The invention belongs to the technical field of unmanned aerial vehicles, and discloses a telescopic rack structure for an aerial survey unmanned aerial vehicle. The telescopic rack structure for the aerial survey unmanned aerial vehicle comprises an upper machine shell, a lower machine shell and a control box, the upper machine shell and the lower machine shell are installed on the upper side and the lower side of the control box respectively, two symmetrical undercarriages are arranged on the lower side of the lower machine shell, and two fixed machine arms are installed on one side of the control box. According to the telescopic rack structure for the aerial survey unmanned aerial vehicle, by means of cooperation of the wing extension mechanism and the angle regulation and control mechanism, the flight mode can be adjusted according to requirements when the unmanned aerial vehicle flies, and for different tasks, for example, the unmanned aerial vehicle is converted into a fixed wing flight mode during aerial survey, the higher speed can be achieved; according to the unmanned aerial vehicle, the requirement for line precision is high, a multi-rotor flight mode can be used when a route needs to be customized, the unmanned aerial vehicle flies more flexibly, compared with a traditional unmanned aerial vehicle, the unmanned aerial vehicle has the advantages of a fixed-wing unmanned aerial vehicle and a multi-rotor unmanned aerial vehicle, the use mode is more flexible, and the equipment cost input is greatly saved.

    本发明属于无人机技术领域,公开了一种航测无人机用伸缩式机架结构。该航测无人机用伸缩式机架结构,包括上机壳、下机壳和控制盒,所述上机壳和下机壳分别安装在控制盒的上下侧,所述下机壳的下侧设置有两个对称的起落架,所述控制盒的一侧安装有两个固定机臂。该航测无人机用伸缩式机架结构,利用机翼扩展机构和角度调控机构配合,在无人机飞行时能够根据需求实现飞行模式的调节,针对不同的任务,如航测时转换为固定翼飞行模式能够具备更高的速度,对线路精度要求高、需要自定义路线时可使用多旋翼飞行模式,无人机飞行的更加灵活,相比于传统的无人机兼备了固定翼和多旋翼无人机的优点,使用方式更加灵活,大大的节省了设备成本投入。


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    Titel :

    Telescopic rack structure for aerial survey unmanned aerial vehicle


    Weitere Titelangaben:

    一种航测无人机用伸缩式机架结构


    Beteiligte:
    WANG JINNA (Autor:in) / YANG YING (Autor:in) / RUAN YUFENG (Autor:in)

    Erscheinungsdatum :

    2023-05-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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