Coated turbine engine components and methods for making the same

Methods for coating a turbine engine rotor component involving depositing at least one platinum group metal selected from platinum, palladium, rhodium, ruthenium, iridium and osmium on the rotor component, and heating the rotor component to a temperature of from about 500°C to about 800°C.

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Bibliographic Details
Main Authors ACKERMAN, JOHN FREDERICK, HEANEY, JOSEPH ALOYSIUS, WEIMER, MICHAEL JAMES, ZIMMERMAN, ROBERT GEORGE, JR, NAGARAJ, BANGALORE ASWATHA
Format Patent
LanguageEnglish
French
German
Published 07.05.2008
Subjects
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Summary:Methods for coating a turbine engine rotor component involving depositing at least one platinum group metal selected from platinum, palladium, rhodium, ruthenium, iridium and osmium on the rotor component, and heating the rotor component to a temperature of from about 500°C to about 800°C.
Bibliography:Application Number: EP20070117608