发明名称 Method for repairing a superalloy turbine component
摘要 An improved coating and method for applying the coating to minimize the consumption of substrate material during high temperature service by formation of an intermediate metal aluminide layer. A layer of Ni or Co or combinations of Ni and Co are added to the substrate material as an overlay by a process such as electroplating or electroless plating. A diffusion aluminide is then formed at the surface by exposing the plated substrate to a source of aluminum at an elevated temperature.
申请公布号 EP1013786(A1) 申请公布日期 2000.06.28
申请号 EP19990309957 申请日期 1999.12.10
申请人 GE AVIATION SERVICES OPERATION (PTE) LTD. 发明人 CHEN, KENG NAM;HU, GENFA;NGIAM, SHIH TUNG
分类号 F02C7/00;C23C4/00;C23C10/02;C23C10/48;C23C16/34;C23C18/31;C23C30/00 主分类号 F02C7/00
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