The invention discloses a composite aircraft composed of fixed wings and deformable electric multi-rotary wings. The composite aircraft comprises a machine head, a machine body, a tail wing and wings. Pushing propellers are arranged in the front of the machine head. Rotary wing rods are connected with the wings through rotation devices with drive devices. The upper end faces of the rotary wing rods are ridge-shaped streamline hook surfaces with the two sides arching towards the middle, and the rotary wing rods are of a telescopic rod structure. The composite aircraft has the beneficial effect that vertical taking-off and landing of a rotary-wing helicopter are not limited by a taking-off and landing field and also has the flying speed and durable cruising capability of a fixed-wing airplane. The rotary wing rods can be bent, overturned and rotated through cooperation of bending devices, rotating devices and roller devices, and therefore the propellers can be controlled by a master controller to change the direction and angle at will, and flying is more flexible and convenient. The invention further discloses a control method of the composite aircraft composed of the fixed wings and the deformable electric multi-rotary wings


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    Titel :

    Composite aircraft composed of fixed wings and multi-rotary wings and control method of composite aircraft


    Beteiligte:
    LIU XIANWEI (Autor:in) / CAI YE (Autor:in)

    Erscheinungsdatum :

    02.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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