发明申请
US20140147278A1 VARIABLE-PITCH NOZZLE FOR A RADIAL TURBINE, IN PARTICULAR FOR AN AUXILIARY POWER SOURCE TURBINE
审中-公开
适用于径向涡轮机的可变喷嘴喷嘴,特别适用于辅助电源涡轮机
- 专利标题: VARIABLE-PITCH NOZZLE FOR A RADIAL TURBINE, IN PARTICULAR FOR AN AUXILIARY POWER SOURCE TURBINE
- 专利标题(中): 适用于径向涡轮机的可变喷嘴喷嘴,特别适用于辅助电源涡轮机
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申请号: US14122490申请日: 2012-05-31
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公开(公告)号: US20140147278A1公开(公告)日: 2014-05-29
- 发明人: Jacques Demolis , Laurent Minel , Hubert Hippolyte Vignau
- 申请人: Jacques Demolis , Laurent Minel , Hubert Hippolyte Vignau
- 申请人地址: FR Bordes
- 专利权人: TURBOMECA
- 当前专利权人: TURBOMECA
- 当前专利权人地址: FR Bordes
- 优先权: FR1154801 20110601
- 国际申请: PCT/FR2012/051217 WO 20120531
- 主分类号: F01D9/02
- IPC分类号: F01D9/02
摘要:
A radial turbine nozzle of a turbine engine rotating about a central axis includes a first annular array of fixed blades and a second annular array with a same number of variable-pitch blades. The blades have pressure and suction surfaces. Each variable-pitch blade is connected to cups and is configured to be rotated by a controller about a geometric axis connecting centers of the cups. Each variable-pitch blade is mounted at a distance from the axis of the cups such that this axis of rotation is positioned facing the suction surface of the blade and substantially closer to a trailing edge than to a leading edge of that blade. The nozzle can modify the reduced flow admitted by a radial turbine in accordance with requirements of a thermodynamic cycle and produce a seal in an area of maximum load of the nozzle blades.
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