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11.发明申请公开(公告)号：US20180079885A1
公开(公告)日：2018-03-22
申请号：US15825007
申请日：2017-11-28
申请人： The Boeing Company
发明人： Andrew P. Nowak , Sophia S. Yang , Thomas I. Boundy , Darrin M. Hansen , Alain A. Adjorlolo , Carissa A. Pajel , Eliana V. Ghantous
CPC分类号： C08K3/22 , B22F1/0059 , B22F1/02 , B22F7/08 , B22F9/24 , B22F2304/058 , B22F2998/10 , B22F2999/00 , B82Y25/00 , B82Y30/00 , C08K9/06 , C08K2201/01 , C08L81/02 , C08L81/04 , C09D181/04 , C09K3/1012 , C22C2202/02 , H01F1/0054 , B22F2304/054 , B22F2304/056 , B22F3/22 , B22F2202/05
摘要： A low viscosity polysulfide sealant composition. The composition comprises a curable polysulfide polymer; a crosslinking agent; and a plurality of core-shell particles. The core-shell particles comprise: a core comprising a ferromagnetic material; and a shell comprising silica treated with an organic sulfur containing compound. The shell is capable of bonding with the polysulfide polymer.
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公开(公告)号：US20200086975A1
公开(公告)日：2020-03-19
申请号：US16135777
申请日：2018-09-19
申请人： The Boeing Company
摘要： A method of forming a monolithic aircraft structure having multiple aerodynamic surfaces includes forming a body component to have a body skin defining a body skin outer surface, and a body side wall integrally formed with the body skin and defining a body mating surface, the body skin outer surface providing a first aerodynamic surface. A cover component is formed to have a cover mating surface and a cover outer surface opposite the cover mating surface, the cover outer surface defining a second aerodynamic surface. The body component is positioned relative to the cover component so that the body mating surface engages the cover mating surface. At least portions of the cover mating surface are friction stir welded to the body mating surface to form friction stir welded joints between the body component and the cover component.
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13.发明授权公开(公告)号：US09856359B2
公开(公告)日：2018-01-02
申请号：US14681747
申请日：2015-04-08
申请人： The Boeing Company
发明人： Andrew P. Nowak , Sophia S. Yang , Thomas I. Boundy , Darrin M. Hansen , Alain A. Adjorlolo , Carissa A. Pajel , Eliana V. Ghantous
IPC分类号： C08K3/22 , C09D181/04 , C08K9/06 , B22F1/02 , C09K3/10 , C08L81/02 , C08L81/04 , H01F1/00 , B22F1/00 , B22F7/08 , B22F9/24 , B82Y25/00 , B82Y30/00
CPC分类号： C08K3/22 , B22F1/0059 , B22F1/02 , B22F7/08 , B22F9/24 , B22F2304/058 , B22F2998/10 , B22F2999/00 , B82Y25/00 , B82Y30/00 , C08K9/06 , C08K2201/01 , C08L81/02 , C08L81/04 , C09D181/04 , C09K3/1012 , C22C2202/02 , H01F1/0054 , B22F2304/054 , B22F2304/056 , B22F3/22 , B22F2202/05
摘要： A low viscosity polysulfide sealant composition. The composition comprises a curable polysulfide polymer; a crosslinking agent; and a plurality of core-shell particles. The core-shell particles comprise: a core comprising a ferromagnetic material; and a shell comprising silica treated with an organic sulfur containing compound. The shell is capable of bonding with the polysulfide polymer.
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公开(公告)号：US09611375B1
公开(公告)日：2017-04-04
申请号：US14931518
申请日：2015-11-03
申请人： THE BOEING COMPANY
CPC分类号： C08G59/10 , C08G59/66 , C08G59/686 , C08J5/24 , C08J2363/00 , C08K3/013 , C08K3/36 , C08K5/5403 , C08K9/06 , C09J163/00 , C08L63/00
摘要： Aspects described herein generally describe epoxy resins and methods of epoxy resin formation. In some embodiments, a resin includes the reaction product of one or more polythiols, one or more polyepoxides, one or more fillers and one or more amine catalysts. Polythiols have between two and about ten thiol moieties. Polyepoxides have between two and about ten epoxy moieties. One or more amine catalysts of the formula NR1R2R3, wherein each of R1, R2, and R3 is independently linear or branched C1-20 alkyl or two or more of R1, R2, and R3 combine to form cycloalkyl. The resin has a compressive strength of at least 14 ksi at 2% offset at 70° F. and at least 8 ksi at 2% offset at 190° F.
