A lever control system integrates taxi operation using an electric motor in an aircraft with speed control of a jet engine in the same aircraft. The lever control system provides a smooth transition between the electric motor system used for aircraft taxi operation, and a jet engine system used to fly the aircraft. The lever control system may include a reverse lockout mechanism to prevent unintended reverse taxi movement of the aircraft.


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    Title :

    CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL


    Contributors:

    Publication date :

    2015-07-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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