发明名称 TURBOMACHINERY BLADE WITH TIP CAP
摘要 A turbomachinery blade including a hollow interior is provided with an improved tip cap comprising first and second members each made of an alloy of a composition and properties different from the other. The first member, in the form of a closure plate bonded to sidewalls of the hollow body, is of a nickel-base or cobalt-base superalloy casting characterized by high mechanical strength properties at elevated temperatures. The second member is a rib of the shape of and bonded to the first member and is of a cast alloy characterized by the combination of resistance to oxidation, sulfidation and thermal fatigue at elevated temperatures. The second member provides an outer tip extension of the blade.
申请公布号 GB2010981(A) 申请公布日期 1979.07.04
申请号 GB19780048407 申请日期 1978.12.13
申请人 GENERAL ELECTRIC CO 发明人
分类号 F01D5/18;F01D5/00;F01D5/20;(IPC1-7):01D5/18 主分类号 F01D5/18
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