IP Library Granted Patent US 7,879,286
Granted Patent B2
US 7,879,286 · App. 11/448,160 · Granted Feb 1, 2011

Method of producing high strength, high stiffness and high ductility titanium alloys

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Quick Facts
Patent No.
US 7,879,286
App. No.
11/448,160
Granted
Feb 1, 2011
Kind
B2
Abstract

A method of producing a high strength, high stiffness and high ductility titanium alloy, comprising combining the titanium alloy with boron so that the boron concentration in the boron-modified titanium alloy does not exceed the eutectic limit. The carbon concentration of the boron-modified titanium alloy is maintained below a predetermined limit to avoid embrittlement. The boron-modified alloy is heated to a temperature above the beta transus temperature to eliminate any supersaturated excess boron. The boron-modified titanium alloy is deformed at a speed slow enough to prevent microstructural damage and reduced ductility.

Claims (49)

1. A method of producing a high strength, high stiffness and high ductility titanium alloy, the method comprising:

alloying a titanium alloy with boron so that the boron concentration in the boron-modified titanium alloy does not exceed the eutectic limit;

maintaining the carbon concentration of the boron-modified titanium alloy below a predetermined limit to avoid embrittlement of the boron-modified titanium alloy;

heating the boron-modified alloy to a temperature above the beta transus temperature to force supersaturated boron out of a titanium lattice of the boron-modified titanium alloy and to increase an inter-particle spacing of a titanium boride microconstituent; and

deforming the boron-modified titanium alloy at a speed that avoids damage to the titanium boride microconstituent of the boron-modified titanium alloy.

2. The method of claim 1 wherein the boron is added to a molten titanium alloy and the melt is atomized to obtain boron-containing titanium alloy powder.

3. The method of claim 2 wherein the boron-containing titanium alloy powder is consolidated and/or formed by hot isostatic pressing, forging, extrusion or rolling.

4. The method of claim 2 wherein the boron is in liquid or powder form.

5. The method of claim 1 wherein the titanium alloy is selected from the group consisting of Ti-6Al-4V, Ti-5Al-2.5Sn and Ti-6Al-2Sn-4Zr-2Mo-0.1Si.

6. The method of claim 1 wherein the boron-modified alloy heated above the beta transus temperature is cooled at a rate slow enough to prevent reduced ductility.

7. The method of claim 1 , wherein the steps of heating the boron-modified titanium alloy and deforming the boron-modified titanium alloy are conducted simultaneously.

8. The method of claim 1 , wherein deforming the boron-modified titanium alloy comprises at least one of forging, extruding, and rolling the boron-modified titanium alloy.

9. The method of claim 8 , wherein deforming the boron-modified titanium alloy comprises extruding the boron-modified titanium alloy at a ram speed no greater than 15 inch/mm.

10. The method of claim 1 , wherein the carbon concentration of the boron-modified titanium alloy is no greater than 0.1 weight percent.

11. A method of processing a titanium alloy, the method comprising:

alloying a molten titanium alloy with boron to form a boron-modified titanium alloy melt, wherein the concentration of boron in the melt is below the eutectic limit of boron in the titanium alloy;

atomizing the melt to form a boron-containing titanium alloy powder;

heating the boron-containing titanium alloy powder to a temperature above a beta transus temperature of the boron-containing titanium alloy powder to force supersaturated boron out of a titanium lattice of the boron-containing titanium alloy powder and to increase an inter-particle spacing in a distribution of titanium boride particles in the boron-containing titanium alloy powder.

12. The method of claim 11 , further comprising maintaining the carbon concentration of the boron-containing titanium alloy powder below a predetermined limit to avoid embrittlement.

13. The method of claim 12 , wherein the predetermined limit is no greater than 0.1 weight percent.

14. The method of claim 11 , further comprising cooling the boron-containing titanium alloy powder from the temperature above the beta transus temperature at a rate slow enough to prevent reduced ductility.

15. The method of claim 11 , wherein heating further comprises consolidating the boron-containing titanium alloy powder at a deformation rate that avoids damage to the titanium boride particles of the boron-containing titanium alloy powder, to provide a consolidated boron-modified titanium alloy powder.

16. The method of claim 15 , wherein consolidating the boron-modified titanium alloy powder comprises at least one of hot isotactic pressing and extruding the boron-containing titanium alloy powder.

17. The method of claim 16 , wherein consolidating the boron-modified titanium alloy powder comprises extruding the boron-modified titanium alloy powder at a ram speed no greater than 15 inch/mm.

18. The method of claim 15 , further comprising thermomechanically processing the consolidated boron-containing titanium alloy powder at a deformation rate that avoids damage the titanium boride particles of the consolidated boron-containing titanium alloy powder.

19. The method of claim 18 , wherein thermomechanically processing the consolidated boron-modified titanium alloy powder comprises at least one of forging, extruding, and rolling the consolidated boron-modified titanium alloy powder.

20. The method of claim 18 , wherein thermomechanically processing the consolidated boron-modified titanium alloy powder comprises extruding the consolidated boron-modified titanium alloy powder at a ram speed no greater than 15 inch/mm.

