国家/地区
IPC部 B（2）
IPC大类 B64（2）
IPC小类 B64D（2）
IPC B64D015/12（2）
发明人 HU J（2）
公开年
申请年 2022（2）
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 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