国家/地区 加拿大（4）
IPC部 C（4） B（3） H（2）
IPC大类 C01（4）
IPC小类 C01B（4）
IPC C01B031/04（4）
发明人 CHIU G（2） HASEGAWA S（2） HASEGAWA SHOJI（2）
HENDRIKS J（2） HENDRIX J（2） KAMIYA N（2）
KAMIYA NAGISA（2） KEAR B（2） LYNCH J（2）
NAGISA K（2） NOSKER T（2） SHEN Y（2）
SHOJI H（2） ZHAO G（2）
公开年 2015（2）
申请年 2015（2） 
专利权人 GRAPHENE PLA.（2） GRAPHENE PLA.（2） UNIV RUTGERS.（2）

Graphene-reinforced polymer matrix composite for use in manufacturing an automotive, aircraft, watercraft or aerospace part, comprises a thermoplastic polymer matrix, and particles, e.g. graphite microparticles.

NOSKER T, LYNCH J, KEAR B, HENDRIX J, CHIU G, LYNCH J K, HENDRIKS J, ZHAO G

Graphite-based carbon material used as graphene precursor for preparing graphene dispersion, comprises rhombohedral graphite layer and hexagonal graphite layer, and has specified rate calculated based on X-ray diffraction method.

HASEGAWA S, KAMIYA N, HASEGAWA SHOJI, KAMIYA NAGISA, SHOJI H, NAGISA K, SHEN Y

Graphite-type carbon raw material used as graphene precursor, has rhombohedral system graphite layer and hexagonal system graphite layer in ratio more than preset value, as measured using peak intensities specific planes of layers.

HASEGAWA S, KAMIYA N, SHOJI H, NAGISA K, HASEGAWA SHOJI, KAMIYA NAGISA, SHEN Y

Forming a graphene-reinforced polymer matrix composite useful in an aircraft, comprises distributing graphite microparticles into molten thermoplastic polymer phase, and applying succession of shear strain events to molten polymer phase.

NOSKER T, LYNCH J, HENDRIX J, KEAR B, CHIU G, TSE S, HENDRIKS J, XIE S, ZHAO G