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91.发明授权公开(公告)号：US12031477B2
公开(公告)日：2024-07-09
申请号：US17533676
申请日：2021-11-23
申请人： The Boeing Company
CPC分类号： F02C1/10 , F01K7/32 , F01K25/103 , F02C6/18 , F05D2220/76 , F05D2220/80
摘要： Methods and apparatus for power generation and/or thermal management on a high speed flight vehicle include circulating a power generation loop working fluid through a power generation loop, which absorbs heat associated with the flight vehicle. A generator operably coupled to the power generation loop generates electrical power. Additionally, a heat transport loop working fluid may circulate through a heat transport loop to provide thermal management through heat transfer.
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公开(公告)号：US12030647B2
公开(公告)日：2024-07-09
申请号：US17675889
申请日：2022-02-18
申请人： The Boeing Company
发明人： Gregory M. Santini , Kevin R. Tsai
摘要： Thermal anti-icing systems are disclosed. An example anti-icing system includes a housing defining an inner recess, a first support fitting, a second support fitting spaced away from the first support fitting. The housing is positioned between the first support fitting and the second support fitting. The first support fitting, the second support fitting and an outer wall of the housing define a heating chamber that is fluidly separated from the inner recess.
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公开(公告)号：US12030637B2
公开(公告)日：2024-07-09
申请号：US17732738
申请日：2022-04-29
申请人： THE BOEING COMPANY
CPC分类号： B64D11/02 , A61G5/1002
摘要： A system configured to transfer an individual between an area and a toilet within a lavatory includes a base, one or more rollers coupled to the base, and a seating assembly coupled to the base. The seating assembly includes a backrest, a toilet overlay seat configured to be disposed over the toilet, and a seat cover that is movable between a covering position over the toilet overlay seat, and a lavatory use position in which the toilet overlay seat is exposed. A counterbalance is coupled to one or both of the base or the seating assembly. The counterbalance is moveable between a stowed position and a deployed position in relation to the toilet.
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公开(公告)号：US12030296B2
公开(公告)日：2024-07-09
申请号：US17931969
申请日：2022-09-14
申请人： The Boeing Company
发明人： Manojkumar Sabanayagam , Harshinder Singh , Mallikarjun Ghasane , Suhasini Lakshmi Darsiv , Ramalakshmi Rajendiran , Ameya Deshpande
CPC分类号： B32B5/26 , B32B5/02 , B32B5/028 , B32B15/02 , B32B15/14 , B64C1/12 , B64C3/26 , B64D45/02 , B32B2255/02 , B32B2255/26 , B32B2262/101 , B32B2262/106 , B32B2307/202 , B32B2307/302 , B32B2307/72 , B32B2307/732 , B32B2605/18
摘要： A lightning strike protection (LSP) apparatus includes a first layer of fiber glass. The LSP apparatus also includes a second layer positioned on the first layer. The second layer includes carbon nanotubes (CNT). The LSP apparatus also includes a third layer positioned on the second layer. The third layer includes a surfacer. The LSP apparatus also includes a fourth layer positioned on the third layer. The fourth layer also includes the fiber glass. The LSP apparatus also includes a fifth layer positioned on the fourth layer. The fifth layer includes a primer. The LSP apparatus also includes a sixth layer positioned on the fifth layer. The sixth layer includes an outer surface material.
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95.发明授权公开(公告)号：US12030262B2
公开(公告)日：2024-07-09
申请号：US17662455
申请日：2022-05-09
申请人： The Boeing Company
CPC分类号： B29C70/342 , B29C70/32 , B29C70/544 , B29L2031/3082
摘要： A rotating manifold includes an axle, a hub rotatable relative to the axle about an axis of rotation, and a compressed air line in fluid communication housed in the axle. The rotating manifold further includes a vacuum line in fluid communication with the hub. The rotating manifold further includes a plurality of conduits connected to the hub. Each conduit of the plurality of conduits is in fluid communication with the vacuum line and houses a compressed air line arm in fluid communication with the compressed air line.
