发明名称 Method for repairing a superalloy turbine component
摘要 <p>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.</p>
申请公布号 EP1013786(B1) 申请公布日期 2004.09.15
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;(IPC1-7):C23C4/00 主分类号 F02C7/00
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