国家/地区 中国（8）
IPC部 B（8） C（3） H（3）
IPC大类 B64（8）
IPC小类 B64D（5） B64C（4） B32B（3）
H05B（3） B05D（2） B64G（2）
C09D（2）
IPC B64D015/12（4） B05D001/36（2） B05D005/00（2）
B64C001/40（2） C09D005/00（2） C09D007/65（2）
H05B003/00（2）
发明人 XU Z（2）
公开年 2023（8）
申请年 2022（8）
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

High-efficiency heat insulation/high-sensitivity heat storage and release integrated sandwich spacecraft thermal protection structure comprises heat storage layer comprising heat conducting component used as shaping substrate, and phase change component adsorbed to hole of heat conducting component.

TAO J, SI Q, WANG Z, HU Y, HE C, TANG G

Guide rail slider device useful to space probe, has guide rail mechanism which is convex, and sliding block, which can be slidingly set on guide rail mechanism, where sliding block is provided with lubricating material storage chamber.

LIANG J, MENG D, FU Z, WANG H, TIAN B, SHE D, YANG R, YUE W, ZHU L, KANG J

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

Light anti-heat bearing invisible integrated structure for aircraft body, has sandwich structure filled with wave-absorbing material, and structure body whose edge is selected as pressing plate area formed by bonding outer layer panel and inner layer panel.

CHENG F, WANG J, MENG Q, QIU F, ZHANG S, XIAO K, CHENG L, XU Z, LI D, CUI Z, ZHANG F, YIN J, DENG Y, TANG Q, XIONG Y, XU F, GU C, WU D, XU J

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