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
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Application No.: US12637174Application Date: 2009-12-14
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Publication No.: US08435002B2Publication Date: 2013-05-07
- Inventor: Mark R. Jolly , Andrew D. Meyers
- Applicant: Mark R. Jolly , Andrew 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

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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