发明名称 Method of depositing protective coatings on turbine combustion components
摘要 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.
申请公布号 EP2290117(A1) 申请公布日期 2011.03.02
申请号 EP20100173661 申请日期 2010.08.23
申请人 GENERAL ELECTRIC COMPANY 发明人 MARGOLIES, JOSHUA LEE;LAU, YUK-CHIU;BUCCI, DAVID VINCENT
分类号 C23C4/08;C23C4/12;C23C28/00;F01D5/28;H05H1/34 主分类号 C23C4/08
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