Liquid assisted additive manufacturing of a superalloy component
A method is provided that facilitates additive manufacturing a superalloy component using a liquid assisted additive manufacturing process. The method includes successively depositing and fusing together layers of a superalloy powder mixture comprising a high melt superalloy powder and a low melt superalloy powder to build up an additive portion of the superalloy component. The method may further include heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture. Each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture may have a nickel content by weight greater than 40% and have an aluminum content by weight of greater than 1.5%. The low melt superalloy powder may include at least 5% by weight of tantalum, and the high melt superalloy powder may include less than half the content by weight percent of tantalum compared to the content by weight percent of tantalum in the low melt superalloy powder.
1. A method of additively manufacturing comprising:
successively depositing and fusing together layers of a superalloy powder mixture to build up an additive portion; and
heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture, wherein the superalloy powder mixture comprises:
at least 51% by weight a high melt superalloy powder; and
at least 5% by weight a low melt superalloy powder,
wherein the low melt superalloy powder has a solidus temperature lower than the solidus temperature of the high melt superalloy powder by between 50° C. and 220° C.
wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 40%, and have an aluminum content by weight of greater than 1.5%,
wherein the low melt superalloy powder includes at least 10% by weight of tantalum,
wherein the high melt superalloy powder includes at maximum 1% by weight of tantalum, and
wherein the superalloy powder mixture is comprised by weight of about 4% to about 23% chromium, about 4% to about 20% cobalt, 0% to about 8% titanium, about 1.5% to about 8% aluminum, 0% to about 11% tungsten, 0% to about 4% molybdenum, about 1% to about 13% tantalum, 0% to about 0.2% carbon, 0% to about 1% zirconium, 0% to about 4% hafnium, 0% to about 4% rhenium, 0% to about 0.1% yttrium and/or cerium, 0% to about 0.04% boron, 0% to about 2% niobium, 0% to about 1.5% optional incidental elements and unavoidable impurities, and balance nickel.
2. The method according to claim 1 , wherein heat treating includes heating the metal component in a furnace at a temperature at or above 1200° C. for at least for 120 minutes.
3. The method according to claim 1 , wherein the low melt superalloy powder has a liquidus temperature above 1300° C.
4. The method according to claim 1 , wherein the low melt superalloy powder has a solidus temperature below the grain boundary melting temperature of a homogenized base alloy by between 10° C. and 150° C.
5. The method according to claim 1 , wherein the high melt superalloy powder has a solidus temperature between 1350° C. and 1430° C.
6. The method according to claim 1 , wherein the low melt superalloy powder has a solidus temperature between 1210° C. and 1360° C.
7. The method according to claim 1 , wherein during successively depositing and fusing together layers of the superalloy powder mixture, the method includes the deposited superalloy filling cracks and/or preventing cracking in order to reduce the total of lengths of cracks in cross-sections of the additive portion to on average less than 1.0 mm/mm 2 .
8. The method according to claim 7 , wherein the superalloy powder mixture has a composition that prior to heat treating of the additive portion causes the superalloy powder mixture to produce less microcracking as the additive portion cools to room temperature relative to alternatively carrying out the method by building up the additive portion using a powder comprised of only the base alloy.
9. The method according to claim 8 , wherein the less microcracking is achieved without carrying out a hot isostatic pressing operation on the additive portion.
10. The method according to claim 1 , forming γ′ volume fractions in the base alloy that are greater than 50%.
11. The method according to claim 1 , wherein at least 95% by weight of the additive portion is formed from the high melt superalloy powder and the low melt superalloy powder.
12. The method according to claim 1 , wherein the superalloy powder mixture has a total of aluminum and optional titanium content by weight of greater than 4%.
13. The method according to claim 12 , wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have an aluminum content by weight of greater than 4.0%.
14. The method according to claim 13 , wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 45% and an aluminum content by weight of greater than 5.5%.
15. The method according to claim 1 , wherein the low melt superalloy powder includes at least 0.5% by weight of hafnium, and wherein the high melt superalloy powder includes less than half the content by weight percent of hafnium compared to the content by weight percent of hafnium in the low melt superalloy powder.
16. The method according to claim 1 , wherein the low melt superalloy powder includes at least 7% by weight of titanium, and wherein the high melt superalloy powder includes less than half the content by weight percent of titanium compared to the content by weight percent of titanium in the low melt superalloy powder.
17. The method according to claim 1 , wherein the superalloy powder mixture, the high melt superalloy powder, and the low melt superalloy powder each comprise by weight at maximum 0.05% titanium.
18. The method according to claim 1 , wherein at least one of the amounts of chromium, aluminum, or molybdenum in weight percent in the low melt superalloy powder is at least 15% to 75% less than the corresponding weight percent in the high melt superalloy powder.
