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
  • 申请号: US14122490
    申请日: 2012-05-31
  • 公开(公告)号: US20140147278A1
    公开(公告)日: 2014-05-29
  • 发明人: Jacques DemolisLaurent MinelHubert Hippolyte Vignau
  • 申请人: Jacques DemolisLaurent MinelHubert 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
VARIABLE-PITCH NOZZLE FOR A RADIAL TURBINE, IN PARTICULAR FOR AN AUXILIARY POWER SOURCE TURBINE
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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