Disclosed is a vertical take-off and landing aerodyne, including a fuselage, two wings, horizontal flight propulsion unit and at least one pair of rotors intended to provide propulsion and lift in the take-off and landing phases. The rotors are retractable and the horizontal flight propulsion unit includes a counter-rotating propeller, situated at the tail of the aerodyne, and a drive unit for rotating the counter-rotating propeller, the counter-rotating propeller being capable of being oriented by a control unit about two axes, one parallel to the yaw axis and the other parallel to the pitch axis of the aerodyne, such that the counter-rotating propeller is used for controlling the attitude of the aerodyne, the latter therefore not having a tail unit.


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    Titel :

    VERTICAL TAKE-OFF AND LANDING AERODYNE OPTIMISED FOR HORIZONTAL FLIGHT


    Beteiligte:
    TAVIN GÉRARD (Autor:in)

    Erscheinungsdatum :

    25.01.2024


    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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