Method to improve stability of burn-resistant titanium alloy
View Patent ↗A powder metallurgy method includes the steps of forming a member, such as a work piece or an aerospace component, from a titanium alloy powder. The average size of a carbide phase in the titanium alloy powder is controlled in order to control an average size of a carbide phase in the member. In one example, an amount of carbon within the titanium alloy and size of the carbide phase are selected to provide a desirable balance of good hot workability, resisting formation of an alpha-titanium phase within the member and a desired level of fatigue performance.
1. A powder metallurgy method comprising:
(a) forming a member from a titanium alloy powder; and
(b) controlling an average size of a carbide phase in the titanium alloy powder to establish a desired average size of a carbide phase in the member.
2. The powder metallurgy method as recited in claim 1 , wherein said step (a) includes forming the member from a burn-resistant composition of the titanium alloy powder.
3. The powder metallurgy method as recited in claim 1 , wherein the titanium alloy powder includes vanadium, chromium, carbon, and titanium.
4. The powder metallurgy method as recited in claim 1 , wherein the titanium alloy powder includes about 35% vanadium by weight, about 15% chromium by weight, more than 0.05% and less than about 1.2% carbon by weight, and a balance titanium.
5. The powder metallurgy method as recited in claim 1 , wherein the titanium alloy powder includes about 35% vanadium by weight, about 15% chromium by weight, between about 0.25% and about 0.35% carbon by weight, and a balance titanium.
6. The powder metallurgy method as recited in claim 1 , wherein the titanium alloy powder consists essentially of about 35% vanadium by weight, about 15% chromium by weight, about 0.3% carbon by weight, and a balance titanium.
7. The powder metallurgy method .as recited in claim 1 , wherein said step (a) includes compacting the titanium alloy powder.
8. The powder metallurgy method as recited in claim 7 , wherein said step (a) includes heating the titanium alloy powder and applying pressure to the titanium alloy powder.
9. The powder metallurgy method as recited in claim 8 , further including selecting an amount of carbon within the titanium alloy powder that is greater than 0.05% by weight and less than about 1.2% by weight to resist cracking from the heating and pressure.
10. The powder metallurgy method as recited in claim 8 , further including selecting an amount of carbon within the titanium alloy powder that is about 0.3% by weight to resist cracking from the heating and pressure.
11. The powder metallurgy method as recited in claim 8 , wherein said step (a) includes a process selected from one of extruding, forging, and rolling.
12. The powder metallurgy method as recited in claim 1 , wherein said step (b) includes controlling the average size of the carbide phase in the titanium alloy powder such that the desired average size of the carbide phase in the member is less than a predetermined threshold size.
13. The powder metallurgy method as recited in claim 1 , wherein said step (b) includes controlling the average size of the carbide phase in the titanium alloy powder such that the desired average size of the carbide phase in the member is less than about 1 micrometer.
14. The powder metallurgy method as recited in claim 1 , further including selecting an amount of carbon within the titanium alloy powder that is greater than 0.05% by weight and less than about 1.2% by weight to resist formation of an alpha-titanium phase within a beta-titanium matrix at a temperature above 900° F.
15. The powder metallurgy method as recited in claim 1 , wherein said step (b) includes controlling cooling of liquid droplets of the titanium alloy to establish the average size of the carbide phase to be within the desired range.
16. A powder metallurgy method comprising:
(a) forming a first member from a titanium alloy powder having 35% vanadium by weight, about 15% chromium by weight, more than 0.05% and less than about 1.2% carbon by weight, and a balance of titanium, wherein at least a portion of the carbon is within a carbide phase;
(b) heating the first member and applying pressure to the first member to form a second member; and
(c) controlling an average size of the carbide phase in the titanium alloy powder to establish a desired level of resistance to cracking during said step (b).
17. The powder metallurgy method as recited in claim 16 , wherein said step (c) includes controlling the average size of the carbide phase in the titanium alloy powder such that the average size of the carbide phase in the second member is less than about 1 micrometer.
18. A powder metallurgy method comprising:
(a) forming a first member from a titanium alloy powder having 35% vanadium by weight, about 15% chromium by weight, more than 0.05% and less than about 1.2% carbon by weight, and a balance of titanium;
(b) heating the first member and applying pressure to the first member to form a second member;
(c) controlling an average size of a carbide phase in the titanium alloy powder to establish a desired level of resistance to cracking during said step (b);
(d) forming a third member from the second member; and
(e) selecting an amount of the carbon to establish a desired rate of formation of an alpha-titanium phase within a beta-titanium matrix of the third member above a predetermined temperature.
19. The powder metallurgy method as recited in claim 18 , wherein the desired rate of formation of the alpha-titanium phase corresponds to a continuous maximum use temperature of 900° F. for at least 350 h.
20. The powder metallurgy method as recited in claim 18 . wherein said step (c) includes controlling cooling of liquid droplets of the titanium alloy to establish the average size of the carbide phase to be within a desired range.