19. The method according to claim 1 , wherein at least one of the amounts of cobalt or tungsten in weight percent in the high melt superalloy powder is at least 50% to 75% less than the corresponding weight percent in the low melt superalloy powder.
20. A method of additively manufacturing comprising:
successively depositing and fusing together layers of a superalloy powder mixture to build up an additive portion; and
heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture, wherein the superalloy powder mixture comprises:
at least 51% by weight a high melt superalloy powder; and
at least 5% by weight a low melt superalloy powder,
wherein the low melt superalloy powder has a solidus temperature lower than the solidus temperature of the high melt superalloy powder by between 50° C. and 220° C.
wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 40%, and have an aluminum content by weight of greater than 1.5%,
wherein the low melt superalloy powder includes at least 5% by weight of tantalum,
wherein the high melt superalloy powder includes less than half the content by weight percent of tantalum compared to the content by weight percent of tantalum in the low melt superalloy powder,
wherein the superalloy powder mixture is comprised by weight of about 4% to about 23% chromium, about 4% to about 20% cobalt, 0% to about 8% titanium, about 1.5% to about 8% aluminum, 0% to about 11% tungsten, 0% to about 4% molybdenum, about 1% to about 13% tantalum, 0% to about 0.2% carbon, 0% to about 1% zirconium, 0% to about 4% hafnium, 0% to about 4% rhenium, 0% to about 0.1% yttrium and/or cerium, 0% to about 0.04% boron, 0% to about 2% niobium, 0% to about 1.5% optional incidental elements and unavoidable impurities, and balance nickel, and
wherein the low melt superalloy powder comprises by weight at least 8% aluminum.
21. A method of additively manufacturing comprising:
successively depositing and fusing together layers of a superalloy powder mixture to build up an additive portion; and
heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture, wherein the superalloy powder mixture comprises:
at least 51% by weight a high melt superalloy powder; and
at least 5% by weight a low melt superalloy powder,
wherein the low melt superalloy powder has a solidus temperature lower than the solidus temperature of the high melt superalloy powder by between 50° C. and 220° C.
wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 40%, and have an aluminum content by weight of greater than 1.5%,
wherein the low melt superalloy powder includes at least 5% by weight of tantalum,
wherein the high melt superalloy powder includes less than half the content by weight percent of tantalum compared to the content by weight percent of tantalum in the low melt superalloy powder,
wherein the superalloy powder mixture is comprised by weight of about 4% to about 23% chromium, about 4% to about 20% cobalt, 0% to about 8% titanium, about 1.5% to about 8% aluminum, 0% to about 11% tungsten, 0% to about 4% molybdenum, about 1% to about 13% tantalum, 0% to about 0.2% carbon, 0% to about 1% zirconium, 0% to about 4% hafnium, 0% to about 4% rhenium, 0% to about 0.1% yttrium and/or cerium, 0% to about 0.04% boron, 0% to about 2% niobium, 0% to about 1.5% optional incidental elements and unavoidable impurities, and balance nickel, and
wherein the low melt superalloy powder comprises by weight at least 3% hafnium.
22. The method according to claim 21 , wherein the high melt superalloy powder comprises by weight at maximum 0.05% hafnium.
23. A method of additively manufacturing comprising:
successively depositing and fusing together layers of a superalloy powder mixture to build up an additive portion; and
heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture, wherein the superalloy powder mixture comprises:
at least 51% by weight a high melt superalloy powder; and
at least 5% by weight a low melt superalloy powder,
wherein the low melt superalloy powder has a solidus temperature lower than the solidus temperature of the high melt superalloy powder by between 50° C. and 220° C.
wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 40%, and have an aluminum content by weight of greater than 1.5%,
wherein the low melt superalloy powder includes at least 5% by weight of tantalum,
wherein the high melt superalloy powder includes less than half the content by weight percent of tantalum compared to the content by weight percent of tantalum in the low melt superalloy powder,
wherein the superalloy powder mixture is comprised by weight of about 4% to about 23% chromium, about 4% to about 20% cobalt, 0% to about 8% titanium, about 1.5% to about 8% aluminum, 0% to about 11% tungsten, 0% to about 4% molybdenum, about 1% to about 13% tantalum, 0% to about 0.2% carbon, 0% to about 1% zirconium, 0% to about 4% hafnium, 0% to about 4% rhenium, 0% to about 0.1% yttrium and/or cerium, 0% to about 0.04% boron, 0% to about 2% niobium, 0% to about 1.5% optional incidental elements and unavoidable impurities, and balance nickel, and
wherein the low melt superalloy powder comprises by weight at maximum 3.4% cobalt.
