Vibration control assembly for an aircraft and method of controlling aircraft vibration
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United States of America Patent
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Feb 2, 2021
Grant Date -
Nov 23, 2017
app pub date -
Oct 21, 2015
filing date -
Oct 21, 2014
priority date (Note) -
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Abstract
A vibration control assembly for an aircraft including a housing operatively coupled to the aircraft. Also included is a cage disposed within an interior region of the housing, the cage rotatable within the housing about a first axis. Further included is a gyroscope wheel disposed within the cage and rotatable about a second axis other than the first axis, wherein a controllable moment is imposed on the aircraft upon rotation of the gyroscope wheel to counter vibratory moments produced by the vehicle.
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