国家/地区 中国（131）
IPC部 B（131）
IPC大类 B22（131）
IPC小类 B22F（131） C22C（113） C01B（17）
C23C（17） C22F（16） H01B（14）
B82Y（9） H01H（7） C21D（5）
F16D（5） B21C（3） B32B（3）
B22D（2） B60L（2） C04B（2）
IPC B22F003/14（131）
发明人 CHEN L（9） LI J（8） LI Z（8）
WANG Y（8） HE C（7） LIU J（7）
LIU Y（7） SHI C（7） WANG L（7）
WANG X（7） ZHAO N（7） LI M（6）
LI X（6） LIU E（6） ZHANG J（6）
公开年 2022（38） 2021（21） 2020（16） 2023（16） 2018（13） 2016（9） 2019（9） 2017（5） 2015（3）
申请年 2021（31）  2022（31）  2019（19）  2018（11）  2020（11）  2016（10）  2023（7）  2015（6）  2017（4） 
专利权人 UNIV TIANJIN（7） UNIV SHANGHA.（6） UNIV NORTH C.（4） UNIV XIAN TE.（4）
INST METAL R.（3） STATE GRID C.（3） UNIV GUIZHOU（3） UNIV HARBIN .（3）
UNIV NANCHAN.（3） UNIV NORTHWE.（3） AVIC MFG TEC.（2） BEIJING INST.（2）
HARBIN INST .（2） INST ELECTRI.（2） INST PROCESS.（2） JIANGSU CHUA.（2）
NINGBO POWER.（2） NORTHWEST IN.（2） RONGCHENG HO.（2） SHANGHAI HEW.（2）

Preparation method of graphene-interface phase core-shell network titanium matrix composite material used in aircraft engine, involves sintering titanium-based material and high-purity graphite ball after mixing powder to obtain composite material.

WANG X, LIU M, LI S, WANG L, ZHANG L, QU L, CUI B, WANG Y, DU Q, SUN Y, LI A

Titanium-doped multilayer copper-based composite material for use in e.g. aerospace field, has titanium-titanium doped composite layer arranged between reinforced-phase composite layer or between reinforced-stage composite layer and copper base surface layer.

ZHU M, DING Y, JIANG X, TAN H, QI F, SHAO Z

Enhanced titanium-based composite material with graphene size and six square boron nitride has titanium-based composite material comprises substrate and reinforcement, where reinforcement is graphene and hexagonal boron nitride nanosheet.

WANG H, XIONG N, MU X, CHENG X, FENG K, ZHANG H

Preparing multilayer graphene reinforced aluminum-based composite material comprises mixing modified multilayer graphene and metal aluminum powder, and hot-melting mixed material in mold, where modified multilayer graphene is prepared by mixing boric acid, pentaerythritol and glacial acetic acid.

LIU J

Preparing magnesium-based composite material coated graphene magnesium nano-particles with excellent interface binding characteristics used in aerospace comprises e.g. synthesizing graphene, and pre-processing bromine ethane and tetrahydrofuran.

ZHAO R, GAO J, BAI P, ZHAO Z

Preparing bimodal structure graphene oxide/magnesium-based composite material comprises adding graphene oxide to pre-milled magnesium alloy powder, hot pressing mixed powder into vacuum environment, and re-melting treatment on prefabricated blank, and adding pre-heated mold for thixotropic forming.

GAO M, ZHANG B, WANG P, WANG L, CHEN T

Preparing two-stage layered titanium-based composite material, involves installing metal foil with clean surface and composite powder of nano-reinforced body adsorption/embedded sheet titanium based powder in mold.

CHENG X, ZHANG H, DUAN H, MU X

Preparation method of composite structure shaft component, involves coating composite material layer on surface of metal base material through powder sintering to obtain blank ingot, deforming by hot extrusion to improve bonding strength between composite material layer and core metal substrate.

WANG Q, WANG D, ZHU S, ZAN Y, ZHANG J, MA Z, XIAO B, LIU Z, MA K

Preparing graphene superconducting copper wire, comprises soaking oxygen-free copper balls in self-adhesive water, adding oxygen-free copper balls coated with self-adhesive, hot-pressing graphene composite copper material and performing drawing forming and annealing treatment.

LI J, CAI M, LI B

Preparing high-strength and high-plasticity graphene-titanium composite material by interface modification, comprises washing graphene oxide with acid and alkali to remove impurities, mixing iron oxide coated graphene oxide with titanium powder, and adopting discharge plasma method to sinter.

TANG B, WAN J, GAO Q, YANG J, LI J, YAN Q, CHEN B