发明名称 METHOD OF DEPOSITING PROTECTIVE COATING ON TURBINE COMBUSTION COMPONENT
摘要 <P>PROBLEM TO BE SOLVED: To provide a method for high velocity air plasma spraying (APS) of a protective coating system, such as a bond coat with or without an overlying ceramic thermal barrier coat, to a superalloy metal substrate. <P>SOLUTION: 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 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 500 &mu;inch Ra, and a density of at least 90% of theoretical density. The protective coating may include a ceramic thermal battier coat applied over the bond coat by any suitable process. <P>COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011047049(A) 申请公布日期 2011.03.10
申请号 JP20100183551 申请日期 2010.08.19
申请人 GENERAL ELECTRIC CO 发明人 MARGOLIES JOSHUA LEE;LAU YUK-CHIU;BUCCI DAVID VINCENT
分类号 C23C4/12;C23C4/06;C23C4/10 主分类号 C23C4/12
代理机构 代理人
主权项
地址