Helicopter with an improved vibration control device

Details Helicopter with an improved vibration control device Helicopter with an improved vibration control device

B - Operations, Transporting

64

C

B64C 27/32 (2006.01) B64D 47/00 (2006.01)

Patent

CA 2546354

A helicopter having a rotor, a fuselage connected to the rotor by connecting means, and a control device for controlling vibration of the fuselage; the control device including generating means for generating signals associated with vibration of the fuselage, and actuating means for producing a force on the fuselage associated with the signals to reduce vibration; and the actuating means being carried by the connecting means.

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