发明申请
US20090180887A1 Turbine Blade With Recessed Tip 审中-公开
涡轮叶片带有凹入尖端

  • 专利标题: Turbine Blade With Recessed Tip
  • 专利标题(中): 涡轮叶片带有凹入尖端
  • 申请号: US12087761
    申请日: 2007-01-15
  • 公开(公告)号: US20090180887A1
    公开(公告)日: 2009-07-16
  • 发明人: Bob MischoReza AbhariThomas Behr
  • 申请人: Bob MischoReza AbhariThomas Behr
  • 国际申请: PCT/EP2007/050336 WO 20070115
  • 主分类号: F01D5/14
  • IPC分类号: F01D5/14
Turbine Blade With Recessed Tip
摘要:
A turbine blade (1) with a side surface (7) having an aerodynamic profile. The turbine blade (1) further comprises an end surface (6) and is mounted in a turbine, whereby the end surface (6) is delimited by a gap from a casing (8) of the turbine. The end surface (6) comprises a recess (2) which is shaped such that it acts as an improved aerodynamic seal.
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