Invention Grant
US08435002B2 Helicopter vibration control system and rotating assembly rotary forces generators for canceling vibrations 有权
直升机振动控制系统和旋转组件旋转力发生器,用于消除振动

  • Patent Title: Helicopter vibration control system and rotating assembly rotary forces generators for canceling vibrations
  • Patent Title (中): 直升机振动控制系统和旋转组件旋转力发生器,用于消除振动
  • Application No.: US12637174
    Application Date: 2009-12-14
  • Publication No.: US08435002B2
    Publication Date: 2013-05-07
  • Inventor: Mark R. JollyAndrew D. Meyers
  • Applicant: Mark R. JollyAndrew D. Meyers
  • Applicant Address: US NC Cary
  • Assignee: Lord Corporation
  • Current Assignee: Lord Corporation
  • Current Assignee Address: US NC Cary
  • Agent Richard G. Miller
  • Main IPC: F01D5/10
  • IPC: F01D5/10
Helicopter vibration control system and rotating assembly rotary forces generators for canceling vibrations
Abstract:
A rotary blade rotating hub mounted rotating assembly vibration control system including a first imbalance mass concentration rotor, a second imbalance mass concentration rotor, a third imbalance mass concentration rotor, and a fourth imbalance mass concentration rotor. The first imbalance mass concentration rotor has a first imbalance mass concentration rotor center axis rotation centered on the rotating assembly center rotation axis. The second imbalance mass concentration rotor has a second imbalance mass concentration rotor center axis rotation centered on the rotating assembly center rotation axis. The third imbalance mass concentration rotor has a third imbalance mass concentration rotor center axis rotation centered on the rotating assembly center rotation axis. The fourth imbalance mass concentration rotor has a fourth imbalance mass concentration rotor center axis rotation centered on the rotating assembly center rotation axis. The first and second imbalance mass concentration rotors are driven at a first rotation speed greater than the rotating assembly operational rotation frequency while controlling the rotational position of the first imbalance mass concentration and the second imbalance mass concentration to produce a first rotating net force vector to inhibit a first vibration frequency. The third and fourth imbalance mass concentration rotors are driven at a second rotation speed greater than the rotating assembly operational rotation frequency while controlling the rotational position of the third imbalance mass concentration and the fourth imbalance mass concentration to produce a second rotating net force vector to inhibit a second vibration frequency.
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