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 |