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公开(公告)号：US20240218523A1
公开(公告)日：2024-07-04
申请号：US18605107
申请日：2024-03-14
申请人： THE BOEING COMPANY
IPC分类号： C23F11/16 , B05D1/02 , B05D1/18 , B05D3/02 , B05D3/10 , B05D7/00 , C09D5/00 , C09D5/08 , C09D183/04 , C23F11/04 , C23F11/12
CPC分类号： C23F11/161 , C09D5/002 , C09D5/086 , C09D183/04 , C23F11/04 , C23F11/12 , B05D1/02 , B05D1/18 , B05D3/0254 , B05D3/107 , B05D7/50
摘要： Aspects described herein generally relate to a method of coating a metallic surface. The method includes forming a solution including a corrosion inhibitor having one or more thiol moieties and a hydroxide. The metallic surface is coated with the solution to form a treated metallic surface. The treated metallic surface is further coated with an organosilane, an acid, and a metal alkoxide to form a coating system.
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公开(公告)号：US12025564B2
公开(公告)日：2024-07-02
申请号：US18312873
申请日：2023-05-05
申请人： The Boeing Company
发明人： Morteza Safai
IPC分类号： G01N21/88 , B29C64/371 , B29C64/393 , B33Y10/00 , B33Y30/00 , B33Y50/02 , G01N21/95
CPC分类号： G01N21/8806 , B29C64/371 , B29C64/393 , B33Y10/00 , B33Y30/00 , B33Y50/02 , G01N21/8851 , G01N21/95 , G01N2201/06113 , G01N2201/0627 , G01N2201/0628
摘要： A method for real-time surface imperfection detection for additive manufacturing and 3-D printing parts is provided. The method includes directing a first light radiation using one or more illumination sources, wherein the first light radiation illuminates a target area of a part being manufactured in a uniform chromatic light such that the target area appears to have a substantially uniform monochromatic color; capturing a current image of a second light radiation that is scattered or reflected by the target area using one or more feedback cameras; and analyzing the current image of the second light radiation using at least one of the one or more feedback camera with a previously acquired image to determine whether a surface imperfection exists or does not exist.
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公开(公告)号：US12024288B2
公开(公告)日：2024-07-02
申请号：US17853634
申请日：2022-06-29
申请人： The Boeing Company
发明人： Samuel L. Block
摘要： An underwing flap support mounting structure is disclosed that includes an underwing beam comprising an integral clevis at a forward end of the underwing beam and mounted to a lower skin of a wingbox, wherein the integral clevis comprises a first clevis bore and second clevis bore; and a wingbox lug fitting comprising a wingbox lug and a spherical bearing support assembly carrying a race and a spherical bearing, the wingbox lug having a wingbox lug bore and the spherical bearing having a spherical bearing bore, wherein a forward-aft oriented fuse pin is slidably received in the spherical bearing bore, the first clevis bore, and the second clevis bore to inhibit relative linear-vertical motion of the underwing beam and the integral clevis relative to a wingbox lug fitting that is mounted to the lower skin of the wingbox.
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公开(公告)号：US12023413B2
公开(公告)日：2024-07-02
申请号：US17452560
申请日：2021-10-27
申请人： The Boeing Company
IPC分类号： A61L2/10
CPC分类号： A61L2/10 , A61L2202/11
摘要： Modules, systems and methods that disinfect surfaces using ultraviolet (UV) light are disclosed. In one aspect, a UV light-emitting module comprises an enclosure including an aluminum rear wall comprising a ventilation opening and a face plate spaced from the rear wall and comprising a light-transmitting aperture. Four aluminum sidewalls extend between the rear wall and the face plate, with at least one sidewall comprising a ventilation opening. At least one aluminum UV light emitter support within the enclosure is electrically coupled to plurality of UV light emitters. A thermally conductive and electrically insulating separator is located between the support and the rear wall. At least one electrical conductor extends through the rear wall and the separator into the support, and an electrically insulating bushing extends between the conductor and surfaces of the rear wall.
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公开(公告)号：US20240212512A1
公开(公告)日：2024-06-27
申请号：US18069672
申请日：2022-12-21
申请人： THE BOEING COMPANY
IPC分类号： G08G5/00
CPC分类号： G08G5/006 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/0043 , G08G5/0082
摘要： A method includes obtaining, at a device, source and destination data for one or more upcoming flights through a particular airspace. The method also includes obtaining, at the device, a map of societal impact hotspots associated with traffic through the particular airspace, and generating, based on the map of societal impact hotspots, a set of trajectories for the one or more upcoming flights through the particular airspace.
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