国家/地区 中国（11） 美国（8） 欧洲专利局（EPO）（5）
IPC部 B（16） H（12） C（3）
IPC大类 B64（16） H05（12） H01（5）
B32（3） C09（3）
IPC小类 B64D（16）
IPC B64D015/12（16）
发明人 BONACCURSO E（2） BOTURA G C（2） HU J（2）
KINLEN P J（2） SLANE C（2） SONG Q（2）
ZHANG Y（2） ZHAO W（2）
公开年 2021（5） 2022（4） 2023（4）
申请年 2021（6）  2022（6）  2019（2） 
专利权人 AIRBUS DEFEN.（2） AIRBUS OPERA.（2） BOEING CO（2） GOODRICH COR.（2）

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

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

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

Graphene film electrothermal deicing device, has connecting block whose side is provided with inclined scraper, where side of inclined scraping plate is connected with butt scraping plate.

WEI S, ZHANG Y, YU P, MEN Z, XU F, LI B

Dielectric barrier discharge plasma actuator of graphene electric heating film base, has insulation layer will be exposed from grid gap of exposing electrode when viewed from bottom to top, super-Hydrophobic layer will also be coated directly on exposed insulation layer.

JIA M, BIAN D, WU Y, LIANG H, ZHENG X, ZONG H, CHENG X, SONG H

Airfoil comprises intermediate section coupled with root section, tip section coupled with intermediate section, layer arranged on root section, intermediate section and/or tip section, and comprising carbon allotrope material, and conductive material arranged on carbon allotrope material.

YOUNG K W, KINLEN P J

Heating device for wind power blade and wing of aircraft, has upper packaging layer that is set on surface of heating layer away from lower packaging layer, and electrode that is connected with heating layer.

LI N, WANG H, JIANG B, SONG Q

Structural component for aircraft, comprises heatable component section having layer structure comprising inner base structure, heating layer having carbon allotropes embedded in matrix material, and first group of consecutive layers.

BONACCURSO E, LINDE P