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公开(公告)号：US20190016438A1
公开(公告)日：2019-01-17
申请号：US15647475
申请日：2017-07-12
Applicant: THE BOEING COMPANY
Inventor： Keith D. Humfeld , Scott D. Hartshorn
CPC classification number: B64C3/20 , B29C70/06 , B29C70/30 , B29D24/008 , B29D99/0014 , B29L2031/3085 , B32B5/26 , B32B2305/073 , B32B2305/076 , B32B2605/18 , B64C3/26
Abstract: An apparatus includes a first composite support structure and a second composite support structure. The first and second composite support structures are in a predetermined position relative to one another. The apparatus further includes an uncured pre-preg ply, wherein: the uncured pre-preg ply overlies at least a portion of the first composite support structure; the uncured pre-preg ply overlies at least a portion of the second composite support structure; and the first and second composite support structures are each stiffer than the uncured pre-preg ply.
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公开(公告)号：US20180313272A1
公开(公告)日：2018-11-01
申请号：US15582010
申请日：2017-04-28
Applicant: The Boeing Company
Inventor： Scott D. Hartshorn , Keith D. Humfeld
Abstract: Multi-layer thermal insulator apparatus and methods are described. An example multi-layer thermal insulator includes a first thermally insulating layer, a second thermally insulating layer, and a thermally conductive layer positioned between and adjacent to the first thermally insulating layer and the second thermally insulating layer.
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公开(公告)号：US11085116B2
公开(公告)日：2021-08-10
申请号：US15465995
申请日：2017-03-22
Applicant: The Boeing Company
Inventor： Scott D. Hartshorn , Keith D. Humfeld
Abstract: An engine shaft assembly for an engine is provided. The engine shaft assembly includes a shaft and a thermal distribution layer. The thermal distribution layer is provided on the shaft, and is configured to minimize the effect of distortion of the shaft caused by asymmetric cooling on shutdown of the engine.
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公开(公告)号：US10781753B2
公开(公告)日：2020-09-22
申请号：US15582010
申请日：2017-04-28
Applicant: The Boeing Company
Inventor： Scott D. Hartshorn , Keith D. Humfeld
Abstract: Multi-layer thermal insulator apparatus and methods are described. An example multi-layer thermal insulator includes a first thermally insulating layer, a second thermally insulating layer, and a thermally conductive layer positioned between and adjacent to the first thermally insulating layer and the second thermally insulating layer.
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公开(公告)号：US20190085218A1
公开(公告)日：2019-03-21
申请号：US15705566
申请日：2017-09-15
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , Scott D. Hartshorn
Abstract: An adhesive system (100) for attachment to a contact surface (122) of an object (120) comprises a backing (110), carbon nanotubes (130), charged nanoparticles (150), and an electrical source (160). The carbon nanotubes (130) each have a first end region (132) and a second end region (134), opposite the first end region (132). Each of the charged nanoparticles (150) is coupled to the second end region (134) of at least one of the carbon nanotubes (130). The electrical source (160) is configured to selectively electrically charge the backing (110) to cause an electrical repulsion force between the backing (110) and the charged nanoparticles (150). The first end region (132) of each of the carbon nanotubes (130) is coupled to the backing (110). The second end region (134) of each of a number of the carbon nanotubes (130) is coupled to none of the charged nanoparticles (150).
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Patent Agency Ranking
公开(公告)号：US11073707B2
公开(公告)日：2021-07-27
申请号：US15805943
申请日：2017-11-07
Applicant: The Boeing Company
Inventor： Scott D. Hartshorn , Keith Daniel Humfeld
Abstract: A dimmable window apparatus is provided. The dimmable window apparatus includes a window including a first linear polarizing film and a second linear polarizing film, the first linear polarizing film and the second linear polarizing film having respectively a first axis of polarization and a second axis of polarization, the second axis of polarization being electronically-controllable. The apparatus further includes a processor coupled to the second linear polarizing film, and configured to control the second axis of polarization to thereby control the opacity of the window that is defined by the first axis of polarization and the second axis of polarization relative to one another.
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公开(公告)号：US10882629B2
公开(公告)日：2021-01-05
申请号：US16057339
申请日：2018-08-07
Applicant: The Boeing Company
Inventor： Scott D. Hartshorn , Christopher E. Hullman
Abstract: An aircraft propulsor that includes a load bearing moveable panel is described herein. In one example, the moveable panel can be coupled to a propulsor structure to receive loads from the propulsor structure. Such loads can include roll and/or torque loads generated by rotation of a core engine of the aircraft propulsor. The moveable panel can be coupled to the propulsor structure through a plurality of coupling portions on one or both of the moveable panel and the propulsor structure.
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公开(公告)号：US10240070B1
公开(公告)日：2019-03-26
申请号：US15705566
申请日：2017-09-15
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , Scott D. Hartshorn
Abstract: An adhesive system for attachment to a contact surface of an object comprises a backing, carbon nanotubes, charged nanoparticles, and an electrical source. The carbon nanotubes each have a first end region and a second end region, opposite the first end region. Each of the charged nanoparticles is coupled to the second end region of at least one of the carbon nanotubes. The electrical source is configured to selectively electrically charge the backing to cause an electrical repulsion force between the backing and the charged nanoparticles. The first end region of each of the carbon nanotubes is coupled to the backing. The second end region of each of a number of the carbon nanotubes is coupled to none of the charged nanoparticles.
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公开(公告)号：US20180299411A1
公开(公告)日：2018-10-18
申请号：US15485757
申请日：2017-04-12
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , Scott D. Hartshorn
Abstract: A method and system for inspecting a structure. The method may comprise sending a pulsed wave signal into the structure from a transmitter array. The method may detect a response signal in response to sending the pulsed wave signal into the structure at a group of receivers in a receiver array. The method may identify a group of time delays between sending the pulsed wave signal and may detect the response signal generated in response to the pulsed wave signal at the group of receivers. The method may identify a group of intensities for the response signal detected at the group of receivers. The method may determine a distance to a reflector within the structure using the group of time delays and the group of intensities.
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公开(公告)号：US10752336B2
公开(公告)日：2020-08-25
申请号：US15647475
申请日：2017-07-12
Applicant: THE BOEING COMPANY
Inventor： Keith D. Humfeld , Scott D. Hartshorn
Abstract: An apparatus includes a first composite support structure and a second composite support structure. The first and second composite support structures are in a predetermined position relative to one another. The apparatus further includes an uncured pre-preg ply, wherein: the uncured pre-preg ply overlies at least a portion of the first composite support structure; the uncured pre-preg ply overlies at least a portion of the second composite support structure; and the first and second composite support structures are each stiffer than the uncured pre-preg ply.
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