High temperature turbine engine alloys containing gold

Alloys or metallic compositions – Nickel base – Chromium containing

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420588, C22C 1905, C22C 3000

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active

053743938

ABSTRACT:
Turbine engine alloys modified by the addition of small amounts of gold are found to have improved properties over similar alloys that do not contain Au. These improved alloys have special application in gas turbines and jet engines. A preferred composition range is (46 to 59) wt % Ni-(10 to 14) wt % Co-(15 to 20) wt % Cr-(1 to 1.5) wt % Al-(2.2 to 3.2) wt % Ti-(3.3 to 4.4) wt % Mo-(0.02 to 0.08) wt % C-(0.05 to 0.06) wt % Zr-(0.004 to 0.006) wt % B-(0.02 to 20) wt % Au.

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