An exemplary electric distributed propulsion system (600) includes two or more rotors (612a-d) that are individually controlled by the rotational speed of associated motors (611a-d), an input control (626) connected to the associated motors to provide rotational speed control to the two or more rotors to produce a desired net thrust, and a logic (624) connected to the input control (626) and the associated motors (611a-d), the logic (624) for controlling speed and direction of the two or more rotors (612a-d) to achieve the desired net thrust and to avoid a motor speed condition.


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    Title :

    ELECTRIC DISTRIBUTED PROPULSION WITH DIFFERENT ROTOR ROTATIONAL SPEEDS


    Additional title:

    ELEKTRISCH VERTEILTER ANTRIEB MIT UNTERSCHIEDLICHEN DREHGESCHWINDIGKEITEN
    PROPULSION ÉLECTRIQUE DISTRIBUÉE AVEC DIFFÉRENTES VITESSES DE ROTATION DU ROTOR



    Publication date :

    2021-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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