Method of heat treating titanium aluminide

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.

Description

The present invention will be more fully described by way of example with reference to the accompanying drawings in which:

FIG. 1 is graph of temperature versus time illustrating a method of heat-treating a titanium aluminide alloy according to the present invention.

FIG. 2 is a graph of temperature versus time illustrating another method of heat-treating a titanium aluminide alloy according to the present invention.

FIG. 3 is a gamma titanium aluminide alloy gas turbine engine compressor blade heat treated according to the present invention.

Claims

1. A method of heat-treating titanium aluminide alloy, the titanium aluminide alloy having a single alpha phase field and being capable of producing a massively transformed gamma microstructure, the titanium aluminide alloy comprises at least 45 at % aluminium, 0-6 at % niobium, 4-10 at % tantalum, niobium plus tantalum is less than or equal to 10 at % and the balance titanium and incidental impurities, the method comprising the steps of : (a) heating a titanium aluminide alloy to a temperature above the alpha transus temperature,(b) maintaining the titanium aluminide alloy at a temperature above the alpha transus temperature in the single alpha phase field for a predetermined time period,(c) cooling the titanium aluminide alloy from the single alpha phase field to produce a massively transformed gamma microstructure,(d) heating the titanium aluminide to a temperature below the alpha transus temperature in the alpha and gamma phase field,(e) maintaining the titanium aluminide at the temperature below the alpha transus temperature for a predetermined time period to precipitate alpha plates in the massively transformed gamma microstructure such that a refined microstructure is produced,(f) cooling the titanium aluminide to ambient temperature.

2. A method as claimed in claim 1 wherein the titanium aluminide alloy comprising at least 45 at % aluminium, 0-4 at % niobium, 4-8 at % tantalum, niobium plus tantalum is less than or equal to 8 at % and the balance titanium and incidental impurities.

3. A method as claimed in claim 1 wherein step (c) comprises cooling the titanium aluminide alloy from the single alpha phase field to a temperature in the range of 900° C. to 1200° C. and maintaining the titanium aluminide alloy at the temperature in the range of 900° C. to 1200° C. for a predetermined time period to produce a massively transformed gamma microstructure.

4. A method as claimed in claim 1 wherein step (c) comprises cooling the titanium aluminide to ambient temperature.

5. A method as claimed in claim 1, wherein in step (b) the predetermined time period is up to 2 hours.

6. A method as claimed in claim 1 wherein in step (e) the predetermined time period is up to 4 hours.

7. A method as claimed in claim 1 wherein step (d) comprises heating the titanium aluminide alloy to a temperature about 30° C. to 60° C. below the alpha transus temperature.

8. A method as claimed in claim 1 wherein step (a) comprises heating the titanium aluminide alloy to a temperature of about 20° C. to 30° C. above the alpha transus temperature.

9. A method as claimed in claim 1 wherein step (f) comprises air-cooling or furnace cooling.

10. A method as claimed in claim 3 wherein step (c) comprises fluidised bed cooling or salt bath cooling.

11. A method as claimed in claim 10 comprising cooling the titanium aluminide to ambient temperature after step (c) and before step (d).

12. A method as claimed in claim 1 wherein the titanium aluminide is cooled to ambient temperature by air-cooling or oil cooling.

13. A method as claimed in claim 1 wherein the titanium aluminide alloy comprises 46 at % aluminium, 4 at % tantalum, 4 at % niobium and the balance titanium and incidental impurities.

14. A method as claimed in claim 13 wherein the alpha transus temperature is about 1340° C., step (a) comprises heating to a temperature of 1360° C., step (b) comprises maintaining the titanium aluminide alloy at a temperature of about 1360° C. for about 1 hour, step (c) comprises salt bath, or fluidised bed, cooling the titanium aluminide alloy from a temperature of 1360° C. to a temperature between 900° C. and 1200° C. and maintaining the titanium aluminide alloy at the temperature in the range of 900° C. to 1200° C. for a predetermined time period to produce a massively transformed gamma microstructure, steps (d) and (e) comprise heating the titanium aluminide alloy to a temperature of 1280° C. to 1310° C. for about 2 hours to precipitate alpha plates in the massively transformed gamma microstructure such that a refined microstructure is produced in the titanium aluminide alloy, and step (f) comprises air cooling the titanium aluminide alloy to ambient temperature.

