Vertical take-off aircraft provided with canards (1) and primary wings (2), which primary wings (2) are provided with two or more primary thrusters (20). The primary wings (2) are rotatable alternately in a vertical configuration for vertical flight mode and in a horizontal configuration for horizontal flight mode. The canards (1) in said vertical flight mode are arranged substantially parallel to a plane perpendicular to the flight direction, each canard (1) being provided with a secondary thruster (10) oriented for vertical flight mode and at least partially comprised in the profile of the canard (1) itself.


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    Titel :

    VERTICAL TAKE-OFF AIRCRAFT WITH CANARDS AND PRIMARY WINGS


    Beteiligte:
    BECCHI PAOLO (Autor:in)

    Erscheinungsdatum :

    25.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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