国家/地区 中国（16）
IPC部 B（16）
IPC大类 B64（16）
IPC小类 B64D（8） B64C（4） B64F（3）
B64G（3） H05B（3） H05K（3）
B60P（2） C08K（2）
IPC B64D015/12（4） B60P003/00（2） B64G001/58（2）
C08K003/22（2） H05B003/02（2） H05B003/03（2）
H05B003/14（2） H05B003/20（2） H05K007/20（2）
发明人 CHEN J（2） CHEN S（2） DU K（2）
FAN Y（2） LI W（2） LIU H（2）
LIU J（2） LIU X（2） WANG Z（2）
ZHANG T（2） ZHOU Y（2）
公开年 2021（16）
申请年 2021（11）  2020（5） 
专利权人 CHENGDU GRAP.（2） WEIHAI GUANG.（2）

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

Device for protecting body from damage, has inner assembly that is adjacent to outer protective cover and comprises thermal energy transfer device adapted to transfer thermal energy to and/or from thermal energy conduction element.

DEVINE S, CHEN S

Ice removing liquid box for de-icing liquid supplementing vehicle, has electric heating device arranged in inner cavity of box body, where heating device is fixedly connected with box body and is controlled by control device.

ZHU L, LIU H, SUI C, LIU J, DU K, LI W

Intelligent electric airplane deicing vehicle for normal operation of winter airplane, has electric control system that is composed of PLC controller, display screen and battery management module.

HUANG B, LIU H, LI W, WEI Y, CHEN M, DU K

Invisible ice-covering-proof compatible material useful as surface material of equipment, comprises insulating and heat insulating layer comprises e.g. polyimide, glass fiber, hollow glass microsphere and/or polyurethane and patterned heating, insulating heat conducting and hydrophobic layer.

MA Z, ZHAN X, WANG Z, ZHAO Z, ZHU Y, CHEN J, LIU X, CHEN H

Polyurethane composition used for forming capsule material for flight device, comprises thermoplastic polyurethane elastomer, polyurethane prepolymer, chain extender, grafting agent, initiator, coupling agent, inorganic nanoparticles and solvent.

ZANG L, LIU X, SONG X, CHEN S, ZHENG Y, ZHAO W, JI X, LIU J

Integrated structure of satellite bearing and heat management, has satellite protection layer structure that is surrounded by metal layer hollow micro lattice structure composed of hollow thin pipe that is provided with phase change material.

CHEN J, LIU L, XU W

Temperature-resistant interval type heating transparent film for wing auxiliary piece of unmanned aerial vehicle, has outer film adhered on two sides of graphene layer through high temperature resistant glue.

FAN Y, ZHANG T, ZHOU Y

Carbon fiber composite material used for helicopter main rotor wings, comprises graphene modified phenolic resin, carbon fiber board coated with pre-cured product, hexamethylenetetramine, wollastonite, carbon black and calcium hydroxide.

YAO E, ZHU X, CHU P, XIE C, TANG J

Aerospace vehicle, has cabin body provided with battery wing and boosting device, and solar battery wings uniformly distributed on circumference of position, where solar battery wing is provided with graphene solar battery.

YUAN N