发明授权
US3671140A Damped turbomachine rotor assembly 失效
阻尼涡轮转子总成

  • 专利标题: Damped turbomachine rotor assembly
  • 专利标题(中): 阻尼涡轮转子总成
  • 申请号: US3671140D
    申请日: 1970-10-05
  • 公开(公告)号: US3671140A
    公开(公告)日: 1972-06-20
  • 发明人: SHANK WAYNE C
  • 申请人: AVCO CORP
  • 专利权人: Avco Corp
  • 当前专利权人: Avco Corp
  • 优先权: US7796970 1970-10-05
  • 主分类号: F01D5/04
  • IPC分类号: F01D5/04 F01D25/28
Damped turbomachine rotor assembly
摘要:
THE DISCLOSURE ILLUSTRATES A CENTRIFUGAL COMPRESSOR COMPRISING AN INDUCE HUB TELESCOPED OVER AN ADJACENT SHOULDER OF AN IMPELLER HUB. THE INDUCER HUB HAS AN INNER ANNULAR SURFACE WHICH RECEIVES AN ANNULAR RELATIVELY THIN SPLIT RING ELEMENT. WHEN THE COMPRESSOR ROTATES AT HIGH R.P.M''S THE SPLIT RING FRICTIONALLY ENGAGES THE INNER ANNULAR SURFACE OF THE INDUCER HUB TO DAMP VIBRATIONS.
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