Method of additively manufacturing or welding with a superalloy powder mixture
A superalloy powder mixture is provided for use with additive manufacturing or welding metal components or portions thereof that includes a high melt superalloy powder and a low melt superalloy powder. 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, 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, greater than 40% nickel, greater than 4% in total of aluminum and optional titanium content. 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.
1 . A method of additively manufacturing or welding a metal component 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 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, greater than 40% nickel, greater than 4% in total of aluminum and optional titanium,
wherein the superalloy powder mixture is comprised of:
at least 51% by weight of a high melt superalloy powder comprising by weight at maximum 1.0% tantalum, at least 1.5% aluminum, and greater than 40% nickel; and
at least 5% by weight of a low melt superalloy powder having a solidus temperature at least 50° C. lower than the solidus temperature of the high melt superalloy powder, having a liquidous temperature above 1300° C., and comprising by weight at least 5% tantalum, at least 1.5% aluminum, and greater than 40% nickel, and 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.
2 . The method according to claim 1 , wherein the high melt superalloy powder comprises by weight at maximum 0.05% tantalum.
3 . The method according to claim 1 , wherein the high melt superalloy powder comprises by weight at maximum 0.05% titanium.
4 . The method according to claim 1 , wherein the high melt superalloy powder comprises by weight at least 12% chromium.
5 . The method according to claim 1 , wherein the high melt superalloy powder comprises by weight at least 10.6% tungsten.
6 . A method of additively manufacturing or welding a metal component 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 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, greater than 40% nickel, greater than 4% in total of aluminum and optional titanium,
wherein the superalloy powder mixture is comprised of:
at least 51% by weight of a high melt superalloy powder comprising by weight at maximum 4.5 tantalum, at least 1.5% aluminum, and greater than 40% nickel; and
at least 5% by weight of a low melt superalloy powder having a solidus temperature at least 50° C. lower than the solidus temperature of the high melt superalloy powder, having a liquidous temperature above 1300° C., and comprising by weight at maximum 3.4% cobalt, at least 5% tantalum, at least 1.5% aluminum, and greater than 40% nickel, and 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.
7 . A method of additively manufacturing or welding a metal component 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 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, greater than 40% nickel, greater than 4% in total of aluminum and optional titanium,
wherein the superalloy powder mixture is comprised of:
at least 51% by weight of a high melt superalloy powder comprising by weight at maximum 4.5 tantalum, at least 1.5% aluminum, and greater than 40% nickel; and
at least 5% by weight of a low melt superalloy powder having a solidus temperature at least 50° C. lower than the solidus temperature of the high melt superalloy powder, having a liquidous temperature above 1300° C., and comprising by weight at least 5% tantalum, at least 8.0% aluminum, and greater than 40% nickel, and 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.
8 . The method according to claim 1 , wherein the low melt superalloy powder comprises by weight at least 3.8% tungsten.
9 . The method according to claim 1 , wherein the low melt superalloy powder comprises by weight about 10% to about 20% tantalum.
10 . A method of additively manufacturing or welding a metal component 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 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, greater than 40% nickel, greater than 4% in total of aluminum and optional titanium,
wherein the superalloy powder mixture is comprised of:
at least 51% by weight of a high melt superalloy powder comprising by weight at maximum 4.5 tantalum, at least 1.5% aluminum, and greater than 40% nickel; and
at least 5% by weight of a low melt superalloy powder having a solidus temperature at least 50° C. lower than the solidus temperature of the high melt superalloy powder, having a liquidous temperature above 1300° C., and comprising by weight at least 3% hafnium, at least 5% tantalum, at least 1.5% aluminum, and greater than 40% nickel, and 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.
11 . The method according to claim 7 , wherein the high melt superalloy powder comprises the following composition in weight %:
Cr
7.7-18
Co
10.6-11
Ti
0-2
Al
4.5-6.5
W
10.6-11
Mo
0.30-0.55
Ta
0-1
C
0.05-0.08
Zr
0-1
Hf
0-0.05
Re
0-0.05
Y and/or Ce
0-0.1
B
0-0.04
the balance nickel and optional incidental elements and unavoidable impurities; and
wherein the low melt superalloy powder comprises the following composition in weight %:
Cr
9.5-10.5
Co
2.9-3.4
Ti
0-2
Al
8-9
W
3.8-4.3
Mo
0.8-1.2
Ta
10-20
C
0-0.08
Zr
0-1
Hf
3-12
Re
0-0.05
Y and/or Ce
0-0.1
B
0-0.04
the balance nickel and optional incidental elements and unavoidable impurities.
12 . The method according to claim 11 , wherein the high melt superalloy powder and the low melt superalloy powder comprise by weight at maximum 0.01% of one or more unavoidable impurities.
13 . The method according to claim 11 , wherein the high melt superalloy powder and the low melt superalloy powder comprises by weight at maximum 1.5% of one or more incidental elements other than Cr, Co, Ti, Al, W, Mo, Ta, C, Zr, Hf, Re, Y, Ce and B.
14 . The method according to claim 11 , wherein the high melt superalloy powder and the low melt superalloy powder comprise one or more incidental elements selected from the following with a respective maximum weight percent or maximum ppm as indicated:
S
30
ppm
Nb
1.5%
Mn
0.6%
Fe
0.05%
Si
0.30%
P
50
ppm
Mg
50
ppm
Cu
0.01%
N
60
ppm
O
250
ppm
Ag
1
ppm
As
5
ppm
Bi
0.1
ppm
Cd
2
ppm
Ga
25
ppm
In
0.2
ppm
Pb
2
ppm
Sb
2
ppm
Se
1
ppm
Sn
10
ppm
Te
0.1
ppm
Tl
0.2
ppm
Zn
5
ppm
V
1.5%.
15 . The method according to claim 11 , wherein for the high melt superalloy powder and the low melt superalloy powder the unavoidable impurities are within the maximum amounts for the respective incidental elements and for any other elements that maximum is 0.001% by weight.
16 . The method according to claim 1 ,
wherein heat treating the additive portion includes heat treating the additive portion at a temperature at or above 1200° C. to form the homogenized base alloy of which the additive portion is comprised.
17 . 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.
18 . 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.
19 . 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.