发明授权
US07575412B2 Anti-stall casing treatment for turbo compressors 有权
涡轮压缩机的防失速套管处理

  • 专利标题: Anti-stall casing treatment for turbo compressors
  • 专利标题(中): 涡轮压缩机的防失速套管处理
  • 申请号: US10505971
    申请日: 2003-02-05
  • 公开(公告)号: US07575412B2
    公开(公告)日: 2009-08-18
  • 发明人: Peter Seitz
  • 申请人: Peter Seitz
  • 申请人地址: DE Munich
  • 专利权人: MTU Aero Engines GmbH
  • 当前专利权人: MTU Aero Engines GmbH
  • 当前专利权人地址: DE Munich
  • 代理机构: Crowell & Moring LLP
  • 优先权: DE2002/1688 20020228
  • 国际申请: PCT/IB03/00371 WO 20030205
  • 国际公布: WO03/072949 WO 20030904
  • 主分类号: F01D25/24
  • IPC分类号: F01D25/24
Anti-stall casing treatment for turbo compressors
摘要:
A compressor includes a casing defining a generally cylindrical flow passage, a rotor carrying at least one set of rotor blades, at least one set of stator blades, and anti-stall casing treatment. The casing treatment includes an annular recess in the casing for removing low momentum flow adjacent the tips of the rotor blades, and returning the flow to the generally cylindrical flow passage upstream of the point of removal. A plurality of curved guide vanes are located within the annular recess so as to define an annular inlet downstream of the vanes and/or an annular outlet upstream of the vanes. Each guide vane projects radially inwardly from the casing towards a free end which is exposed at or near the mouth of the recess to define a series of curved channels within the recess adjacent the annular inlet and/or the annular outlet.
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