国家/地区 美国（3）
IPC部 C（3） H（2）
IPC大类 H05（2）
IPC小类 H05K（2）
IPC
发明人
公开年 2017（2）
申请年 2016（3）
专利权人 BOEING CO（3）

Method for forming ceramic matrix composite structure, involves providing mixture of carbon nanotubes, graphene, and silicon carbon nitride, heating mixture to bond carbon nanotubes and graphene, and sintering carbon nitride in mixture.

BRALEY D J, BELK J H, BRELEY D J, BRALEY D Y, BELK Y H

High-conductivity electrical interconnect structure for electrically interconnecting electrical components, has metallic overlay portion that connects peripheral edges of graphene elements with each other.

TANIELIAN M H

Composite material used in an aircraft, comprises carbon reinforcement fibers and a matrix material comprising functionalized graphene nanoplatelets having imide groups formed on a surface of the graphene nanoplatelets.

HUMFELD K D