Synthetic diamond overlays for gas turbine engine parts having t

Coating processes – Coating by vapor – gas – or smoke – Carbon or carbide coating

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427577, 427566, 427456, 4274192, 427404, 427124, C23C 1626, C23C 408, B05D 306

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active

057142025

ABSTRACT:
This invention discloses methods of making new and improved multi-layer coatings for gas turbine engine parts that are exposed to elevated temperatures, such as blades and vanes in the high pressure compressor and turbine of multi-stage aircraft engines, by applying a diamond film over columnar thermal barrier coatings such as yttria-stabilized zirconia, improving the erosion resistance of the thermal barrier coating.

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