24. A method of additively manufacturing comprising:
successively depositing and fusing together layers of a superalloy powder mixture to build up an additive portion; and
heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture, wherein the superalloy powder mixture comprises:
at least 51% by weight a high melt superalloy powder; and
at least 5% by weight a low melt superalloy powder,
wherein the low melt superalloy powder has a solidus temperature lower than the solidus temperature of the high melt superalloy powder by between 50° C. and 220° C.
wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 40%, and have an aluminum content by weight of greater than 1.5%,
wherein the low melt superalloy powder includes at least 5% by weight of tantalum,
wherein the high melt superalloy powder includes less than half the content by weight percent of tantalum compared to the content by weight percent of tantalum in the low melt superalloy powder,
wherein the superalloy powder mixture is comprised by weight of about 4% to about 23% chromium, about 4% to about 20% cobalt, 0% to about 8% titanium, about 1.5% to about 8% aluminum, 0% to about 11% tungsten, 0% to about 4% molybdenum, about 1% to about 13% tantalum, 0% to about 0.2% carbon, 0% to about 1% zirconium, 0% to about 4% hafnium, 0% to about 4% rhenium, 0% to about 0.1% yttrium and/or cerium, 0% to about 0.04% boron, 0% to about 2% niobium, 0% to about 1.5% optional incidental elements and unavoidable impurities, and balance nickel, and
wherein the low melt superalloy powder comprises by weight at least 3.8% tungsten.
25. A method of additively manufacturing comprising:
successively depositing and fusing together layers of a superalloy powder mixture to build up an additive portion; and
heat treating the additive portion to form a homogenized base alloy of which the additive portion is comprised, which base alloy has a chemistry defined by the superalloy powder mixture, wherein the superalloy powder mixture comprises:
at least 51% by weight a high melt superalloy powder; and
at least 5% by weight a low melt superalloy powder,
wherein the low melt superalloy powder has a solidus temperature lower than the solidus temperature of the high melt superalloy powder by between 50° C. and 220° C.
wherein each of the high melt superalloy powder, the low melt superalloy powder, and the superalloy powder mixture have a nickel content by weight greater than 40%, and have an aluminum content by weight of greater than 1.5%,
wherein the low melt superalloy powder includes at least 5% by weight of tantalum,
wherein the high melt superalloy powder includes less than half the content by weight percent of tantalum compared to the content by weight percent of tantalum in the low melt superalloy powder, and
wherein the superalloy powder mixture comprises by weight about 4% to about 23% chromium, about 4% to about 20% cobalt, 0% to about 8% titanium, about 1.5% to about 8% aluminum, at least 9% to about 11% tungsten, 0% to about 4% molybdenum, about 1% to about 13% tantalum, 0% to about 0.2% carbon, 0% to about 1% zirconium, 0% to about 4% hafnium, 0% to about 4% rhenium, 0% to about 0.1% yttrium and/or cerium, 0% to about 0.04% boron, 0% to about 2% niobium, 0% to about 1.5% optional incidental elements and unavoidable impurities, and balance nickel.
26. The method according to claim 1 , wherein the superalloy powder mixture comprises by weight at maximum 6.2% tantalum.
27. The method according to claim 1 , wherein the superalloy powder mixture is deposited and fused together via:
a selective laser melting (SLM) 3D printer to form the additive portion; and/or
a Directed Energy Deposition (DED) nozzle that both provides the superalloy powder mixture and emits an energy beam that melts the superalloy powder mixture to form the additive portion.
28. The method according to claim 1 , wherein the superalloy powder mixture is deposited and fused together via a laser wire deposition (LWD) system, which employs a welding wire to provide the superalloy powder mixture.
29. The method according to claim 1 , wherein the superalloy powder mixture is deposited and fused together with a polymer binder via a binder-based 3D-printer to form the additive portion, wherein at least one heat treatment is carried out in at least one furnace that burns off the binder, sinters the superalloy powder mixture, causes the superalloy powder mixture to at least partially fill in pores in the additive portion, and at least partially homogenizes the additive portion.
30. The method according to claim 1 , wherein the additive portion is built-up on a substrate corresponding to a preexisting metal component having a chemistry that does not correspond to the base alloy.
31. The method according to claim 1 , further comprising brazing the additive portion to a metal component.
32. The method according to claim 30 , wherein the metal component includes greater than 0.05% titanium by weight, wherein the base alloy includes at maximum 0.05% titanium by weight.
33. The method according to claim 31 , wherein the metal component includes a root of a blade.
34. The method according to claim 1 , wherein the ratio of the high melt superalloy powder to the low melt superalloy powder by weight is between 94:06 and 76:24 in the superalloy powder mixture.
35. The method according to claim 1 , wherein the ratio of the high melt superalloy powder to the low melt superalloy powder by weight is between 85:15 and 75:25 in the superalloy powder mixture.