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US 4,477,044 AGranted
Elevator feel actuator
AssigneeThe Boeing Company
InventorsKevin A. Darcy, Terence F. H. Faithfull
Life of this patent
Estimating the term…
Abstract
A constant force mechanical spring and a varying force hydraulic actuator combine to provide feel to a pilot of his movement of an airplane's elevators. A constant force bias spring works against the hydraulic actuator to reduce the actuators effectiveness to nearly zero at minimum feel force conditions.
Claims2
An airplane elevator movement feel mechanism comprising:
- a hydraulic feel unit responsive to elevator control movement, means for varying the reaction of the hydraulic feel unit to reflect varying aircraft operating conditions, a bias spring located to directly work against the hydraulic feel unit for partially counteracting the hydraulic feel unit to all but cancel out the hydraulic feel unit at the lowest hydraulic feel unit setting, and a spring means for supplementing the hydraulic feel units for providing the feel means in case of an emergency in the hydraulic feel units.
An airplane elevator movement feel mechanism comprising:
- a pair of pivotally mounted spaced apart arms, linkages to extend between and to pivotally join one end of the arms, means connected to airplane elevator controls for imparting movement to the linkages to move that end of the arms inward, a variable pressure hydraulic actuator to extend between and to pivotally join the opposite end of the arms to resist arm movement created by the linkages, a bias spring to extend between the arms and located to work against the hydraulic actuator and sized to nearly cancel the hydraulic actuator at the lowest pressure setting, and a spring located to be actuated in response to elevator control movement.
Dependencies are inferred from the claim text.