Method and system for reducing engine induced vibration...

Details Method and system for reducing engine induced vibration... Method and system for reducing engine induced vibration...

B - Operations, Transporting

64

D

B64D 47/00 (2006.01) B64C 13/16 (2006.01) B64C 17/00 (2006.01) B64D 27/00 (2006.01) B64D 33/00 (2006.01) F16F 15/00 (2006.01) F16F 15/02 (2006.01)

Patent

CA 2436928

Vertical and/or lateral acceleration sensors are mounted in or on the engines or pylons of an aircraft to measure the vibrations induced by the operating dynamics of the engines. The sensors provide measured vibration signals to a controller that generates control signals in response to and dependent on the measured vibration signals. The control signals are provided to the aileron actuators, so as to actuate the ailerons appropriately to counteract and thereby reduce the engine-induced vibrations. Thus, the engine-induced vibrations acting on the fuselage are diminished and the passenger flight comfort is significantly improved.

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