发明名称 Method for aluminizing serpentine cooling passages of jet engine blades
摘要 Disclosed herein is a method for aluminiding an internal passage of a metal substrate comprising injecting a slurry composition that comprises a powder comprising aluminum, a binder selected from the group consisting of colloidal silica, an organic resin, and a combination thereof, into the internal passage; applying compressed air to the internal passage to facilitate distribution of the slurry composition throughout the internal passage; and, heat treating the slurry composition under conditions sufficient to remove volatile components from the composition, and to cause diffusion of aluminum into a surface of the internal passage.
申请公布号 US7829142(B2) 申请公布日期 2010.11.09
申请号 US20060425555 申请日期 2006.06.21
申请人 GENERAL ELECTRIC COMPANY 发明人 KOOL LAWRENCE BERNARD;RUCKER MICHAEL HOWARD
分类号 B05D3/02;B05D7/14;B05D7/22 主分类号 B05D3/02
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