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Patent/Software
Synthetic Diamond Overlays for Gas Turbine Engine Parts Having Thermal Barrier Coatings
Author(s)
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.
Date Published:
1995
Citations:
Lemelson, Jerome, James Gerard Conley. 1995. Synthetic Diamond Overlays for Gas Turbine Engine Parts Having Thermal Barrier Coatings.