The present application relates essentially to a fixed-wing aircraft made up of a fuselage (02) in the shape of an aerofoil with four wings (10) having the same aerofoil shape with aerodynamic wing behaviour contributing to the lift and minimizing the drag of the aircraft, allowing it to have a larger payload and longer flight range.


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    Title :

    Vertical-take-off aerial vehicle with aerofoil-shaped integrated fuselage and wings



    Publication date :

    2023-07-19


    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




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