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公开(公告)号：US11038273B1
公开(公告)日：2021-06-15
申请号：US16826338
申请日：2020-03-23
Applicant: THE BOEING COMPANY
Inventor： Lixin Cai , Alec Adams , Manny Urcia
Abstract: An antenna assembly includes a base including one or more feed transitions, a support panel separated from the base, a patch secured to the support panel, and one or more T-shaped probes that couple the feed transition(s) to the patch. The T-shaped probe(s) are separated from the patch.
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公开(公告)号：US12196115B2
公开(公告)日：2025-01-14
申请号：US18458588
申请日：2023-08-30
Applicant: THE BOEING COMPANY
Inventor： Michael Hayes , Keith A. Etling , Jordan Kreitzman , Rehan Milarachi , Manny Urcia , Andrews Guadron
IPC: G10K11/16 , B64D27/00 , B64D33/02 , B64U10/13 , B64U50/12 , F01N1/02 , F02C7/045 , G10K11/172 , B64U30/40 , F02C6/20
Abstract: A flow path duct system for a propulsion system of an aircraft includes a base defining a flow surface. The base has an internal surface and an external surface. A plurality of perforations are formed through the base between the internal surface and the external surface. A plurality of supports define a plurality of cavities. The plurality of supports extend outwardly from the external surface of the of the base. One or more of the plurality of cavities are in fluid communication with the one or more of the plurality of perforations. A backing surface is secured to the plurality of supports. The plurality of supports are disposed between the base and the backing surface. The one or more of the plurality of cavities are in fluid communication with an internal volume defined by the internal surface of the base through the one or more of the plurality of perforations. The base, the plurality of supports, and the backing surface can be integrally formed together as a monolithic, load-bearing structure.
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Patent Agency Ranking
公开(公告)号：US20230407775A1
公开(公告)日：2023-12-21
申请号：US18458588
申请日：2023-08-30
Applicant: THE BOEING COMPANY
Inventor： Michael Hayes , Keith A. Etling , Jordan Kreitzman , Rehan Kaluarachchi , Manny Urcia , Andrews Guadron
IPC: F01N1/02 , B64D27/00 , G10K11/16 , G10K11/172 , F02C7/045
CPC classification number: F01N1/023 , B64D27/00 , G10K11/161 , G10K11/172 , F02C7/045 , F02C6/20
Abstract: A flow path duct system for a propulsion system of an aircraft includes a base defining a flow surface. The base has an internal surface and an external surface. A plurality of perforations are formed through the base between the internal surface and the external surface. A plurality of supports define a plurality of cavities. The plurality of supports extend outwardly from the external surface of the of the base. One or more of the plurality of cavities are in fluid communication with the one or more of the plurality of perforations. A backing surface is secured to the plurality of supports. The plurality of supports are disposed between the base and the backing surface. The one or more of the plurality of cavities are in fluid communication with an internal volume defined by the internal surface of the base through the one or more of the plurality of perforations. The base, the plurality of supports, and the backing surface can be integrally formed together as a monolithic, load-bearing structure.
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公开(公告)号：US11767776B2
公开(公告)日：2023-09-26
申请号：US17321591
申请日：2021-05-17
Applicant: THE BOEING COMPANY
Inventor： Michael Hayes , Keith A. Etling , Jordan Kreitzman , Rehan Kaluarachchi , Manny Urcia , Andrews Guadron
CPC classification number: F01N1/023 , B64D27/00 , F02C7/045 , G10K11/161 , G10K11/172 , B64D2033/0206 , F02C6/20 , F05D2220/323 , F05D2260/963
Abstract: A flow path duct system for a propulsion system of an aircraft includes a base defining a flow surface. The base has an internal surface and an external surface. A plurality of perforations are formed through the base between the internal surface and the external surface. A plurality of supports define a plurality of cavities. The plurality of supports extend outwardly from the external surface of the of the base. One or more of the plurality of cavities are in fluid communication with the one or more of the plurality of perforations. A backing surface is secured to the plurality of supports. The plurality of supports are disposed between the base and the backing surface. The one or more of the plurality of cavities are in fluid communication with an internal volume defined by the internal surface of the base through the one or more of the plurality of perforations. The base, the plurality of supports, and the backing surface can be integrally formed together as a monolithic, load-bearing structure.
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公开(公告)号：US20210206139A1
公开(公告)日：2021-07-08
申请号：US16733383
申请日：2020-01-03
Applicant: The Boeing Company
Inventor： Scott Johnston , Manny Urcia
Abstract: A composite member that includes plies of composite material and an integral antenna. The integral antenna includes one or more plies of conductive material. A pin is connected to and extends outward from one of the conductive plies. The pin extends through openings in one or more of the composite plies that are positioned between and/or around the one or more plies of conductive material.
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公开(公告)号：US20220074329A1
公开(公告)日：2022-03-10
申请号：US17321591
申请日：2021-05-17
Applicant: THE BOEING COMPANY
Inventor： Michael Hayes , Keith A. Etling , Jordan Kreitzman , Rehan Kaluarachchi , Manny Urcia , Andrews Guadron
IPC: F01N1/02 , B64D27/00 , G10K11/16 , G10K11/172
Abstract: A flow path duct system for a propulsion system of an aircraft includes a base defining a flow surface. The base has an internal surface and an external surface. A plurality of perforations are formed through the base between the internal surface and the external surface. A plurality of supports define a plurality of cavities. The plurality of supports extend outwardly from the external surface of the of the base. One or more of the plurality of cavities are in fluid communication with the one or more of the plurality of perforations. A backing surface is secured to the plurality of supports. The plurality of supports are disposed between the base and the backing surface. The one or more of the plurality of cavities are in fluid communication with an internal volume defined by the internal surface of the base through the one or more of the plurality of perforations. The base, the plurality of supports, and the backing surface can be integrally formed together as a monolithic, load-bearing structure.
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公开(公告)号：US11207866B2
公开(公告)日：2021-12-28
申请号：US16733383
申请日：2020-01-03
Applicant: The Boeing Company
Inventor： Scott Johnston , Manny Urcia
Abstract: A composite member that includes plies of composite material and an integral antenna. The integral antenna includes one or more plies of conductive material. A pin is connected to and extends outward from one of the conductive plies. The pin extends through openings in one or more of the composite plies that are positioned between and/or around the one or more plies of conductive material.
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