Methods for preparing superalloy articles and related articles
A method for preparing an improved article including a nickel-based superalloy is presented. The method includes heat-treating a workpiece including a nickel-based superalloy at a temperature above the gamma-prime solvus temperature of the nickel-based superalloy and cooling the heat-treated workpiece with a cooling rate less than 50 degrees Fahrenheit/minute from the temperature above the gamma-prime solvus temperature of the nickel-based superalloy so as to obtain a cooled workpiece. The cooled workpiece includes a coprecipitate of a gamma-prime phase and a gamma-double-prime phase, wherein the gamma-prime phase of the coprecipitate has an average particle size less than 250 nanometers. An article having a minimum dimension greater than 6 inches is also presented. The article includes a material having a coprecipitate of a gamma-prime phase and a gamma-double-prime phase, wherein the gamma-prime phase of the coprecipitate has an average particle size less than 250 nanometers.
1. An article comprising:
a material comprising:
at least 30 weight percent nickel;
from about 0.1 weight percent to about 6 weight percent titanium, from about 0.1 weight percent to about 6 weight percent tantalum or from about 0.1 weight percent to about 6 weight percent of a combination of titanium and tantalum;
from about 0.1 weight percent to about 6 weight percent aluminum; and
from about 0.5 weight percent to about 9 weight percent niobium,
wherein an atomic ratio of titanium to aluminum, an atomic ratio of tantalum to aluminum or an atomic ratio of the combination of titanium and tantalum to aluminum is in a range from about 0.2 to about 2;
wherein the material further comprises a coprecipitate comprising a gamma-prime phase and a gamma-double-prime phase dispersed within a matrix phase at a concentration of at least 10 percent by volume of the material, wherein the gamma-prime phase has an average particle size less than 250 nanometers,
wherein the article has a minimum dimension greater than 6 inches.
2. The article of claim 1 , wherein the material comprises:
from about 0.2 weight percent to about 4 weight percent titanium, from about 0.2 weight percent to about 4 weight percent tantalum or from about 0.2 weight percent to about 4 weight percent of a combination of titanium and tantalum;
from about 0.2 weight percent to about 3 weight percent aluminum; and
from about 1.5 weight percent to about 7 weight percent niobium.
3. The article of claim 1 , wherein the material further comprises from about 10 weight percent to about 30 weight percent chromium, from 0 weight percent to about 45 weight percent cobalt, from 0 weight percent to about 40 weight percent iron, from 0 weight percent to about 4 weight percent molybdenum, from 0 weight percent to about 4 weight percent tungsten, from 0 weight percent to about 2 weight percent of hafnium, from 0 weight percent to about 0.1 weight percent of zirconium, from 0 weight percent to about 0.2 weight percent of carbon, from 0 weight percent to about 0.1 weight percent of boron or combinations thereof.
4. The article of claim 1 , wherein the gamma-prime phase has an average particle size less than 200 nanometers.
5. The article of claim 1 , wherein the gamma-prime phase has an average particle size less than 100 nanometers.
6. The article of claim 1 , wherein the article has a minimum dimension greater than 8 inches.
7. The article of claim 1 , wherein the coprecipitate comprises the gamma-prime phase in direct contact with the gamma-double-prime phase.
8. The article of claim 1 , wherein the article is one or more of a disk, vane, blade, or shroud of an engine.
9. The article of claim 1 , wherein the material further comprises from about 0.1 weight percent to about 0.2 weight percent of carbon.