Component, anti-oxidation coating for such a component and...

Stock material or miscellaneous articles – All metal or with adjacent metals – Composite; i.e. – plural – adjacent – spatially distinct metal...

Reexamination Certificate

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Details

C428S680000, C428S670000, C416S24100B, C427S383700

Reexamination Certificate

active

07662484

ABSTRACT:
A component such as a gas turbine engine component has an oxidation protective layer formed as a substrate surface region in a substrate of the component. The substrate has a nickel-based composition including nickel and an aluminum proportion of greater than 4.5 weight %. The surface region is formed by diffusion of at least platinum into the substrate surface region to provide an integrated platinum proportion of 5 to 40 weight percent over the integration depth range in the surface region.

REFERENCES:
patent: 5482578 (1996-01-01), Rose et al.
patent: 6066405 (2000-05-01), Schaeffer
patent: 0 718 420 (1996-06-01), None
patent: 0 784 104 (1997-07-01), None
patent: 1 076 116 (2001-02-01), None
patent: 1 094 131 (2001-04-01), None

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