15. A method as claimed in claim 13 wherein the alpha transus temperature is about 1340° C., step (a) comprises heating to a temperature of 1360° C., step (b) comprises maintaining the titanium aluminide alloy at a temperature of about 1360° C. for about 1 hour, step (c) comprises air cooling the titanium aluminide alloy from a temperature of 1360° C. to ambient temperature to produce a massively transformed gamma microstructure, steps (d) and (e) comprise heating the titanium aluminide alloy to a temperature of 1280° C. to 1310° C. for about 2 hours to precipitate alpha plates in the massively transformed gamma microstructure such that a refined microstructure is produced in the titanium aluminide alloy, and step (f) comprises air cooling the titanium aluminide alloy to ambient temperature.

16. A method as claimed in claim 1 wherein the titanium aluminide alloy comprises 46 at % aluminium, 8 at % tantalum and the balance titanium and incidental impurities.

17. A method as claimed in claim 16 wherein the alpha transus temperature is between 1310° C. and 1320° C., step (a) comprises heating to a temperature of 1330° C., step (b) comprises maintaining the titanium aluminide alloy at a temperature of about 1330° C. for about 1 hour, step (c) comprise salt bath cooling, or fluidised bed cooling, the titanium aluminide alloy from a temperature of 1330° C. to a temperature between 900° C. and 1200° C. and maintaining the titanium aluminide alloy at the temperature in the range of 900° C. to 1200° C. for a predetermined time period to produce a massively transformed gamma microstructure, steps (d) and (e) comprise heating the titanium aluminide alloy to a temperature of about 1250° C. to about 1290° C. for about 4 hours to precipitate alpha plates in the massively transformed gamma microstructure such that a refined microstructure is produced in the titanium aluminide alloy, and step (f) comprises air cooling the titanium aluminide alloy to ambient temperature.

18. A method as claimed in claim 16 wherein the alpha transus temperature is between 1310° C. and 1320° C., step (a) comprises heating to a temperature of 1330° C., step (b) comprises maintaining the titanium aluminide alloy at a temperature of about 1330° C. for about 1 hour, step (c) comprise air cooling the titanium aluminide alloy from a temperature of 1330° C. to ambient temperature to produce a massively transformed gamma microstructure, steps (d) and (e) comprise heating the titanium aluminide alloy to a temperature of about 1250° C. to about 1290° C. for about 4 hours to precipitate alpha plates in the massively transformed gamma microstructure such that a refined microstructure is produced in the titanium aluminide alloy, and step (f) comprises air cooling the titanium aluminide alloy to ambient temperature.

19. A method as claimed in claim 16 wherein step (c) comprises cooling the titanium aluminide at a cooling rate of 4° C.S−1 to 150° C.S−1.

20. A method as claimed in claim 13 wherein step (c) comprises cooling the titanium aluminide at a cooling rate of 15° C.S−1 to 150° C.S−1.

21. A method as claimed in claim 1 wherein the titanium aluminide alloy is a cast titanium aluminide component.

22. A method as claimed in claim 1 wherein comprising hot isostatic pressing of the cast titanium aluminide alloy component.

23. A method as claimed in claim 22 wherein the hot isostatic pressing of the cast titanium aluminide alloy component is concurrent with step (e).

24. A method as claimed in claim 22 wherein the hot isostatic pressing comprises applying a pressure of about 150 MPa for about 4 hours.

25. A method as claimed in claim 1 wherein the titanium aluminide alloy is a compressor blade or a compressor vane.