国家/地区 中国（2）
IPC部 B（3）
IPC大类 C01（3）
IPC小类 C01B（3）
IPC C01B031/04（2）
发明人
公开年
申请年 2016（3）
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

Graphene thermal conductivity coating modified radiator comprises e.g. outer surface with graphite heat-conducting layer of radiating substrate connected with radiating substrate or outer surface of conducting graphene layer.

XU H, ZHOU Q

Drying device for graphene or graphite oxide, comprises heater, storage tank, feeding pump, heat exchanger, drying tower, cyclone collector, air filter, draft fan and waste gas discharge pipe, where air filter is connected with heater.

CHEN C, KONG Q, WANG D, LI S, DAN J, XIE L, WANG W, SU X