发明名称 Turbine nozzle for air cycle machine
摘要 A turbine nozzle for an air cycle machine includes a disk section with a multiple turbine vanes which each extend for a vane height H, a throat width W defined between each of the multiple of turbine vanes, wherein a ratio W/H is 0.745-0.769.
申请公布号 US8814510(B2) 申请公布日期 2014.08.26
申请号 US201012974159 申请日期 2010.12.21
申请人 Hamilton Sundstrand Corporation 发明人 Colson Darryl A.;Hipsky Harold W.
分类号 F04D29/54;F02C6/12;F01D25/28;F02C9/18 主分类号 F04D29/54
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. A turbine nozzle for an air cycle machine comprising: a disk section with a multiple of turbine vanes which extend for a vane height H relative said disk section, a throat width W defined between each of said multiple of turbine vanes, where a ratio W/H is 0.745-0.769, wherein each of said multiple of turbine vanes have an airfoil profile section defined by a set of points in Table T-1 scaled by a desired factor, said set of points include paired chord and thickness dimensions.
地址 Windsor Locks CT US