IP Library Granted Patent US 12,071,678
Granted Patent B2
US 12,071,678 · App. 18/307,474 · Granted Aug 27, 2024

High strength titanium alloys

Inventors: Matias Garcia-Avila (Matthews, NC); John V. Mantione (Indian Trail, NC); Matthew J. Arnold (Charlotte, NC)
Assignee: ATI PROPERTIES LLC
C22C14/00C22F1/183
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Quick Facts
Patent No.
US 12,071,678
App. No.
18/307,474
Granted
Aug 27, 2024
Kind
B2
Abstract

A non-limiting embodiment of a titanium alloy comprises, in weight percentages based on total alloy weight: 2.0 to 5.0 aluminum; 3.0 to 8.0 tin; 1.0 to 5.0 zirconium; 0 to a total of 16.0 of one or more elements selected from the group consisting of oxygen, vanadium, molybdenum, niobium, chromium, iron, copper, nitrogen, and carbon; titanium; and impurities. A non-limiting embodiment of the titanium alloy comprises an intentional addition of tin and zirconium in conjunction with certain other alloying additions such as aluminum, oxygen, vanadium, molybdenum, niobium, and iron, to stabilize the α phase and increase the volume fraction of the α phase without the risk of forming embrittling phases, which was observed to increase room temperature tensile strength while maintaining ductility.

Claims (67)

1. A titanium alloy consisting of, in weight percentages based on total alloy weight:

6.0 to 12.0 vanadium;

3.0 to 8.0 tin;

2.0 to 5.0 aluminum;

1.0 to 5.0 zirconium;

1.0 to 5.0 molybdenum;

0 to 0.25 oxygen;

0 to 0.40 iron;

0 to 0.50 chromium;

0 to 0.05 carbon;

0 to 0.05 nitrogen;

optionally, one or more of niobium and copper;

titanium; and

impurities.

2. The titanium alloy of claim 1 , wherein the titanium alloy consists of, in weight percentages based on total alloy weight:

8.6 to 11.4 vanadium;

4.6 to 7.4 tin;

2.0 to 3.9 aluminum;

1.6 to 3.4 zirconium;

1.0 to 3.0 molybdenum;

0.005 to 0.25 oxygen;

0 to 0.40 iron;

0 to 0.50 chromium;

0 to 0.05 carbon;

0 to 0.05 nitrogen;

optionally, one or more of niobium and copper;

titanium; and

impurities.

3. The titanium alloy of claim 1 , wherein a total content of vanadium and niobium in the titanium alloy is 6.0 to 12.0 weight percent.

4. The titanium alloy of claim 1 , wherein a total content of vanadium and niobium in the titanium alloy is 6.0 to 10.0 weight percent.

5. The titanium alloy of claim 1 , wherein a total content of oxygen, vanadium, molybdenum, niobium, chromium, iron, copper, nitrogen, and carbon in the titanium alloy is no greater than 16.0.

6. The titanium alloy of claim 1 , wherein a total content of aluminum, tin, and zirconium in the titanium alloy is 8 to 15.

7. The titanium alloy of claim 1 , wherein the titanium alloy comprises an aluminum equivalent value of 6.0 to 9.0 and a molybdenum equivalent value of 5.0 to 10.0.

8. The titanium alloy of claim 7 , wherein a ratio of the aluminum equivalent value to the molybdenum equivalent value is 0.6 to 1.3.

9. A titanium alloy comprising, in weight percentages based on total alloy weight:

8.6 to 11.4 vanadium;

4.6 to 7.4 tin;

2.0 to 3.9 aluminum;

1.6 to 3.4 zirconium;

1.0 to 3.0 molybdenum;

0.005 to 0.30 oxygen;

titanium; and

impurities.

10. The titanium alloy of claim 9 , comprising 8.6 to 9.4 vanadium, in weight percent based on total alloy weight.

11. The titanium alloy of claim 9 , comprising 4.6 to 7.0 tin, in weight percent based on total alloy weight.

12. The titanium alloy of claim 9 , comprising 3.0 to 3.9 aluminum, in weight percent based on total alloy weight.

13. The titanium alloy of claim 9 , comprising 2.0 to 3.4 zirconium, in weight percent based on total alloy weight.

14. The titanium alloy of claim 9 , comprising 2.0 to 3.0 molybdenum, in weight percent based on total alloy weight.

15. The titanium alloy of claim 9 , comprising 0.005 to 0.25 oxygen, in weight percent based on total alloy weight.

16. The titanium alloy of claim 9 , wherein the titanium alloy exhibits, at room temperature, an ultimate tensile strength of at least 170 ksi and an elongation of at least 6%.

17. The titanium alloy of claim 9 , wherein the titanium alloy exhibits, at room temperature, an ultimate tensile strength of at least 180 ksi and an elongation of at least 6%.

18. A titanium alloy consisting of, in weight percentages based on total alloy weight:

8.6 to 9.4 vanadium;

4.6 to 7.0 tin;

3.0 to 3.9 aluminum;

2.0 to 3.4 zirconium;

2.0 to 3.0 molybdenum;

0.005 to 0.25 oxygen;

0 to 0.05 carbon;

0 to 0.05 nitrogen;

0 to 0.40 iron;

0 to 0.50 chromium;

optionally, one or more of niobium and copper;

titanium; and

impurities.

19. The titanium alloy of claim 18 , wherein a total content of vanadium and niobium in the titanium alloy is 8.6 to 11.4 weight percent.

20. The titanium alloy of claim 18 , wherein a total content of oxygen, vanadium, molybdenum, niobium, chromium, iron, copper, nitrogen, and carbon in the titanium alloy is no greater than 16.0.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 11, 2024
From: GARCIA-AVILA, MATIAS; MANTIONE, JOHN V.; ARNOLD, MATTHEW J.
To: ATI PROPERTIES LLC
Reel/Frame 067072/0537 →
Continuity (3)
Continuation 17226517 · Apr 9, 2021
Continuation 15972319 · May 7, 2018
Related Publication 20240102133A1 · Mar 28, 2024