请号:US16113987
申请日:2018-08-27
Applicant: The Boeing Company
Inventor: Keith Daniel Humfeld , Joseph Andrew Bolton
Abstract: A composite structure forming system configured to form a contoured elongate composite structure in a continuous process is presented. The composite structure forming system comprises a plurality of charge forming stations and a plurality of conveyor systems. The plurality of charge forming stations is configured to operate in parallel, each charge forming station of the plurality of charge forming stations is configured to form a respective composite charge of the contoured elongate composite structure. Each conveyor system of the plurality of conveyor systems is configured to transport a respective composite charge through a respective charge forming station.
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公开(公告)号:US11235359B2
公开(公告)日:2022-02-01
申请号:US16272561
申请日:2019-02-11
Applicant: The Boeing Company
Inventor: Joseph Andrew Bolton , Keith Daniel Humfeld
IPC: B08B7/00 , B23K26/361 , A47L7/00 , B23K26/40 , B23K101/34
Abstract: Methods, systems, and apparatuses are disclosed for the selective and controlled removal of debris from specific areas of a substrate outer surface without adversely impacting the substrate outer surface, including substrate outer surface coatings, and returning an actual substrate outer surface profile containing affixed debris to a predetermined substrate outer surface profile by comparing a library of predetermined profiles to an actual substrate outer surface profile in real time.
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公开(公告)号:US11220321B2
公开(公告)日:2022-01-11
申请号:US16351949
申请日:2019-03-13
Applicant: THE BOEING COMPANY
Inventor: Joseph Andrew Bolton , Keith Daniel Humfeld
IPC: G02B6/32 , B64C1/14 , F16B5/00 , G02B6/26 , G02B6/42 , F16B35/00 , F16B33/00 , F16B19/04 , F16B15/00
Abstract: A fastener includes a head that is configured to be engaged by a tool, and a shaft extending from the head. The shaft includes a distal end that is opposite from the head. At least one optical component is coupled to one or both of the head or the shaft. The optical component(s) is configured to allow light to pass through the fastener. A window system includes a panel that includes an exterior surface and an interior surface, and the fastener extending between the exterior surface and the interior surface of the panel. A screen is coupled to the interior surface. The screen receives light from the optical component(s) of the fastener.
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9.
公开(公告)号:US20210114749A1
公开(公告)日:2021-04-22
申请号:US16658459
申请日:2019-10-21
Applicant: The Boeing Company
Inventor: Keith Daniel Humfeld , Joseph Andrew Bolton
Abstract: Methods for machining a composite material substrate are discloses comprising integrating a predetermined pattern area having a disbond material for the purpose of creating a disbond region into the composite material substrate at a predetermined thickness, detecting the disbond region and forming a plurality of recesses in the composite material substrate by removing a machined plug from the composite material substrate to form recesses positioned at locations corresponding to the predetermined pattern area, and composite components comprising the recesses machined according to such methods.
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公开(公告)号:US20200290717A1
公开(公告)日:2020-09-17
申请号:US16351949
申请日:2019-03-13
Applicant: THE BOEING COMPANY
Inventor: Joseph Andrew Bolton , Keith Daniel Humfeld
Abstract: A fastener includes a head that is configured to be engaged by a tool, and a shaft extending from the head. The shaft includes a distal end that is opposite from the head. At least one optical component is coupled to one or both of the head or the shaft. The optical component(s) is configured to allow light to pass through the fastener. A window system includes a panel that includes an exterior surface and an interior surface, and the fastener extending between the exterior surface and the interior surface of the panel. A screen is coupled to the interior surface. The screen receives light from the optical component(s) of the fastener.
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