Servo Drive Vernier Control
    1.
    发明公开

    公开(公告)号:US20230227148A1

    公开(公告)日:2023-07-20

    申请号:US18155036

    申请日:2023-01-16

    CPC classification number: B64C13/50

    Abstract: 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.

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