• 专利标题:   Aircraft cylinder piston material comprises titanium oxide, niobium oxide, aluminum dioxide, graphene, cobalt powder, iron powder, puffed silicon, graphite and nickel arsenide powder.
  • 专利号:   CN107739952-A
  • 发明人:   XU S
  • 专利权人:   QINGDAO AIFEIKE AVIATION TECHNOLOGY CO
  • 国际专利分类:   C22C029/12
  • 专利详细信息:   CN107739952-A 27 Feb 2018 C22C-029/12 201819 Pages: 4 Chinese
  • 申请详细信息:   CN107739952-A CN10752852 28 Aug 2017
  • 优先权号:   CN10752852

▎ 摘  要

NOVELTY - Aircraft cylinder piston material comprises 35-45 pts. wt. titanium oxide, 4-8 pts. wt. niobium oxide, 4-6 pts. wt. aluminum dioxide, 5-9 pts. wt. graphene, 4-6 pts. wt. cobalt powder, 3-7 pts. wt. iron powder, 2-6 pts. wt. puffed silicon, 1-2 pts. wt. graphite and 1-3 pts. wt. nickel arsenide powder. USE - Used as aircraft cylinder piston material. ADVANTAGE - The material has high temperature performance, high hardness and excellent wear resistance. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is also included for preparing aircraft cylinder piston material comprising (i) adding titanium oxide, oxides, aluminum dioxide, graphene, heating at 1500-1800 degrees C and stirring to obtain mixture A, and (ii) adding 4-6 pts. wt. cobalt powder, 3-7 pts. wt. iron powder, 2-6 pts. wt. extruded silicon, 1-2 pts. wt. graphite, 1-3 pts. wt. nickel arsenide powder into mixture A, heating at 2100-2400 degrees C, mixing to obtain mixture B and then cooling to obtain final product.