• 专利标题:   Casting aircraft-based cylinder piston material comprises titanium carbide, niobium carbide, alumina, graphene flake, cobalt powder, iron powder, silicon nitride, heavy rare earth, graphite, and nickel powder.
  • 专利号:   CN107699765-A
  • 发明人:   XU S
  • 专利权人:   QINGDAO AIFEIKE AVIATION TECHNOLOGY CO
  • 国际专利分类:   C22C001/10, C22C029/02, F02F003/00
  • 专利详细信息:   CN107699765-A 16 Feb 2018 C22C-029/02 201818 Pages: 4 Chinese
  • 申请详细信息:   CN107699765-A CN10751926 28 Aug 2017
  • 优先权号:   CN10751926

▎ 摘  要

NOVELTY - Casting aircraft-based cylinder piston material comprises 35-45 pts. wt. titanium carbide, 4-6 pts. wt. niobium carbide, 4-6 pts. wt. alumina, 1.5-2.5 pts. wt. graphene flake, 0.4-0.6 pt. wt. cobalt powder, 0.4-0.6 pt. wt. iron powder, 1.5-2.5 pts. wt. silicon nitride, 1.5-2.5 pts. wt. heavy rare earth, 1-2 pts. wt. graphite, and 1-2 pts. wt. nickel powder. USE - Casting aircraft-based cylinder piston material. ADVANTAGE - The material has excellent high temperature performance, hardness and abrasion resistance, and low thermal expansion coefficient. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is included for preparation of the casting aircraft-based cylinder piston material comprising taking titanium carbide, niobium carbide, alumina, graphene, cobalt powder and iron powder, heating at 1500-1800 degrees C, stirring, mixing remaining raw materials, heating at 2100-2400 degrees C, stirring, and mixing mixtures.