Flight compensator control system for aircraft with haptic feedback
AssigneeSafran Electronics & Defense
InventorsRemi-Louis Lawniczak, Christophe Bastide
Life of this patent
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Abstract
This aircraft flight compensator control system includes a motor and a variable-friction actuator coupled with the motor and with an output shaft. The variable-friction actuator includes a variable-friction-torque magnetic clutch connected to the output shaft.
Claims8
An aircraft flight compensator control system comprising a motor, and a variable-friction actuator coupled with the motor and with an output shaft, wherein the variable-friction actuator comprises a variable-friction-torque magnetic clutch connected to the output shaft, the aircraft flight compensator control system comprising means for detecting a sense of force applied to the output shaft, wherein the aircraft flight compensator control system comprises a reduction gear placed between the motor and the actuator, wherein the aircraft flight compensator control system further comprises a magnetorheological brake inserted between the magnetic clutch and the motor.
Dependencies are inferred from the claim text.