The present application discloses an aircraft. The aircraft comprises a first wing and a second wing, a fuselage to which the first wing and the second wing are mounted, a first engine operatively mounted to the first wing, and a second engine operatively mounted to the second wing. The aircraft is configured to vertically take-off and land. The first engine and the second engine are used for both (i) vertical take-off and landing, and (ii) horizontal flight.

    La présente demande divulgue un aéronef. L'aéronef comprend une première aile et une seconde aile, un fuselage sur lequel sont montées la première aile et la seconde aile, un premier moteur monté de manière fonctionnelle sur la première aile, et un second moteur monté de manière fonctionnelle sur la seconde aile. L'aéronef est conçu pour décoller et atterrir verticalement. Le premier moteur et le second moteur sont utilisés à la fois pour (i) le décollage et l'atterrissage verticaux, et (ii) le vol horizontal.


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    Title :

    DUAL ENGINE VERTICAL TAKE OFF AND LANDING COLLAPSIBLE FIXED WING AIRCRAFT


    Additional title:

    AÉRONEF À VOILURE FIXE PLIABLE À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX À DOUBLE MOTEUR


    Contributors:

    Publication date :

    2024-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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