A manned aircraft having wing parts, an internal combustion engine which is connected via a shaft to a left thrust nacelle and to a right thrust nacelle, which are pivotable from a vertical position for a hovering flight phase into a horizontal position for the forward flight phase, and having a left thrust unit and a right thrust unit which are driven by electric motors, and having a control unit which carries out a moment-dynamic flight control and which controls the thrust units to generate thrust for the hovering flight phase and at least partially stops them for the forward flight phase.


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    Titel :

    VTOL AIRCRAFT WITH A BATTERY ELECTRIC DRIVE AND AN INTERNAL COMBUSTION ENGINE


    Beteiligte:
    HEEL PATRICK (Autor:in) / POHN THOMAS (Autor:in)

    Erscheinungsdatum :

    06.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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