Patent · US Expired

High-temperature creep-resistant material

US5503798A · kind A · utility

18Cited by
6References
7Claims
0Family size

Assignees

Inventors

Key dates

Filing dateApr 18, 1994
Grant dateApr 2, 1996
Priority date
Expiry dateApr 18, 2014

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05C2201/043
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.