Methods for preparing superalloy articles and related articles
US-2018002794-A1 · Jan 4, 2018 · US
US10184166B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10184166-B2 |
| Application number | US-201615198514-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 30, 2016 |
| Priority date | Jun 30, 2016 |
| Publication date | Jan 22, 2019 |
| Grant date | Jan 22, 2019 |
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A method for preparing an article including a nickel-based superalloy is presented. The method includes heat-treating a workpiece including a nickel-based superalloy at a temperature above a 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 gamma-prime precipitate phase having an average particle size less than 250 nanometers at a concentration of at least 10 percent by volume, and is substantially free of a gamma-double-prime phase. An article having a minimum dimension greater than 6 inches is also presented. The article includes a material that has a gamma-prime precipitate phase having an average particle size less than 250 nanometers, and is substantially free of a gamma-double-prime phase.
Opening claim text (preview).
The invention claimed is: 1. A method for preparing an article, comprising: heat-treating a workpiece comprising a nickel-based superalloy at a temperature above a gamma-prime solvus temperature of the nickel-based superalloy, wherein the nickel-based superalloy comprises: from about 0.5 weight percent to about 4 weight percent aluminum; from about 1.5 weight percent to about 7 weight percent niobium, and less than 2 weight percent titanium, less than 2 weight percent tantalum or less than 2 weight percent of a combination of titanium and tantalum, 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; the balance being nickel and wherein there is at least 30 weight percent nickel, 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 less than 1; and cooling the heat-treated workpiece with a cooling rate less than 10 degrees Fahrenheit/minute from the temperature above the gamma-prime solvus temperature of the nickel-based superalloy to a temperature below the gamma-prime solvus temperature of the nickel-based superalloy so as to obtain a cooled workpiece comprising a gamma-prime precipitate phase at a concentration of at least 20 percent by volume of a material of the cooled workpiece and having an average particle size less than 100 nanometers, wherein the cooled workpiece is substantially free of a gamma-double-prime phase. 2. An article comprising: a material comprising: from about 0.5 weight percent to about 4 weight percent aluminum; from about 1.5 weight percent to about 7 weight percent niobium, and less than 2 weight percent titanium, less than 2 weight percent tantalum or less than 2 weight percent of a combination of titanium and tantalum, 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 bout 0.2 weight percent of carbon from 0 weight percent to about 0.1 weight percent of boron or combinations thereof, the balance being nickel and wherein there is at least 30 weight percent nickel 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 less than 1; wherein the material further comprises a gamma-prime precipitate phase having an average particle size less than 100 nanometers dispersed within the material at a concentration of at least 10 percent by volume of the material, and wherein the material is substantially free of a gamma-double-prime phase, and wherein the article has a minimum dimension greater than 6 inches. 3. The article of claim 2 , wherein the article has a minimum dimension greater than 8 inches.
of nickel or cobalt or alloys based thereon · CPC title
with the maximum Cr content being at least 10% but less than 20% · CPC title
with chromium · CPC title
with the maximum Cr content being at least 20% but less than 30% · CPC title
based on nickel · CPC title
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