A multirotor aircraft (100) that comprises a chassis (200), three or more engines (300) and one or more free wings (400). Each free wing (400) is attached to said chassis by an axial connection (18) in such a way that enables to change the attack angle of the free wing relative to said chassis according to the direction of the flow of air over the free wing. The aircraft may be equipped with control surfaces or movement-limiting devices.


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    Title :

    Tilt Winged Multi Rotor


    Contributors:
    REGEV AMIT (author)

    Publication date :

    2018-03-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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