国家/地区 中国（2）
IPC部 F（3）
IPC大类 F28（3）
IPC小类 F28D（3）
IPC F28D015/02（3）
发明人
公开年 2017（2）
申请年 2016（3）
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

Heat pipe core, has single layer arranged on sheet metal net double-layer, sheet- shaped metal net whose sputtering surface with sputtered film that is formed with graphene material layer, and shell whose end is connected to heat pipe.

GUO Z, WANG L

Graphene nano-fluid gravity heat pipe comprises shell lower part which has heating section, upper part which has condensation section, and adhesive layer which is located on the bottom of the heating space.

ZHAO W, SHI J, DUAN G, LI J, LIU Z