An aircraft (100) includes a gas turbine engine (108), an electric motor (110), and a propulsion device (112). The gas turbine engine (108) and the electric motor (110) are configured to provide a target cumulative output to the propulsion device (112). An electronic control unit (106) is configured to set the gas turbine engine (108) to a first engine mode to provide a first engine output to the propulsion device (112), set the electric motor (110) to a first motor mode to provide a first motor output to the propulsion device (112), a sum of the first engine output and the first motor output being within a predetermined range of the target cumulative output, and in response to a speed of the aircraft (100) reaching a target speed and the first engine output increasing to a second engine output, set the electric motor (110) to a second motor mode.


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    Title :

    AIRCRAFTS, SYSTEMS, AND METHODS FOR PROVIDING CONSTANT TORQUE ON TAKEOFF


    Additional title:

    FLUGZEUGE, SYSTEME UND VERFAHREN ZUR BEREITSTELLUNG EINES KONSTANTEN DREHMOMENTS BEIM START
    AÉRONEFS, SYSTÈMES ET PROCÉDÉS POUR FOURNIR UN COUPLE CONSTANT AU DÉCOLLAGE


    Contributors:
    KUMAR VINOD (author)

    Publication date :

    2024-02-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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