| 发明名称 |
Turbine Nozzle and Shroud |
| 摘要 |
A nozzle and shroud for use in an air cycle machine has a plate and a shroud curving in a first axial direction about a center axis of the shroud relative to the plate. A plurality of vanes extends in a second axial direction away from the plate. The plurality of vanes extends for a height away from the plate and a width defined as the closest distance between two adjacent vanes, with a ratio of the height to the width being between 1.7377 and 2.1612. An air cycle machine and a method of repair are also disclosed. |
| 申请公布号 |
US2014321978(A1) |
申请公布日期 |
2014.10.30 |
| 申请号 |
US201313869045 |
申请日期 |
2013.04.24 |
| 申请人 |
HAMILTON SUNDSTRAND CORPORATION |
发明人 |
Beers Craig M.;McAuliffe Christopher |
| 分类号 |
F01D9/02 |
主分类号 |
F01D9/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A nozzle and shroud for use in an air cycle machine comprising:
a plate and a shroud curving in a first axial direction about a center axis of said shroud relative to said plate; a plurality of vanes extending in a second axial direction away from said plate, with said plurality of vanes extending for a height away from said plate and a width being defined as the closest distance between two adjacent vanes, with a ratio of said height to said width being between 1.7377 and 2.1612. |
| 地址 |
Windsor Locks CT US |
