An aircraft control system includes: a motor with a rotating shaft; a pilot control input; a linear actuator connecting the pilot control input to the rotating shaft; a sensor identifying a position of the pilot control input; and a transmitter transmitting the pilot control input position to a controller, the controller adjusting an aircraft performance device based on the received pilot control input position.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT TORQUE CONTROL DEVICE


    Contributors:

    Publication date :

    2021-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT TORQUE CONTROL DEVICE

    LAMBTON MICHAEL / SIMONS LOUIS / GREENE RANDALL A | European Patent Office | 2020

    Free access

    AIRCRAFT TORQUE CONTROL DEVICE

    LAMBTON MICHAEL J / SIMONS LOUIS C / GREENE RANDALL A | European Patent Office | 2019

    Free access

    Aircraft torque control device

    LAMBTON MICHAEL J / SIMONS LOUIS C / GREENE RANDALL A | European Patent Office | 2022

    Free access