发明名称 Turbine nozzle with curved recesses in the outer platforms
摘要 <p>A turbine nozzle includes: a hollow, airfoil-shaped turbine vane (14); and an arcuate first band (16, 18) disposed at a first end of the turbine vane (14), the first band (16, 18) having a tlowpath face adjacent the turbine vane (14), arid an opposed back face (56). The back face (56) includes at least one open pocket (58), the at least one pocket (58) defined in part by a bottom wall (66) recessed front the back face (56), opposed ends of the bottom wall (66) merging with the back face (56). The bottom wall (66)is substantially free of interior corners, in order to avoid recirculation and thermal stress due to the secondary air flow "X", coming in the presence of high velocity flow, which creates the streamline "S".</p>
申请公布号 EP2169183(B1) 申请公布日期 2014.03.26
申请号 EP20090171321 申请日期 2009.09.25
申请人 GENERAL ELECTRIC COMPANY 发明人 BRIGGS, ROBERT DAVID;PEARSON, SHAWN MICHAEL;SMITH, JACK WILLARD, JR.;IGLESIAS, DENNIS CENTENO
分类号 F01D9/04;F01D5/18 主分类号 F01D9/04
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