The invention relates to a panel type flapping wing aircraft with a stepping motor, belonging to the technical field of aviation. The panel type flapping wing aircraft with the stepping motor is composed of a machine body, a tail rotor, a left flapping wing device, a right flapping wing device, a control system, a remote control device and an undercarriage, wherein the left flapping wing device and the right flapping wing device are same in structure, parameters and working principle and are symmetrically arranged at the left side and the right side of the machine body, the rotating plane of the tail rotor can incline towards the left or the right to achieve the pitching and yawed flight states of the aircraft; the right flapping wing device comprises an engine, a speed reducer, a main shaft, a rotating arm, a wing axis, a panel, a stepping motor, a central sprocket wheel, a chain and a wing sprocket wheel; the panel is a right panel and is rectangular; the transmission ratio of the central sprocket wheel to the wing sprocket wheel is 1 to 1; the panel is kept to be perpendicular to the corresponding rotating arm in an uptrend process, and the panel is kept to be in a horizontal state in a swooping process. The aircraft has simple structure and high efficiency, and is suitable for aerial photography, geographic survey, traffic duty, military reconnaissance and rescue and relief tasks.


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    Titel :

    Panel type flapping wing aircraft with stepping motor


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    08.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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