21. The method of claim 11 , further comprising, subsequent to heating the boron-containing titanium alloy powder above the beta transus temperature, consolidating the boron-containing titanium alloy powder at a deformation rate that avoids damage to the titanium boride particles of the boron-containing titanium alloy powder.

22. The method of claim 21 , wherein consolidating the boron-containing titanium alloy powder comprises one of hot isotactic pressing and extruding the boron-containing titanium alloy powder.

23. The method of claim 22 , wherein consolidating the boron-containing titanium alloy powder comprises extruding the consolidated boron-modified titanium alloy powder at a ram speed no greater than 15 inch/mm.

24. The method of claim 21 , further comprising thermomechanically processing the consolidated boron-containing titanium alloy powder at a deformation rate that avoids damage the titanium boride particles of the titanium alloy.

25. The method of claim 24 , wherein thermomechanically processing the consolidated boron-containing titanium alloy powder comprises at least one of forging, extruding, and rolling the consolidated boron-containing titanium alloy powder.

26. The method of claim 25 , wherein thermomechanically processing the consolidated boron-containing titanium alloy powder comprises extruding the boron-modified titanium alloy powder at a ram speed no greater than 15 inch/mm.

27. The method of claim 11 , wherein the boron is in liquid or powder form.

28. The method of claim 11 , wherein the molten titanium alloy is selected from the group consisting of Ti-6Al-4V alloy, Ti-5Al-2.5Sn alloy, and Ti-6Al-2Sn-4Zr-2Mo-0.1Si alloy.

29. A method of processing a titanium alloy, the method comprising:

alloying a molten titanium alloy with boron to form a boron-modified titanium alloy melt, wherein the concentration of boron in the melt is below the eutectic limit of boron in the titanium alloy;

atomizing the melt to form a boron-containing titanium alloy powder;

consolidating the boron-containing titanium alloy powder to form a consolidated boron-containing titanium alloy powder; and

heating the consolidated boron-containing titanium alloy powder above a beta transus temperature of the consolidated boron-containing alloy powder to force supersaturated boron out of a titanium lattice of the boron-containing titanium alloy powder and to increase an inter-particle spacing in a distribution of titanium boride particles in the consolidated boron-containing titanium alloy powder.

30. The method of claim 29 , further comprising maintaining the carbon concentration of the consolidated boron-containing titanium alloy powder below a predetermined limit to avoid embrittlement.

31. The method of claim 30 , wherein the predetermined limit is no greater than 0.1 weight percent.

32. The method of claim 29 , further comprising cooling the consolidated boron-containing titanium alloy powder from the temperature above the beta transus temperature at a rate slow enough to prevent reduced ductility.

33. The method of claim 29 , further comprises thermomechanically processing the consolidated boron-containing titanium alloy powder at a deformation rate that does not damage the titanium boride particles of the consolidated boron-containing titanium alloy powder.

34. The method of claim 33 , wherein the steps of heating the consolidated boron-containing titanium alloy powder above the beta transus temperature and thermomechanically processing the consolidated boron containing titanium alloy powder occur simultaneously.

35. The method of claim 33 , wherein thermomechanically processing the consolidated boron-containing titanium alloy powder comprises at least one of forging, extruding, and rolling the consolidated boron-containing titanium alloy powder.

36. The method of claim 33 , wherein thermomechanically processing the consolidated boron-containing titanium alloy powder comprises extruding the consolidated boron-containing titanium alloy powder at a ram speed no greater than 15 inch/mm.

37. The method of claim 29 , wherein the boron is in liquid or powder form.

38. The method of claim 29 , wherein the molten titanium alloy is selected from the group consisting of Ti-6Al-4V alloy, Ti-5Al-2.5Sn alloy, and Ti-6Al-2Sn-4Zr-2Mo-0.1Si alloy.

Assignments (7)
RELEASE OF SECURITY INTEREST Recorded Nov 20, 2025
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: CARPENTER TECHNOLOGY CORPORATION
Reel/Frame 072983/0743 →
SECURITY INTEREST Recorded Apr 14, 2023
From: CARPENTER TECHNOLOGY CORPORATION
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 063326/0230 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 7, 2017
From: PURIS, LLC
To: CARPENTER TECHNOLOGY CORPORATION
Reel/Frame 041927/0498 →
CORRECTIVE ASSIGNMENT TO CORRECT THE NATURE OF CONVEYANCE PREVIOUSLY RECORDED ON REEL 041024 FRAME 0988. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Jan 24, 2017
From: FMW COMPOSITE SYSTEMS, INC.
To: PURIS, LLC
Reel/Frame 041465/0019 →
SECURITY INTEREST Recorded Jan 20, 2017
From: FMW COMPOSITE SYSTEMS, INC.
To: PURIS, LLC
Reel/Frame 041024/0988 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 22, 2016
From: HANUSIAK, WILLIAM M.
To: FMW COMPOSITE SYSTEMS, INC.
Reel/Frame 040741/0964 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2010
From: YOLTON, C. FRED; BONO, ERIC S.
To: ATI PROPERTIES, INC.
Reel/Frame 025451/0534 →