The invention belongs to the technical field of ornithopter manufacturing, and particularly relates to an ornithopter flight device. According to the main structure, the ornithopter flight device comprises a power machine, a first connecting rod, a second connecting rod, a third connecting rod, a mandrel, a connecting shaft, a first support, a second support, a third support, a main skeleton, ribs, films, a left wing, a right wing, an airframe, a head, a fuselage and a tail. The first connecting rod, the second connecting rod, the third connecting rod and the mandrel form a four-connecting-rod structure to provide power for the left wing and the right wing. A high rotating speed is reduced to a speed needed by action of the four-connecting-rod structure through the deceleration type power machine, and then the left wing and the right wing are driven to swing; based on the principle that power generated in left-and-right swinging of fish tails in moving is used for providing climbing power and advancing power for flight, the effect of flight regulation and control is achieved. The ornithopter flight device is simple in structure, scientific in principle, low in manufacturing cost, easy to regulate and control and good in flight effect and has broad application prospects.


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    Titel :

    Ornithopter flight device


    Beteiligte:
    WU YI (Autor:in) / WU KAIZHEN (Autor:in) / WU RUOGU (Autor:in) / WU RUODING (Autor:in) / WU RUOYAO (Autor:in)

    Erscheinungsdatum :

    2015-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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