国家/地区 欧洲专利局（EPO）（2）
IPC部 F（2）
IPC大类 F01（2）
IPC小类 F01D（2）
IPC
发明人
公开年
申请年 2016（2）
专利权人

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