Patent · US Active

Method of heat treating titanium aluminide

US7704339B2 · kind B2 · utility

2Cited by
4References
24Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 18, 2007
Grant dateApr 27, 2010
Priority date
Expiry dateSep 10, 2027

Classification

  • Technology area (CPC C)Chemistry; Metallurgy
  • CPC primaryC22C30/00
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

A gamma titanium aluminide alloy consisting of 46 at % aluminium, 8 at % tantalum and the balance titanium plus incidental impurities has an alpha transus temperature Tα between 1310° C. and 1320° C. The gamma titanium aluminide alloy was heated to a temperature T1=1330° C. and was held at T1=1330° C. for 1 hour or longer. The gamma titanium aluminide alloy was air cooled to ambient temperature to allow the massive transformation to go to completion. The gamma titanium aluminide alloy was heated to a temperature T2=1250° C. to 1290° C. and was held at T2 for 4 hours. The gamma titanium aluminide alloy was air cooled to ambient temperature. The gamma titanium aluminide alloy has a fine duplex microstructure comprising differently orientated alpha plates in a massively transformed gamma matrix. The heat treatment reduces quenching stresses and allows larger castings to be grain refined.

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