Claims
- 1. Titanium aluminide alloy composition consisting essentially of, in atomic %, about 44 to about 49 Al, about 0.5 to about 4.0 Nb, about 0.0 to about 3.0 Mn, about 1.0 to about 1.5 W, about 0.1 to about 1.0 Mo, about 0.4 to about 0.75 Si, and the balance Ti.
- 2. An investment casting having the composition of claim 1.
- 3. Titanium aluminide alloy composition consisting essentially of, in atomic %, about 47 Al, 2.0 Nb, 0.0 Mn, 1.0 W, 0.5 Mo, 0.5 Si, and the balance Ti.
- 4. An investment casting having the composition of claim 2.
- 5. A creep resistant titanium aluminide alloy article consisting essentially of, in atomic %, about 44 to about 49 Al, about 0.5 to about 4.0 Nb, about 0.0 to about 3.0 Mn, about 1.0 to about 1.5 W, about 0.1 to about 1.0 Mo, about 0.4 to about 0.75 Si, and the balance Ti, said article having a microstructure including gamma phase and at least one additional phase bearing at least one of W, Mo, and Si dispersed as distinct regions in the microstructure.
- 6. The article of claim 5 wherein the microstructure comprises a majority of gamma phase with a minority of alpha-two phase present.
- 7. The article of claim 5 wherein the additional phase is present as distinct regions located intergranularly of the gamma and alpha-two phases.
- 8. A creep resistant gas turbine engine component consisting essentially of, in atomic %, about 44 to about 49 Al, about 0.5 to about 4.0 Nb, about 0.0 to about 3.0 Mn, about 1.0 to about 1.5 W, about 0.1 to about 1.0 Mo, about 0.4 to about 0.75 Si, and the balance Ti, said article having a microstructure including gamma phase an at least one additional phase including W, Mo, or Si, or combinations thereof, dispersed as distinct regions in the microstructure.
CROSS REFERENCE TO RELATED APPLICATION
Priority is claimed to provisional application Ser. No. 60/058,872, filed Sep. 15, 1997.
US Referenced Citations (13)
Provisional Applications (1)
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Number |
Date |
Country |
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60/058872 |
Sep 1997 |
US |