国家/地区 美国（4） 欧洲专利局（EPO）（2） 日本（2）
IPC部 F（4）
IPC大类 F01（4） F02（2）
IPC小类 F01D（4）
IPC F01D025/00（2） F02C007/00（2）
发明人
公开年 2018（2）
申请年 2016（4）
专利权人 GENERAL ELEC.（2）

Graphene disk for use in gas turbine engine, has disk main body defining outer surface, and multiple graphene layers arranged along outer surface and embedded in base material, where disk main body comprises base material.

VALENCIA A G

Graphene heat pipe for gas turbine engine for aircraft, comprises body with graphene, where body is provided with hot side to accept heat from gas turbine engine, and end cap is provided to establish closed fluid flow environment.

FORCIER M P, STAUBACH J B

Wrap for a casing surrounding rotating element of a core engine of a turbofan engine, has matrix that is configured receive mechanical fastener to stabilize graphene sheets and gap is provided between the abutted sheets.

GUIJARRO VALENCIA A, GUIJARRO V A, GUGARO V A

Deposition method of composite on surface, involves thermally spraying mixture of graphene/graphene oxide flakes and metal and/or metal oxide material on surface to form composite with enhanced mechanical and corrosion resistant properties.

SEAL S, WARD D, SARAF S, GUPTA A