国家/地区 美国（3）
IPC部 F（3）
IPC大类 F01（3）
IPC小类 F01D（3）
IPC F01D025/00（3）
发明人
公开年
申请年 2016（2） 
专利权人 GENERAL ELEC.（2）

Airfoil e.g. fan blade for fan section of turbine engine, has matrix composite that is provided with toughness that is greater than toughness of first material, and edge guard that is provided with heating conduit arranged within portion of edge guard.

SUN C, KRAY N J, ZHENG L

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

Deposition method of composite on surface, involves thermally spraying mixture of graphene/graphene oxide flakes and metal and/or metal oxide material on surface to form composite with enhanced mechanical and corrosion resistant properties.

SEAL S, WARD D, SARAF S, GUPTA A