Additive manufacturing of high-temperature components from TiAl

Patent metadata

Field	Value
Publication number	US-10544485-B2
Application number	US-201715600864-A
Country	US
Kind code	B2
Filing date	May 22, 2017
Priority date	May 23, 2016
Publication date	Jan 28, 2020
Grant date	Jan 28, 2020

Abstract

Disclosed is a process for producing a component from a TiAl alloy by layer-by-layer deposition of powder on a substrate and/or an already produced semifinished product. The component has a proportion of x at % of aluminum which is in the range from about 34 to about 47 at % of aluminum, the powder having a proportion of x+1 at % to x+6 at % of aluminum. Also disclosed is a component formed from a TiAl alloy which has been produced by a corresponding process.

First claim

What is claimed is:

1. A process for producing a component from a TiAl alloy by layer-by-layer deposition of powder on a substrate and/or an already produced semifinished product, wherein the component has a proportion of x at % of aluminum which ranges from 34 at % to 47 at % of aluminum and the powder has a proportion of from x+1 at % to x+6 at % of aluminum.

2. The process of claim 1 , wherein the powder has a proportion of from x+2 at % to x+6 at % of aluminum.

3. The process of claim 1 , wherein the powder is melted in the layer-by-layer deposition.

4. The process of claim 3 , wherein the powder is melted by a high-energy beam.

5. The process of claim 3 , wherein the layer-by-layer deposition is effected by electron beam melting (EBM) or laser melting.

6. The process of claim 1 , wherein the powder has a chemical composition that enables at least partial peritectic solidification of molten powder.

7. The process of claim 1 , wherein the powder is formed from a TiAl alloy comprising from 35 at % to 53 at % of aluminum as well as niobium, molybdenum and/or tungsten, optionally zirconium, optionally silicon and optionally carbon, remainder titanium and unavoidable impurities.

8. The process of claim 1 , wherein the powder is formed from a TiAl alloy comprising from 35 at % to 53 at % of aluminum, from 6 at % to 11 at % of niobium, from 0.1 at % to 5 at % of molybdenum and/or from 0.1 at % to 2 at % of tungsten, from 0 at % to 4 at % of zirconium, from 0 at % to 4 at % of silicon and from 0 at % to 1 at % of carbon, remainder titanium and unavoidable impurities.

9. The process of claim 1 , wherein the already produced semifinished product and/or the powder is preheated to a temperature of from about 1000° C. to about 1150° C.

10. The process of claim 1 , wherein the layer-by-layer formation of the component is followed by hot isostatic pressing of the component at temperatures of from about 1200° C. to about 1300° C. and at pressures of from about 100 MPa to about 200 MPa for from about 2 to about 8 hours.

11. The process of claim 1 , wherein the component has a composition of from 34 at % to 39 at % of aluminum, from 6 at % to 11 at % of niobium, from 3 at % to 5 at % of molybdenum and/or from 0.6 at % to 2 at % of tungsten, from 0 at % to 4 at % of zirconium, from 0 at % to 4 at % of silicon, remainder titanium and unavoidable impurities.

12. The process of claim 1 , wherein the component has a composition of from 43 at % to 47 at % of aluminum, from 6 at % to 9 at % of niobium, from 0.1 at % to 1 at % of molybdenum, from 0.1 at % to 2 at % of tungsten, from 0.1 at % to 4 at % of zirconium, from 0.5 at % to 4 at % of silicon, from 0.4 at % to 1 at % of carbon, remainder titanium and unavoidable impurities.

13. The process of claim 1 , wherein the component has a composition of from 34 at % to 47 at % of aluminum, from 6 at % to 11 at % of niobium, from 0.1 at % to 5 at % of molybdenum and/or from 0.1 at % to 2 at % of tungsten, from 0 at % to 4 at % of zirconium, from 0 at % to 4 at % of silicon and from 0 at % to 1 at % of carbon, remainder titanium and unavoidable impurities.

14. The process of claim 13 , wherein a microstructure of the component comprises Si-containing, C-containing and Zr-containing precipitates.

15. The process of claim 13 , wherein the powder has a composition of from 35 at % to 53 at % of aluminum, from 6 at % to 11 at % of niobium, from 0.1 at % to 5 at % of molybdenum and/or from 0.1 at % to 2 at % of tungsten, from 0 at % to 4 at % of zirconium, from 0 at % to 4 at % of silicon and from 0 at % to 1 at % of carbon, remainder titanium and unavoidable impurities.

16. The process of claim 15 , wherein the powder has a composition of from 35 at % to 45 at % of aluminum, from 6 at % to 11 at % of niobium, from 3 at % to 5 at % of molybdenum and/or from 0.6 at % to 2 at % of tungsten, from 0 at % to 4 at % of zirconium, from 0 at % to 4 at % of silicon, remainder titanium and unavoidable impurities.

17. The process of claim 15 , wherein the powder has a composition of from 45 at % to 53 at % of aluminum, from 6 at % to 9 at % of niobium, from 0.1 at % to 1 at % of molybdenum, from 0.1 at % to 2 at % of tungsten, from 0.1 at % to 4 at % of zirconium, from 0.5 at % to 4 at % of silicon, from 0.4 at % to 1 at % of carbon, remainder titanium and unavoidable impurities.

18. The process of claim 13 , wherein the component has a predominantly lamellar microstructure.

19. The process of claim 18 , wherein the component has a lamellar structure in more than about 75% by volume of the component.

20. The process of claim 18 , wherein the component has a lamellar structure in more than about 90% by volume of the component.

Assignees

• MTU Aero Engines AG

Inventors

• Schloffer Martin
• Smarsly Wilfried

Classifications

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B22F3/15

  Hot isostatic pressing · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title

• B23K15/0086

  welding for purposes other than joining, e.g. build-up welding · CPC title

• C22C14/00 Primary

  Alloys based on titanium · CPC title