An aircraft includes a canard having a trailing edge, a forward swept and fixed wing having a horizontal plane and a trailing edge, and a plurality of tilt rotors. At least one of the plurality of tilt rotors is attached to the trailing edge of the canard and at least one of the plurality of tilt rotors is attached to the trailing edge of the forward swept and fixed wing. The aircraft also includes a T-tail having a horizontal plane, where the horizontal plane of the T-tail is at a height that is higher than the horizontal plane of the forward swept and fixed wing.

    La présente invention concerne un aéronef qui comprend un canard ayant un bord de fuite, une aile à flèche avant fixe ayant un plan horizontal et un bord de fuite, ainsi qu'une pluralité de rotors basculants. Au moins un rotor de la pluralité de rotors basculants est fixé au bord de fuite du canard et au moins un rotor de la pluralité de rotors basculants est fixé au bord de fuite de l'aile à flèche avant fixe. L'aéronef comprend également une queue en T ayant un plan horizontal, le plan horizontal de la queue en T étant à une hauteur qui est supérieure au plan horizontal de l'aile à flèche avant fixe.


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    Title :

    FIXED WING AIRCRAFT WITH TRAILING ROTORS AND T-TAIL


    Additional title:

    AÉRONEF À AILE FIXE AVEC ROTORS DE FUITE ET QUEUE EN T


    Contributors:

    Publication date :

    2021-02-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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