The invention discloses a bionic swing wing aircraft, and belongs to the technical field of bionic aircrafts. The aircraft comprises a body, a left swing wing driving unit, a right swing wing driving unit, a left swing wing device, a right swing wing device, a left auxiliary wing device, a right auxiliary wing device and an undercarriage. The left swing wing driving unit and the right swing wing driving unit are respectively symmetrically arranged at the left side and the right side of the body, and the left auxiliary wing device and the right auxiliary wing device are respectively symmetrically arranged at the left side and the right side of the body; and the left swing rods and the right swing rods of the output members of the left and right swing wing driving devices swing up and down around one point in the movement process, and lower swing portions are always greater than upper swing portions, so the lower swooping portions of left and right swing wings fixedly connected with the lower swing portions are always greater than top swing portions, thereby the bionic swing wing aircraft generates positive lift force in the whole flapping swing movement process. The aircraft has the advantages of simple driving mechanism, easy realization and high flapping swing pneumatic efficiency.


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    Titel :

    Bionic swing wing aircraft


    Beteiligte:
    QIU HAN (Autor:in) / WANG HUIXING (Autor:in)

    Erscheinungsdatum :

    2016-01-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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