Heat-treatment of an alloy for a bearing component

Patent metadata

Field	Value
Publication number	US-9732408-B2
Application number	US-201214114677-A
Country	US
Kind code	B2
Filing date	Apr 26, 2012
Priority date	Apr 29, 2011
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A method for preparing titanium alloy that is created to be formed into a bearing component, wherein the titanium alloy comprises from 5 to 7 wt % Al, from 3.5 to 4.5 wt % V, from 0.5 to 1.5 wt % Mo, from 2.5 to 4.5 wt % Fe, from 2.5 to 4.5 wt % Fe, and from 0.05 to 2 wt % Cr. The alloy can optionally include one or more of the following elements: up to 2.5 wt % Zr, up to 2.5 wt % Sn, and up to 0.5 wt % C. The balance of the composition comprises Ti together with unavoidable impurities. The alloy is heated to a temperature T below the (α+β/β)-transition temperature Tβ and then quenched. The alloy is then aged a temperature of from 400 to 600° C.

First claim

The invention claimed is:

1. A method for manufacturing a bearing component selected from the group consisting of a rolling element, an inner ring, and an outer ring, the method comprising:
(i) providing an alloy composition comprising:
5 to 7 wt % Al,
3.5 to 6 wt % V,
0.5 to 6 wt % Mo,
0.2 to 4.5 wt % Fe,
0.05 to 2.5 wt % Cr,
up to 2.5 wt % Zr,
up to 2.5 wt % Sn, and
up to 0.5 wt % C;
the balance being Ti and unavoidable impurities;

(ii) heating the alloy composition to a temperature T below the (α+β/β)-transition temperature T α and then quenching; and
(iii) aging the alloy composition at a temperature of from 400 to 600° C.

2. The method according to claim 1 , wherein after the alloy composition has been heated to the temperature T, it is worked before being quenched.

3. The method according to claim 2 wherein the working comprises rolling the alloy composition.

4. The method according to claim 3 wherein the rolling comprises multiple rolling stages with intermediate annealing stages.

5. The method according to claim 1 wherein the temperature T is greater than the (α/α+β)-transition temperature T α and less than the (α+β/β)-transition temperature T β .

6. The method according to claim 1 wherein the temperature T falls within the range of:
T β >T≧T β −50° C.

7. The method according to claim 1 wherein the temperature T is 820 to 900° C.

8. The method according to claim 1 wherein the quenching is carried out in water.

9. The method according to claim 1 wherein the quenching is performed so that the alloy composition has a microstructure comprising from 10 to 15 vol % α-phase after the quenching.

10. The method according to claim 1 wherein the aging is carried out at a temperature of 425 to 525° C.

11. The method according to claim 10 wherein the aging is carried out 25 to 35 hours.

12. The method according to claim 1 wherein the alloy composition comprises:
5 to 7 wt % Al,
3.5 to 4.5 wt % V,
0.5 to 1.5 wt % Mo,
2.5 to 4.5 wt % Fe,
0.05 to 2 wt % Cr,
up to 2.5 wt % Zr,
up to 2.5 wt % Sn, and
up to 0.5 wt % C,
the balance being Ti and unavoidable impurities.

13. The method according to claim 1 wherein the alloy composition comprises:
5.5 to 6.5 wt % Al,
3.5 to 4.5 wt % V,
0.5 to 1.5 wt % Mo,
3.5 to 4.5 wt % Fe,
0.05 to 2 wt % Cr,
1.5 to 2.5 wt % Zr,
1.5 to 2.5 wt % Sn, and
0.01 to 0.2 wt % C,
the balance being Ti together with unavoidable impurities.

14. The method according to claim 1 wherein the alloy composition comprises:
5 to 7 wt % Al,
3.5 to 6 wt % V,
3 to 6 wt % Mo,
0.2 to 2.5 wt % Fe,
0.1 to 2.3 wt % Cr,
up to 0.7 wt % Zr,
up to 0.7 wt % Sn, and
up to 0.5 wt % C,
the balance being Ti and unavoidable impurities.

15. The method according to claim 1 wherein the quenching is performed so that the alloy composition has a Rockwell harness of at least 50 HRC after the quenching.

16. The method according to claim 1 wherein the alloy composition has a microstructure that comprises β-phase having precipitates of α-phase dispersed therein, the α-phase comprising 10-20 vol % of the microstructure.

17. The method according to claim 1 , further comprising:
machining the alloy composition into a desired shape of the bearing component, the machining being carried out between the quenching and the aging.

18. The method according to claim 17 wherein after the aging, the machining is performed to remove a layer not less than 50 μm in depth from the bearing component.

19. The method according to claim 1 wherein the bearing component is an inner ring or an outer ring.

20. The method according to claim 1 wherein the temperature T is from 835 to 880° C.

21. The method according to claim 20 wherein the quenching is carried out at a rate of at least 20° C./s to a temperature of 60° C. or lower.

22. The method according to claim 21 wherein the aging is performed at 425 to 525° C. degrees C. for about 25-35 hours, and then the bearing component is cooled at a rate of from 2 to 10° C./s.

23. The method according to claim 1 , wherein V is 3.5-4.5 wt %, Mo is 0.5-1.5 wt %, Fe is 2.5-4.5 wt % and Cr is 0.05-2 wt %.

24. The method according to claim 1 wherein the alloy composition has a molybdenum equivalence [Mo] eq that is from 10 to 12, the molybdenum equivalence being calculated according to the following formula:
[Mo] eq =[Mo]+0.2[Ta]+0.28[Nb]+0.4[W]+0.67[V]+1.25[Cr]+1.25[Ni]+1.7[Mn]+1.7[Co]+2.5[Fe].

25. The method according to claim 1 , wherein Al is 6-6.5 wt %.

26. The method according to claim 1 , wherein V is 3.5-4.5 wt %.

27. The method according to claim 1 , wherein Fe is 2.5-4.5 wt %.

28. The method according to claim 1 , wherein Cr is 0.06-1.5 wt %.

29. The method according to claim 1 , wherein Zr is 1-2.5 wt %.

30. The method according to claim 1 , wherein Sn is 1.5-2.5 wt %.

31. The method according to claim 1 , wherein C is 0.015-0.35 wt %.

32. The method according to claim 1 wherein the temperature T falls within the range of:
T β >T≧T β −30° C.

33. The method according to claim 1 wherein the temperature T falls within the range of:
T β −10° C.≧ T≧T β −20° C.

34. A method for manufacturing a bearing component selected from the group consisting of a rolling element, an inner ring, and an outer ring, the method comprising:
(i) providing an alloy composition comprising:
5to 7 wt % Al,
3.5 to 6 wt % V,
0.5 to 1.5 wt % Mo,
0.2 to 4.5 wt % Fe,
0.05 to 2.5 wt % Cr,
up to 2.5 wt % Zr,
up to 2.5 wt % Sn, and
up to 0.5 wt % C;
the balance being Ti and unavoidable impurities;

(ii) heating the alloy composition to a temperature T below the (α+β/β)-transition temperature T β and then quenching; and
(iii) aging the alloy composition at a temperature of from 400 to 600° C.

Assignees

• Sanz Alejandro
• Vries De Alexander
• Skf Ab

Inventors

• Sanz Alejandro
• Vries De Alexander

Classifications

• C22F1/183 Primary

  of titanium or alloys based thereon · CPC title

• F16C33/62

  Selection of substances · CPC title

• F16C2204/42

  Alloys based on titanium · CPC title

• C22C1/02

  by melting {(C22C1/1036 takes precedence)} · CPC title

• C22C14/00

  Alloys based on titanium · CPC title