A servo drive vernier control for aircraft having a push-pull mechanism configured for manual actuation by a user includes a push rod mechanically coupled with an input knob. The push rod is configured for manual actuation via the input knob. An electromechanical control system is operatively coupled with the push rod for providing automated operation of the push rod. The electromechanical system includes a motor operatively coupled to the push rod. The motor is configured to rotate the push rod for actuating the push-pull mechanism. A controller is communicatively coupled to the motor for enabling electronic control of the push-pull mechanism.
Servo Drive Vernier Control
2023-07-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
IEEE | 2023
|British Library Online Contents | 2010
|Modulating Vernier Flap Control System
NTIS | 1977
|Modulating Vernier Flap Control System
NTIS | 1977
|