国家/地区 中国（5）
IPC部 B（5） H（4）
IPC大类 B64（5） H05（4） H01（2）
IPC小类 B64D（5）
IPC B64D015/12（5）
发明人
公开年 2023（4）
申请年 2022（5）
专利权人

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

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