国家/地区 中国（27） 美国（17） 欧洲专利局（EPO）（13） 世界知识产权组织（12） 英国（5） 日本（5） 澳大利亚（3） 加拿大（2） 法国（2） 韩国（2）
IPC部 B（46）
IPC大类 B64（46） H05（15） H01（10）
B32（8） C09（7） C08（5）
B05（4） F02（4） H02（4）
B01（2） B60（2） C23（2）
C25（2） D06（2） G03（2）
IPC小类 B64D（46）
IPC B64D015/12（16） H05B003/14（9） B64D015/00（5）
C09D005/00（5） H05B003/20（5） B64D027/24（4）
B64D045/02（4） C08K003/04（4） H05B003/02（4）
B05D001/36（3） B05D005/00（3） B64D037/32（3）
C08K003/22（3） C09D007/61（3） C09D007/65（3）
发明人 ZHANG Y（3） BONACCURSO E（2） BOTURA G C（2）
FAN Y（2） HU J（2） KINLEN P J（2）
LIU H（2） SLANE C（2） SONG Q（2）
YANG W（2） ZHANG T（2） ZHAO W（2）
ZHOU Y（2）
公开年 2021（15） 2022（11） 2023（9） 2018（3） 2014（2） 2016（2）
申请年 2021（16）  2022（11）  2020（6）  2019（3）  2014（2）  2015（2）  2018（2） 
专利权人 GOODRICH COR.（3） AIRBUS DEFEN.（2） AIRBUS OPERA.（2） AIRBUS OPERA.（2）
BOEING CO（2） CHENGDU GRAP.（2） EATON INTELL.（2） UNIV BEIHANG（2）

Annular air inlet lip for nacelle of e.g. turbofan engine of aircraft, has upstream annular wall connecting external and internal annular walls to delimit cavity, where thermal transfer coating is located on portions of surface of lip.

DIGEOS V E A, COATLENZOTTI C, LE DOCTE T J A

Wave-transparent anti-icing composite structure for use in aircraft, has graphene modified quartz fiber heating component paved on bearing layer, where graphene of graphene of heating component is paved with protective layer.

ZHANG G, DING T, ZHUO Y, LIAO L, XIA Y, HU J

Method for tuning electrical resistance of laser-induced graphene heater, involves directing laser energy on to base carbon heating element based on targeted laser-induced graphene pattern to form laser-induced graphene region from heater.

SLANE C, BOTURA G C, ZHAO W

Covalent bond coupling of ethylene-propylene-diene monomer-reduced graphene oxide composite material used in aviation seat rubber by slowly adding graphite powder to concentrated sulfuric acid and compounding oxygen deficient EPDM and oxygen-rich reduced graphene oxide by solvothermal method.

YIN C, SUN W, YANG R, TANG G, WU Z, WU Q

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

Carbon fiber composite panel with deicing structure for manufacturing aerospace and aviation equipment, has connecting platforms whose opposite sides are provided with connecting grooves and connecting block which is meshed with connecting groove.

XU Z

Structural battery for use in electrical charge providing system used in power aircraft, has seal operable to seal anode to pair of cathodes, where pair of cathodes is arranged partially within second half of housing, and anode extends from first half of housing.

BREWER R A, ELLER M R

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

Method for providing heating system to outer skin of aircraft, involves forming laser-induced graphene on polymer sheet by directing laser energy towards polymer sheet, and coupling electrical leads to laser induced graphene.

CHING N, HU J, SLANE C, BOTURA G C, WENPING Z, ZHAO W