国家/地区 欧洲专利局（EPO）（3）
IPC部 F（3）
IPC大类 F28（3）
IPC小类 F28D（3）
IPC F28F021/02（3）
发明人
公开年
申请年 2014（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

Composite structure comprises organic resin, carbon fiber and flat graphene nanosheets embedded in resin.

LUTZ M, TANZILLI D, BURGER N, LAACHACHI A

System for extracting and distributing geothermal heat energy, has graphene-enriched product that is provided with graphene contacts heat source for conduction of heat.

BHARGAVA M