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公开(公告)号:US5503798A
公开(公告)日:1996-04-02
申请号:US228684
申请日:1994-04-18
IPC分类号: C22C14/00
CPC分类号: C22C14/00 , F05C2201/021 , F05C2201/043
摘要: A multiphase, high-temperature material contains an intermetallic base alloy of the Ti.sub.3 Al type, which is intended especially for use in heat engines such as internal combustion engines, gas turbines and aircraft engines. The material contains from 44 to 73 atom % titanium, from 19 to 35 atom % aluminum, from 2 to 6 atom % silicon, and from 5 to 15 atom % niobium. The desired microstructure is attained by heat treating the alloy at between 800.degree. and 1100.degree. C.
摘要翻译: 多相高温材料含有Ti3Al型金属间基体合金,其特别用于内燃机,燃气轮机和飞机发动机等发动机。 该材料含有44至73原子%的钛,19至35原子%的铝,2至6原子%的硅和5至15原子%的铌。 所需的微观结构是通过在800〜1100℃之间热处理合金而实现的。