国家/地区 美国（2）
IPC部 F（2）
IPC大类 F28（2）
IPC小类 F28D（2）
IPC F28F021/02（2）
发明人
公开年 2018（2）
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

Spacecraft structure i.e. satellite, has exhaust source points whose portion is directed such that outflow from exhaust source points partially impacts functional component, and graphene coating comprising set of graphene flakes.

KHAYMS V, SINTON S W, BEDWORTH P V