国家/地区 美国（14）
IPC部 B（14）
IPC大类 B64（14）
IPC小类 B64D（7） B64C（6） C08K（5）
B32B（4） C08J（4） C09D（4）
B29C（3） B64G（3） B82Y（3）
C08L（3） C23C（3） H05B（3）
B05D（2） C01B（2） C25D（2）
IPC C08K003/04（4） C08K003/22（4） C09D005/00（4）
B64D015/12（3） C08J005/00（3） B05D001/36（2）
B05D005/00（2） B32B027/04（2） B64C001/00（2）
B64D037/14（2） B64G001/10（2） B64G001/40（2）
B82Y030/00（2） C08J005/04（2） C08J005/24（2）
发明人
公开年 2021（4） 2018（3） 2023（3） 2016（2） 2022（2）
申请年 2022（5）  2016（3）  2020（2）  2021（2） 
专利权人 BOEING CO（2） EATON INTELL.（2）

Aircraft tire component comprises natural rubber, peptizer, carbon black, graphene, aliphatic hydrocarbon resin, distilled aromatic extract, N-(1,3-dimethylbutyl)-N'-phenyl-1,4-benzenediamine, 2,2,4-trimethyl-1,2-dihydroquinoline, paraffinic wax, microcrystalline wax, zinc oxide, and stearic acid.

HALASA A F, RODGERS M B, PASCHALL D

Aircraft engine component used as gearboxes, comprises wall comprising aluminum alloy and/or magnesium alloy, and protective coating comprising prime layer, silicone elastomer layer and abrasion resistant layer covering surface of wall.

IURLARO S, GARGIOLI A, GARABELLO M, GAROFALO S, GILARDI E, PICA O, ARGENTIERI G

Coating substrate by depositing a conductive layer comprising electrically conductive material over substrate, where conductive layer has specific resistivity, and depositing anti-icing layer comprising nanomaterials over conductive layer to form coating system.

KINLEN P J, PRIFTIS D

Manufacture of aerospace component involves treating surface of polymeric substrate with laser to form porous graphene at surface, and bonding metallic layer to porous graphene.

POTEET S, HUAPAYA R L N, BORDAGE K R, ROJAS HUAPAYA L N, ROJAS L N R

Solid polymer conductive composite used for non-metallic aircraft fuel delivery system component, is prepared from composition comprising polyaryletherketone polymer, conductive filler, and dispersing and processing additive.

MAPKAR J A, SALUNKE N, DEMUTH M J

Invisible ice-covering-proof compatible material useful as surface material of equipment, comprises insulating and heat insulating layer comprises e.g. polyimide, glass fiber, hollow glass microsphere and/or polyurethane and patterned heating, insulating heat conducting and hydrophobic layer.

MA Z, ZHAN X, WANG Z, ZHAO Z, ZHU Y, CHEN J, LIU X, CHEN H

Composition for forming article e.g. tube, comprises single nylon polymer, conductive nanomaterials, dielectric filler comprising an inorganic, non-conductive, non-platelet nanomaterial containing alumina nanotubes, and dispersing agent.

ZHOU Z, MAPKAR J

Pulsed E-field propulsion system used in spacecraft, comprises capacitor stack comprising capacitance elements, right circular cylindrical sections, or spiroidal ribbons, pulse coil, electromagnetic field, energy supply, pulse control circuit, and charge control circuit.

PURVIS J W

Tray for galley trolley for aircraft, has body which describes sealed volume, in which sealed volume has phase change material, engagement unit which releasably engages trolley, phase change material which has phase change temperature.

LATCHAM D

Method for forming ceramic matrix composite structure, involves providing mixture of carbon nanotubes, graphene, and silicon carbon nitride, heating mixture to bond carbon nanotubes and graphene, and sintering carbon nitride in mixture.

BRALEY D J, BELK J H, BRELEY D J, BRALEY D Y, BELK Y H