国家/地区 中国（11） 美国（4） 巴西（2） 欧洲专利局（EPO）（2） 世界知识产权组织（2）
IPC部 B（16）
IPC大类 B64（16）
IPC小类 B64C（6） B64G（6） B32B（4）
B64D（4） C08J（3） C08K（3）
B23K（2） B82Y（2） C08L（2）
H05B（2）
IPC B32B007/12（3） B32B009/04（3） C08K003/04（3）
B23K026/00（2） B32B003/08（2） B32B003/12（2）
B32B009/00（2） B32B027/28（2） B64D015/12（2）
B64G001/22（2） B64G001/40（2） B64G001/50（2）
C08K007/06（2）
发明人 LI B（2） LIU Y（2） WANG Y（2）
ZHANG J（2） ZHANG Y（2）
公开年 2022（16）
申请年 2022（16）
专利权人 GOODRICH COR.（2）

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

Preparing coating useful for space capsule, comprises mixing quaternary ammonium salt modified epoxy resin, titanium dioxide, inorganic antibacterial particles, inorganic colored pigments, butyl acetate and n-butanol, adding glass microspheres and stirring and removing glass microspheres.

LIU Y, LI C, CHEN X, WU X, WANG Y, YANG X, BAI J, CUI Q, ZHANG L, ZHANG J, WEN C, JIN Y

Radiating device for fixing solar wing of spacecraft, has heat conduction film whose end is mounted on side of spacecraft main body that is not directly irradiated by sun, and secondary surface mirror mounted on heat-conducting film.

CHEN Q, YANG Z, YIN M, WANG C, SUN R

Preparing X-band stealth/lightning protection skin comprises laying up carbon fiber prepreg, conductive prepreg, wave-absorbing prepreg and wave-transmitting prepreg in sequence on surface of tooling, obtaining first skin, and molding first skin by vacuum bag process.

LI B, SONG Z, WEN Y, LIU Y

Thermal power reactor i.e. nuclear fission reactor, for use in spacecraft or planetary environment, has solid state thermal conductor arranged to transfer thermal energy generated by reactor core away from reactor core.

MORRIS P

Manufacture of aerospace component involves treating surface of polymeric substrate with laser to form porous graphene at surface, and bonding metallic layer to porous graphene.

POTEET S, HUAPAYA R L N, BORDAGE K R, ROJAS HUAPAYA L N, ROJAS L N R

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

Honeycomb wave-absorbing composite material used in edge structures e.g. spacecraft fuselage edge structures, comprises sheet and honeycomb wave-absorbing core material which is impregnated with wave absorbing slurry agent, and pouring sealant filled in core material.

DONG Q, WANG W, HE J, ZHANG J, WANG Y, SUN X

Reversible rigidized composite film used for space inflatable unfolding structure, comprises airtight layer, rigidized layer made of resin material and fiber reinforced material, heat equalizing layer, heating layer and packaging layer.

WU Y, YE X

Surface texture for use in aircraft wings, municipal power lines, satellite lines, optical applications, photography, microscopy, autonomous aerial devices, drones, comprises cross-section of three-dimensional structure containing first, second serration, and coating covers portion of valley.

HUANG H, HUANG J, PARK K K, MACHADO C J