A vertical take-off aircraft (1) has two wings arranged on an aircraft fuselage (2) of the aircraft (1). Along each wing (3), in each case at least one pivoting drive unit (5) is arranged pivotably on the wings. The at least one pivoting drive unit (5) can be brought into a vertical flying position and into a horizontal flying position. In the vertical flying position, the pivoting drive units (5) generate an uplift necessary for a vertical flying movement of the aircraft (1) and, in the horizontal flying position, a propulsion necessary for a horizontal flying movement of the aircraft (1). On each wing (3), at least one vertical drive unit (6) is arranged rigidly in a vertical flying position.


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    Title :

    VERTICAL TAKEOFF AIRCRAFT


    Contributors:

    Publication date :

    2024-07-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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