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15.发明申请公开(公告)号：US20160300646A1
公开(公告)日：2016-10-13
申请号：US14681747
申请日：2015-04-08
申请人： The Boeing Company
发明人： Andrew P. Nowak , Sophia S. Yang , Thomas I. Boundy , Darrin M. Hansen , Alain A. Adjorlolo , Carissa A. Pajel , Eliana V. Ghantous
CPC分类号： C08K3/22 , B22F1/0059 , B22F1/02 , B22F7/08 , B22F9/24 , B22F2304/058 , B22F2998/10 , B22F2999/00 , B82Y25/00 , B82Y30/00 , C08K9/06 , C08K2201/01 , C08L81/02 , C08L81/04 , C09D181/04 , C09K3/1012 , C22C2202/02 , H01F1/0054 , B22F2304/054 , B22F2304/056 , B22F3/22 , B22F2202/05
摘要： A low viscosity polysulfide sealant composition. The composition comprises a curable polysulfide polymer; a crosslinking agent; and a plurality of core-shell particles. The core-shell particles comprise: a core comprising a ferromagnetic material; and a shell comprising silica treated with an organic sulfur containing compound. The shell is capable of bonding with the polysulfide polymer.
摘要翻译： 低粘度聚硫密封剂组合物。 该组合物包含可固化的多硫化物聚合物; 交联剂; 和多个核 - 壳颗粒。 核 - 壳颗粒包括：包含铁磁材料的芯; 以及包含用有机含硫化合物处理的二氧化硅的壳。 壳体能够与多硫化物聚合物结合。
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16.发明公开公开(公告)号：US20230312076A1
公开(公告)日：2023-10-05
申请号：US18171514
申请日：2023-02-20
申请人： The Boeing Company
CPC分类号： B64C1/00 , C08L63/00 , C08K7/06 , C09D7/70 , C08L2205/16 , B64C2001/0072
摘要： 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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公开(公告)号：US11584859B2
公开(公告)日：2023-02-21
申请号：US16541754
申请日：2019-08-15
申请人： The Boeing Company
发明人： John J. Vajo , Jason Graetz , Alain A. Adjorlolo
摘要： A crystalline titanium and magnesium compound having an X-ray diffraction pattern having interplanar spacing (d-spacing) values at about 5.94, 3.10, 2.97, 2.10, 1.98, 1.82, and 1.74±0.1 angstroms may be used in protective coatings for metal or metal alloy substrates. The coatings exhibit excellent corrosion resistances and provide corrosion protection equal to or better than typical non-chromate coatings.
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公开(公告)号：US11084569B2
公开(公告)日：2021-08-10
申请号：US16135777
申请日：2018-09-19
申请人： The Boeing Company
IPC分类号： B64C9/32 , B64F5/10 , B23K20/12 , B23K20/233 , B64C3/26 , B64C9/02 , B23K103/10 , B23K101/00
摘要： A method of forming a monolithic aircraft structure having multiple aerodynamic surfaces includes forming a body component to have a body skin defining a body skin outer surface, and a body side wall integrally formed with the body skin and defining a body mating surface, the body skin outer surface providing a first aerodynamic surface. A cover component is formed to have a cover mating surface and a cover outer surface opposite the cover mating surface, the cover outer surface defining a second aerodynamic surface. The body component is positioned relative to the cover component so that the body mating surface engages the cover mating surface. At least portions of the cover mating surface are friction stir welded to the body mating surface to form friction stir welded joints between the body component and the cover component.
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公开(公告)号：US20210047522A1
公开(公告)日：2021-02-18
申请号：US16541754
申请日：2019-08-15
申请人： The Boeing Company
发明人： John J. VAJO , Jason Graetz , Alain A. Adjorlolo
摘要： A crystalline titanium and magnesium compound having an X-ray diffraction pattern having interplanar spacing (d-spacing) values at about 5.94, 3.10, 2.97, 2.10, 1.98, 1.82, and 1.74±0.1 angstroms may be used in protective coatings for metal or metal alloy substrates. The coatings exhibit excellent corrosion resistances and provide corrosion protection equal to or better than typical non-chromate coatings.
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公开(公告)号：US20190283341A1
公开(公告)日：2019-09-19
申请号：US16430092
申请日：2019-06-03
申请人： The Boeing Company
发明人： Hardik Dalal , Alain A. Adjorlolo , Adam F. Gross , Andrew P. Nowak , Brad Andrew Coxon , Kurtis Willden , Daniel M. Rotter , Stephen Lee Metschan , Berryinne Decker
摘要： The present disclosure is directed to a method of making a composite part. The method comprises covering a mold tool for a composite part with a parting film. The method further comprises laying up at least one layer of pre-preg on the parting film covering the mold tool to form a layed-up composite part and removing the layed-up composite part from the parting film. The parting film comprises a polymer sheet having a first major surface and a second major surface; and a first adhesive disposed on the first major surface of the polymer sheet, the first adhesive adhering the polymer sheet to the mold tool.
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