国家/地区 中国（6）
IPC部 B（6）
IPC大类 B64（6） H05（4） H01（3）
IPC小类 B64D（6）
IPC B64D015/12（4） H05B003/00（2） H05B003/02（2）
H05B003/14（2） H05B003/20（2）
发明人 ZHANG Y（2）
公开年 2022（3） 2023（3）
申请年 2022（6）
专利权人

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

Solid polymer conductive composite used for non-metallic aircraft fuel delivery system component, is prepared from composition comprising polyaryletherketone polymer, conductive filler, and dispersing and processing additive.

MAPKAR J A, SALUNKE N, DEMUTH M J

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

Magnetic suspension ring rotor structure for aviation core less wheel rim electric propulsion, has rotor magnetic yoke made of high-strength amorphous alloy material, and fan assembly disassembled and installed by adopting locking ring structure.

ZHANG Y, WANG S, BAI M, JIANG C, YAO X, YANG W, HE P