发明授权
US08573935B2 Helicopter rotor comprising a vibration damper, and method for updating the same 有权
包括减震器的直升机转子及其更新方法

  • 专利标题: Helicopter rotor comprising a vibration damper, and method for updating the same
  • 专利标题(中): 包括减震器的直升机转子及其更新方法
  • 申请号: US12665303
    申请日: 2008-06-19
  • 公开(公告)号: US08573935B2
    公开(公告)日: 2013-11-05
  • 发明人: Santino Pancotti
  • 申请人: Santino Pancotti
  • 申请人地址: IT Samarate
  • 专利权人: Agusta S.p.A.
  • 当前专利权人: Agusta S.p.A.
  • 当前专利权人地址: IT Samarate
  • 代理机构: McCracken & Frank LLC
  • 优先权: ITTO2007A0442 20070620
  • 国际申请: PCT/IB2008/001594 WO 20080619
  • 国际公布: WO2008/155632 WO 20081224
  • 主分类号: B64C27/32
  • IPC分类号: B64C27/32
Helicopter rotor comprising a vibration damper, and method for updating the same
摘要:
A rotor for a helicopter, having: a hub rotating about an axis and in turn having a number of blades; and an at least partly hollow drive shaft connectable to a drive of the helicopter and connected functionally to the hub to rotate the hub about the axis; the rotor also having vibration damping means in turn having a mass, and an elastically deformable member connected to the mass and supported by the shaft; the member extending at least partly inside the shaft, and being elongated parallel to the axis; and the mass vibrating, in use, at such a frequency as to oppose transmission to the shaft of the vibration produced by rotation of the hub and blades.
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