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filingDate 2010-08-23^^<http://www.w3.org/2001/XMLSchema#date>
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publicationDate 2011-03-02^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-2290117-A1
titleOfInvention Method of depositing protective coatings on turbine combustion components
abstract A method is provided for high velocity air plasma spraying (APS) application of a protective coating system, such as a bond coat with or without an overlying ceramic thermal barrier coat, to a superalloy metal substrate. Application of MCrAlY alloy bond particles (where M is at least one of iron, cobalt, or nickel) onto the metal substrate is maintained at a particle velocity of at least 400 meters per second (m/s), for example within a range of 400 m/s to 700 m/s. The resulting bond coat on the metal substrate has a surface roughness of about 300 to about 500 µinch Ra, and a density of at least 90% of theoretical density. The protective coating may include a ceramic thermal barrier coat applied over the bond coat by any suitable process.
priorityDate 2009-08-27^^<http://www.w3.org/2001/XMLSchema#date>
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