Component repair using brazed surface textured superalloy foil
US-2015375346-A1 · Dec 31, 2015 · US
US9103003B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9103003-B2 |
| Application number | US-54362309-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 19, 2009 |
| Priority date | Sep 30, 2008 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
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A Ni-based superalloy contains 13.1 to 16.0 percent by mass of Cr, 1.0 to 6.8 percent by mass of Co, 3.0 to 3.4 percent by mass of Al, 4.6 to 5.6 percent by mass of Ti, 2.0 to 4.4 percent by mass of Ta, 3.5 to 4.9 percent by mass of W, 0.1 to 0.9 percent by mass of Mo, 0.3 to 1.4 percent by mass of Nb, 0.05 to 0.20 percent by mass of C, and 0.01 to 0.03 percent by mass of B with the remainder being nickel and inevitable impurities. The superalloy excels in corrosion resistance, oxidation resistance, has high strength, and is used in parts of a gas turbine to be used at high temperature. The resulting gas turbine excels in durability.
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What is claimed is: 1. A casting that is a conventional casting formed of a Ni-based conventional casting superalloy comprising: 13.1 to 16.0 percent by mass of Cr, 1.0 to 6.8 percent by mass of Co, 3.0 to 3.4 percent by mass of Al, more than 5.0 to 5.6 percent by mass of Ti, 2.0 to 4.4 percent by mass of Ta, 3.5 to 4.9 percent by mass of W, 0.1 to 0.9 percent by mass of Mo, 0.3 to 1.4 percent by mass of Nb, 0.05 to 0.20 percent by mass of C, and 0.014 to 0.02 percent by mass B, wi…
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