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1.
公开(公告)号:US20240026164A1
公开(公告)日:2024-01-25
申请号:US17870041
申请日:2022-07-21
Applicant: The Boeing Company
Inventor: Melinda D. Miller , Patrice K. Ackerman , Jason A. Bolles
Abstract: Co-curable and co-cured UV/visible light-resistant composite material assemblies comprising a co-curable UV/visible light-resistant lightning strike protection layer are disclosed that can facilitate and streamline manufacture of composite material assemblies and sub-assemblies, including exterior assemblies and sub-assemblies for aircraft, vehicles, and objects exposed to electromagnetic effects including lightning strikes.
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2.
公开(公告)号:US20230391063A1
公开(公告)日:2023-12-07
申请号:US18171474
申请日:2023-02-24
Applicant: The Boeing Company
Inventor: Patrice K. Ackerman , Melinda D. Miller , Jason A. Bolles
CPC classification number: C08J5/042 , B64C3/20 , C08J5/243 , C08J2363/00
Abstract: Co-curable and co-cured UV/visible light-resistant composite materials are disclosed with UV/visible light protection exclusively imparted to a co-curable composite material substrate assembly by a co-curable UV/visible light-resistant layer disposed to cover the co-curable and co-cured composite material substrate.
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3.
公开(公告)号:US20230311427A1
公开(公告)日:2023-10-05
申请号:US17708404
申请日:2022-03-30
Applicant: The Boeing Company
Inventor: Alain A. Adjorlolo , Patrice K. Ackerman , Jason A. Bolles
CPC classification number: B29C70/06 , B64C1/00 , B29C70/28 , B64C2001/0072 , B29K2309/08
Abstract: Co-curable and co-cured UV/visible light-resistant fiberglass-coated UV/visible light composite structural material substrates, and aircraft fuselages comprising co-cured UV/visible light-resistant fiberglass-coated composite material substrates and methods of their manufacture are disclosed.
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4.
公开(公告)号:US20230312124A1
公开(公告)日:2023-10-05
申请号:US17708207
申请日:2022-03-30
Applicant: The Boeing Company
Inventor: Patrice K. Ackerman , Melinda D. Miller , Jason A. Bolles
CPC classification number: B64D37/06 , B64C3/34 , B29C35/02 , B29K2309/08
Abstract: Composite material protection from UV degradation is disclosed by providing a co-cured composite material substrate co-cured with a UV/visible light-resistant fiberglass layer to form co-cured composite materials for exclusively imparting UV/visible light-resistant properties to co-cured composite material substrates for use in UV/visible light-resistant vehicle fuel tank assemblies.
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5.
公开(公告)号:US20230312076A1
公开(公告)日:2023-10-05
申请号:US18171514
申请日:2023-02-20
Applicant: The Boeing Company
Inventor: Alain A. Adjorlolo , Patrice K. Ackerman , Jason A. Bolles
CPC classification number: B64C1/00 , C08L63/00 , C08K7/06 , C09D7/70 , C08L2205/16 , B64C2001/0072
Abstract: Co-curable and co-cured UV/visible light-resistant coated UV/visible light composite structural material substrates, and aircraft fuselages comprising co-cured UV/visible light-resistant coated composite material substrates and methods of their manufacture are disclosed.
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6.
公开(公告)号:US20230312125A1
公开(公告)日:2023-10-05
申请号:US18171493
申请日:2023-02-20
Applicant: The Boeing Company
Inventor: Patrice K. Ackerman , Melinda D. Miller , Jason A. Bolles
Abstract: Composite material protection from UV degradation is disclosed by providing a co-cured composite material substrate co-cured with a UV/visible light-resistant layer to form co-cured composite materials for exclusively imparting UV/visible light-resistant properties to co-cured composite material substrates for use in UV/visible light-resistant vehicle fuel tank assemblies.
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7.
公开(公告)号:US20230311470A1
公开(公告)日:2023-10-05
申请号:US17708128
申请日:2022-03-30
Applicant: The Boeing Company
Inventor: Patrice K. Ackerman , Melinda D. Miller , Jason A. Bolles
CPC classification number: B32B37/06 , B32B7/027 , B32B7/08 , B32B27/38 , B32B5/022 , B32B27/12 , B32B27/20 , B32B2307/732 , B32B2307/71 , B32B2307/42 , B32B2250/02 , B32B2255/02 , B32B2260/021 , B32B2260/046 , B32B2262/106 , B32B2305/08 , B32B2309/02 , B32B2605/00
Abstract: Co-curable and co-cured UV/visible light-resistant composite materials are disclosed with UV/visible light protection exclusively imparted to a co-curable composite material substrate assembly by a co-curable UV/visible light-resistant fiberglass layer disposed to cover the co-curable and co-cured composite material substrate.
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公开(公告)号:US11572480B2
公开(公告)日:2023-02-07
申请号:US16490852
申请日:2018-02-27
Applicant: THE BOEING COMPANY
Inventor: Ranya Simons , Sheng Li , Stuart Arthur Bateman , Emma Simmonds , Jill Elisabeth Seebergh , Jason A. Bolles , Douglas Henry Berry
Abstract: The present disclosure relates to a method of reactivating the surface of an organic paint coating, a method of facilitating adhesion of a further coating to the organic paint coating, and a substrate having a reactivated organic paint coating. There is also disclosed a surface reactivation treatment for an organic paint coating. The reactivation method also facilitates adhesion of the organic paint coating to further coating(s) across a broad application window.
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