Welded component, a welded gas turbine component, and a process of welding a component
A welded component, a welded gas turbine component, and a process of welding a component are disclosed. The welded component includes a first alloy, a second alloy, and a weld positioned between the first alloy and the second alloy. The weld is formed by a first shim and a second shim being beam welded.
1. A welded component, comprising:
a first alloy subcomponent;
a second alloy subcomponent; and
a weld between the first alloy subcomponent and the second alloy subcomponent;
wherein the weld includes a gradient having a transition region, the transition region formed by a plurality of shims;
wherein the gradient includes a first welded shim composition at least partially formed by welding of a first shim having a first shim composition, a second welded shim composition at least partially formed by welding of a second shim having a second shim composition, a shim-shim transition composition between the first welded shim composition and the second welded shim composition, a first shim-alloy transition composition between the first welded shim composition and the first alloy subcomponent, and a second shim-alloy transition composition between the second welded shim composition and the second alloy subcomponent;
wherein the first shim composition includes a nickel-based alloy including, by weight, up to about 22% chromium;
wherein the gradient has a gradient composition, the gradient composition increasing or decreasing in concentration, by weight, of one or both of aluminum and titanium front the first alloy subcomponent, through the first welded shim composition, through the shim-shim transition composition, through the second welded shim composition, to the second alloy subcomponent.
2. The welded component of claim 1 , wherein the first alloy subcomponent has a first subcomponent composition and the second alloy subcomponent has a second subcomponent composition, the first subcomponent composition differing from the second subcomponent composition.
3. The welded component of claim 2 , wherein the first subcomponent composition is a nickel-based alloy including, by weight, up to about 15% chromium, up to about 10% cobalt, up to about 4% tungsten, up to about 2% molybdenum, up to about 5% titanium, up to about 3% aluminum, and up to about 3% tantalum.
4. The welded component of claim 2 , wherein the first subcomponent composition is a nickel-based alloy including, by weight, up to about 10% chromium, up to about 8% cobalt, up to about 4% titanium, up to about 5% aluminum, up to about 6% tungsten, and up to about 5% tantalum.
5. The welded component of claim 2 , wherein the first subcomponent composition is a nickel-based alloy including, by weight, up to about 8% cobalt, up to about 7% chromium, up to about 6% tantalum, up to about 7% aluminum, up to about 5% tungsten, up to about 3% rhenium, and up to about 2% molybdenum.
6. The welded component of claim 2 , wherein the first subcomponent composition is a nickel-based alloy including, by weight, up to about 10% chromium, up to about 8% cobalt, up to about 5% aluminum, up to about 4% titanium, up to about 2% molybdenum, up to about 6% tungsten, and up to about 5% tantalum.
7. The welded component of claim 2 , wherein the first subcomponent composition is nickel-based alloy including, by weight, up to about 10% cobalt, up to about 8% chromium, up to about 10% tungsten, up to about 6% aluminum, up to about 3% tantalum, and up to about 2% hafnium.
8. The welded component of claim 1 , wherein the first welded shim composition and the second welded shim composition have substantially identical thicknesses.
9. The welded component of claim 1 , wherein the first welded shim composition and the second welded shim composition have different thicknesses.
10. The welded component of claim 1 , wherein the nickel-based alloy includes, by weight, up to about 13% cobalt, up to about 3% iron, and up to about 9% molybdenum.
11. The welded component of claim 1 , wherein the nickel-based alloy includes, by weight, up to about 3% iron, up to about 20% chromium, and up to about 3% manganese.
12. The welded component of claim 1 , wherein the nickel-based alloy includes, by weight, up to about 14% tungsten, and up to about 2% molybdenum.
13. The welded component of claim 1 , wherein the gradient further includes a third welded shim composition at least partially formed by welding of a third shim having a third shim composition within the shim-shim transition composition: wherein the shim-shim transition composition also includes a first-third shim-shim transition composition between the first welded shim composition and the third welded shim composition, and a second-third shim-shim transition composition between the second welded shim composition and the third welded shim composition.
14. The welded component of claim 13 , wherein the first welded shim composition and the third welded shim composition have different thicknesses.
15. The welded component of claim 1 , wherein the component is a gas turbine component.
16. The welded component of claim 1 , wherein the gradient further comprises a shim-shim transition region between the first welded shim composition and the second welded shim composition.
17. A welded gas turbine component, comprising:
a first alloy;
a second alloy; and
a weld positioned between the first alloy and the second alloy;
wherein the weld is formed by a first shim and a second shim being beam welded, the first shim and the second shim forming a transition region of a gradient within the weld;
wherein the first shim includes a first composition compatible with the first alloy, the second shim includes a second composition compatible with the second alloy, and the first shim and the second shim include compatible compositions;
wherein the gradient has a gradient composition, the gradient composition increasing or decreasing in concentration, by weight; of one or both of aluminum and titanium from the first alloy, throughout both of the first composition and the second composition, to the second alloy.
18. A process of welding a component, comprising:
positioning a first alloy subcomponent;
positioning a second alloy subcomponent;
positioning a first shim and a second shim between the first alloy subcomponent and the second alloy subcomponent; and
beam welding the first alloy subcomponent, the second alloy subcomponent, the first shim and the second shim to form the welded component of claim 1 .
19. The process of claim 18 , wherein the beam welding is electron beam welding.