发明名称 GAS TURBINE TIP SHROUD RAILS
摘要 <p>A tip shroud rail for a tip shroud of at least one turbine rotor blade, the tip shroud rail comprising a base integrally attached to the tip shroud, a top distally positioned from the base, an upstream surface, and a downstream surface, wherein the tip shroud rail has a height, h, as measured from the base to the top, and a width, w, as measured from the upstream surface to the downstream surface, wherein the width, w, of the tip shroud rail, as measured at the top, is greater than the width, w, of the tip shroud rail, as measured at one-half the height, h/2, of the tip shroud rail.</p>
申请公布号 WO2005061854(A1) 申请公布日期 2005.07.07
申请号 WO2004US41027 申请日期 2004.12.08
申请人 WATSON COGENERATION COMPANY;INGISTOV, STEVEN 发明人 INGISTOV, STEVEN
分类号 F01D5/14;F01D5/20;F01D5/22;F01D11/08;(IPC1-7):F01D5/20 主分类号 F01D5/14
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