The purpose of the present invention is to provide a flight control mechanism for controlling flight of an unmanned aerial vehicle by controlling collision between the vehicle and a boundary surface,an unmanned aerial vehicle equipped with the mechanism, and a method for using the mechanism and the vehicle. Provided is the flight control mechanism for the unmanned aerial vehicle including: a first initial collision member; a second initial collision member; and a holding member that holds the first and second initial collision members with a space therebetween above the body of the unmanned aerial vehicle, is tiltable with respect to the vehicle body by rotating about a predetermined position inside or above the vehicle body toward the side of the vehicle body, and rotates in response tocollision between the first or second initial collision member and a boundary surface.

    本发明提供一种用于通过控制与边界面的碰撞来控制无人航空器的飞行的飞行控制机构、具备该机构的无人航空器及使用它们的方法。本发明提供一种无人航空器的飞行控制机构,其具备:第一先行碰撞部件;第二先行碰撞部件;保持部件,其将第一及第二先行碰撞部件分开地保持在无人航空器的机身上方,通过以机身内或机身上的规定位置为中心向机身的侧方侧旋转而相对于机身可倾斜,并且根据第一及第二先行碰撞部件中一方与边界面碰撞而旋转。


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    Titel :

    UNMANNED AERIAL VEHICLE, FLIGHT CONTROL MECHANISM FOR UNMANNED AERIAL VEHICLE, AND METHOD FOR USING UNMANNED AERIAL VEHICLE AND MECHANISM FOR UNMANNED AERIAL VEHICLE


    Weitere Titelangaben:

    无人航空器、无人航空器的飞行控制机构及使用它们的方法


    Beteiligte:
    KUROIWA KENJI (Autor:in) / INOUE SHOSUKE (Autor:in) / INAGAKI YUSUKE (Autor:in)

    Erscheinungsdatum :

    2021-01-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT






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