Titanium alloy
A titanium alloy which, even under the influence of high application temperatures, has a low tendency to becoming brittle as a result of coarse grain formation, comprises (in wt. %) Fe: ≦2%, Si: 0.01 to 0.8%, 0: ≦0.3%, C: ≦0.1%, one or more elements of the Lanthanide group at total levels of 0.01-2% and, optionally, one or more elements of Al and O at total levels of a maximum of 1%, one or more elements of Mo, Ta, Nb, Zr, Mn, Cr, Co, Ni, Cu, V, Si, and H at total levels of a maximum of 3%, the remainder being titanium and unavoidable impurities.
1. A titanium alloy comprising the following composition (in % by weight)
Fe: ≦2%,
Si: 0.01 to 0.8%,
O: ≦0.3%,
C: ≦0.1%,
Al: ≦0.02 to 1.0%,
one or more lanthanide elements from the group consisting of lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, and ytterbium in contents which total 0.01 to 2%, and
the remainder being titanium and unavoidable impurities.
2. The titanium alloy according to claim 1 , wherein the Fe content is 0.03% to 2% by weight.
3. The titanium alloy according to claim 2 , wherein the Fe content is 0.03 to 0.3% by weight.
4. The titanium alloy according to claim 1 , wherein the Si content is 0.25 to 0.5% by weight.
5. The titanium alloy according to claim 1 , wherein the oxygen content is 0.03% to 0.3% by weight.
6. The titanium alloy according to claim 5 , wherein the oxygen content is 0.03 to 0.25% by weight.
7. The titanium alloy according to claim 1 , wherein the lanthanide element content is 0.5 to 1.0% by weight.
8. The titanium alloy according to claim 1 , comprising at least one of La and Ce as the lanthanide element.
9. The titanium alloy according to claim 1 , comprising at least one of a La and Ce composition metal as the lanthanide element.
10. The titanium alloy according to claim 1 , wherein the amount of Al is 0.05 to 1.0%, by weight, and the amount of O is 0.05 to 0.3% by weight.
11. The titanium alloy according to claim 1 , further comprising one or more elements of the group consisting of Mo, Ta, Nb, Zr, Mn, Cr, Co, Ni, Cu, V, and H in contents of at least 0.03% by weight.
12. The titanium alloy of claim 1 , wherein a combined amount of Al and O is less than or equal to 1% by weight.
13. The titanium alloy of claim 12 further comprising one or more elements from the group consisting of Mo, Ta, Nb, Zr, Mn, Cr, Co, Ni, Cu, V, and H in contents which total a maximum of 3%.
14. The titanium alloy of claim 1 further comprising one or more elements from the group consisting of Mo, Ta, Nb, Zr, Mn, Cr, Co, Ni, Cu, V, and H in contents which total a maximum of 3%.
15. A method of using a titanium alloy, comprising:
receiving a component comprising the titanium alloy comprising the following composition (in % by weight):
Fe: ≦2%,
Si: 0.01 to 0.8%,
O: ≦0.3%,
C: ≦0.1%,
Al: 0.02 to 1.0%,
one or more lanthanide elements from the group consisting of lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, and ytterbium in contents which total 0.01 to 2%,
the remainder being titanium and unavoidable impurities; and
using the component at temperatures greater than 800° C. over a total action time of at least 50 hours.
16. The method of claim 15 wherein the component is part of an exhaust system for an internal-combustion engine.
17. The method of claim 15 wherein the titanium alloy includes a combined amount of Al and O that is less than or equal to 1% by weight.
18. The method of claim 15 wherein the titanium alloy further comprises one or more elements from the group consisting of Mo, Ta, Nb, Zr, Mn, Cr, Co, Ni, Cu, V, and H in contents which total a maximum of 3%.