国家/地区 美国（2）
IPC部 F（3）
IPC大类 F01（3）
IPC小类 F01D（3）
IPC
发明人
公开年 2018（3）
申请年 2016（2） 
专利权人

Turbomachine composite portion for low-pressure turbomachine compressor, comprises organic matrix and reinforcing fibers, where matrix includes graphene particles, in particular enriched in oxygen, rotor blade and fan blade.

ROUSSEAU C, PEREZ R

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