Diffusion barrier and protective coating for turbine engine...

Details Diffusion barrier and protective coating for turbine engine... Diffusion barrier and protective coating for turbine engine...

2005-08-23

2005-08-23

McNeil, Jennifer (Department: 1775)

Stock material or miscellaneous articles

Composite

Of metal

C428S698000, C428S472000, C428S701000, C428S702000, C416S24100B, C416S24100B

Reexamination Certificate

active

06933052

ABSTRACT:
A turbine engine component comprising a substrate made of a nickel-base or cobalt-base superalloy, a non-metallic oxide or nitride diffusion barrier layer overlying the substrate, and a protective coating overlying the barrier layer, the protective coating comprising at least one platinum group metal selected from the group consisting of platinum, palladium, rhodium, ruthenium and iridium. The diffusion barrier layer may be a deposited or thermally grown oxide material, especially aluminum oxide. The protective coating may be heat treated to increase homogeneity of the coating and adherence with the substrate. The component typically further comprises a ceramic thermal barrier coating overlying the protective coating. Also disclosed are methods for forming a protective coating system on the turbine engine component by forming the non-metallic oxide or nitride diffusion barrier layer on the substrate and then depositing the platinum group metal on top of the barrier layer.

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