国家/地区 美国（2）
IPC部 B（2）
IPC大类 C23（2）
IPC小类 C23C（2） F28F（2）
IPC F28F021/02（2）
发明人
公开年
申请年 2016（2）
专利权人

Spacecraft structure i.e. satellite, has exhaust source points whose portion is directed such that outflow from exhaust source points partially impacts functional component, and graphene coating comprising set of graphene flakes.

KHAYMS V, SINTON S W, BEDWORTH P V

Heat transfer device e.g. heat spreader, for use in CPU during heating operation, has composite plating layer formed on base material, where composite plating layer includes metal and graphene particles dispersed in metal.

SUWA Y, KAWAMURA K, ARAI S, SUWA N