Repair nickel-based superalloy and methods for refurbishment of gas turbine components

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United States of America Patent

APP PUB NO 20060219329A1
SERIAL NO

11093350

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Abstract

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A nickel-based superalloy includes, in terms of weight, about 0.06% to about 0.10% carbon, about 6.0% to about 6.4% aluminum, about 5.8% to about 6.3% tantalum, about 6.5% to about 7.0% chromium, about 8.8% to about 9.3% cobalt, about 0.6% to about 1.0% molybdenum, about 2.4% to about 2.8% rhenium, about 4.8% to about 5.3% tungsten, about 0.3% to about 0.80% hafnium, about 0.01% to about 0.03% zirconium, about 0.10% to about 0.18% silicon, and nickel. A method for repairing a surface of a turbine component includes the step of applying the nickel-based superalloy to a damaged area of the component surface. Post-deposition processes are also performed as necessary.

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Patent Owner(s)

Patent OwnerAddress
HONEYWELL INTERNATIONAL INC855 S MINT STREET CHARLOTTE NC 28202

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bye, Richard L Morristown, NJ 16 156
Hu, Yiping Greer, SC 42 556

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