Hybrid device for vibration control

Details Hybrid device for vibration control Hybrid device for vibration control

B - Operations, Transporting

64

C

B64C 27/00 (2006.01) B64C 27/51 (2006.01) F16F 15/10 (2006.01)

Patent

CA 2664264

Disclosed herein are control systems relating generally to the field of aerodynamics and more particularly to the control of vibration of rotor blades such as helicopter blades. Such systems involve devices for vibration control of each rotor blade, which incorporate control systems of the flow control type (e.g. actively controlled flap) and structural control type (e.g. active pitch link). Also disclosed are related methods of controlling vibration in a rotor blade, wherein the rotor blade is coupled to a rotor hub and has at least a torsional stiffness and a pitch angle associated therewith.

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