国家/地区 欧洲专利局（EPO）（5） 美国（5） 中国（3） 世界知识产权组织（3） 加拿大（2） 日本（2）
IPC部 B（7）
IPC大类 B64（7）
IPC小类 B64D（7）
IPC C09D005/00（5） B05D001/36（3） B05D005/00（3）
B64D015/12（3） C09D007/61（3） C09D007/65（3）
B32B027/04（2） B64D015/00（2） B64D045/02（2）
C09D005/24（2） C09D007/40（2） C09D175/04（2）
C09D183/04（2）
发明人
公开年 2021（3） 2023（3）
申请年 2022（3）  2021（2） 
专利权人

Coated product used in e.g. aircraft propulsion system component, comprises product, and coating applied to at least part of product, where coating comprises polymer matrix material, inorganic filler, organic filler, and lamellar filler.

PICOT O, BEDEL V

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

Forming graphene-infused fiber composite which is used as air frame materials for aircraft, comprises providing graphene consisting of graphene particles in solvent to form mixture and applying mixture to surface of fiber composite layer.

KOZIOL K

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

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

Structural element for use in e.g. aircraft, has resistive heater comprising conductive paths of partially reduced graphene oxide, where paths generate heat by Joule effect for carrying out defrosting operation of region of element.

BRELATI A, DEL GIUDICE R, NONIS F, RICCO I