1. 平台首页
  2. 国际专利信息
  • 专利标题:   Graphene-reinforced nickel base alloy composite material for hot end component of aircraft engine, comprises chromium, molybdenum, zirconium, beryllium, boron, graphene, and nickel.
  • 专利号:   CN114058904-A, ZA202202647-A
  • 发明人:   LV H, ZHU H, CHEN Z, ZHAO X, ZHANG Y, LYU H, WANG H
  • 专利权人:   UNIV NINGBO FINANCE ECONOMICS, UNIV NINGBO FINANCE ECONOMICS
  • 国际专利分类:   B22F003/105, B22F003/24, B22F009/04, C22C001/05, C22C001/10, C22C019/05, C22F001/10, C22C000/00
  • 专利详细信息:   CN114058904-A 18 Feb 2022 C22C-019/05 202227 Chinese
  • 申请详细信息:   CN114058904-A CN11342687 12 Nov 2021
  • 优先权号:   CN11342687, ZA002647

▎ 摘　　要

NOVELTY - The graphene-reinforced nickel base alloy composite material comprises 15-20 mass% chromium, 8-10 mass% molybdenum, 0.03-0.08 mass% zirconium, 0.003-0.005 mass% berylium, 0.05-0.1 mass% boron, 0.2-0.4 mass% graphene, and balance nickel. USE - The graphene-reinforced nickel base alloy composite material is used for the hot end component of the aircraft engine, e.g. turbine blade, turbine disk and guide blade. ADVANTAGE - The graphene-reinforced nickel-base alloy composite material has high bearing capacity and high mechanical property. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is included for a preparation method of graphene-reinforced nickel-base alloy composite material.