| 发明名称 |
VARIABLE AREA TURBINE NOZZLE WITH A POSITION SELECTOR |
| 摘要 |
A gas turbine engine (100) variable nozzle (460) includes an outer shroud (461), an inner shroud (462), a variable nozzle airfoil (463), and a position selector (470). The inner shroud (462) is located radially inward from the outer shroud (461). The variable nozzle airfoil (463) extends radially between the outer shroud (461) and the inner shroud (462). The variable nozzle airfoil (463) includes a vane shaft (464) extending radially outward from the variable nozzle airfoil (463) through the outer shroud (461). The position selector (470) is coupled with the variable nozzle airfoil (463) to fixedly lock the variable nozzle airfoil (463) into one of a plurality of preselected positions. |
| 申请公布号 |
US2014154046(A1) |
申请公布日期 |
2014.06.05 |
| 申请号 |
US201213660849 |
申请日期 |
2012.10.25 |
| 申请人 |
Solar Turbines Incorporated |
发明人 |
Hensley John James;Stang Ulrich Edmund |
| 分类号 |
F01D17/14 |
主分类号 |
F01D17/14 |
| 代理机构 |
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代理人 |
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| 主权项 |
1. A gas turbine engine variable nozzle, comprising:
an outer shroud; an inner shroud located radially inward from the outer shroud; a variable nozzle airfoil extending radially between the outer shroud and the inner shroud, the variable nozzle airfoil including a vane shaft extending radially outward from the variable nozzle airfoil through the outer shroud; and a position selector coupled with the variable nozzle airfoil to fixedly lock the variable nozzle airfoil into one of a plurality of preselected positions.
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| 地址 |
US |
