An aeronautical vehicle (1) performs horizontal flight and/or vertical flight, and has a fuselage (2), a wing assembly (3) having a first wing part (3a) and a second wing part (3b) rigidly coupled to one another, a rotor assembly (4), a horizontal thruster (7), and an attitude control system. The wing assembly is arranged rotatably with respect to the fuselage to rotate about a vertical pivot axis between a stow position and an active position. The rotor assembly comprises two vertical thrust rotors arranged on a rotor support rotatably with respect to the fuselage to rotate the rotor assembly between a stow position and an active position. In a horizontal flight mode the wing assembly is in the active position and the rotor assembly is in the stow position, and in a vertical flight mode the wing assembly is in the stow position and the rotor assembly is in the active position.


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    Title :

    AERONAUTICAL VEHICLE AND METHOD OF TRANSITIONING BETWEEN FLIGHT MODES FOR AN AERONAUTICAL VEHICLE


    Additional title:

    LUFTFAHRZEUG UND VERFAHREN ZUM ÜBERGANG ZWISCHEN FLUGMODI FÜR EIN LUFTFAHRZEUG
    VÉHICULE AÉRONAUTIQUE ET PROCÉDÉ DE TRANSITION ENTRE DES MODES DE VOL POUR UN VÉHICULE AÉRONAUTIQUE


    Contributors:

    Publication date :

    2025-03-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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