Invention Application
- Patent Title: VIBRATION CONTROL WITH ACTIVE LAG DAMPER
- Patent Title (中): 具有活性胶囊阻尼器的振动控制
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Application No.: US14494036Application Date: 2014-09-23
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Publication No.: US20160083088A1Publication Date: 2016-03-24
- Inventor: David E. Heverly, II , Frank B. Stamps , Michael Smith
- Applicant: BELL HELICOPTER TEXTRON INC.
- Main IPC: B64C27/635
- IPC: B64C27/635 ; B64C27/64 ; B64C27/51

Abstract:
A rotor system includes a hub assembly, a first, second, and third rotor blade rotatably attached to the hub assembly, a first, second, and third damper pivotally attached to the hub assembly and pivotally attached to the first, second, and third rotor blade, respectively, and a control system operably associated with the first, second, and third damper. A method to control vibratory forces exerted on the hub assembly via the first and second rotor blade includes separately controlling a dynamic spring rate of each of the first and second dampers with the control system.
Public/Granted literature
- US10112709B2 Vibration control with active lag damper Public/Granted day:2018-10-30
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