The invention relates to a small rescue unmanned aerial vehicle which comprises a control body, a plurality of rotor wings and indicating lamps arranged under the rotor wings, the lower end of the control body is connected with a resource storage box, and the rotor wings are connected with self-adaptive adjustment supporting mechanisms; a moving groove is formed in the resource storage box; a limiting groove is formed in the side wall of the moving groove, the storage box is arranged in the moving groove, a sealing door is connected with the storage box through a locking mechanism, a limitingblock is connected to the side wall of the storage box, an installation cavity and a storage battery are arranged over the moving groove, a first motor is arranged in the installation cavity, and a worm is connected to an output shaft of the first motor. According to the small rescue unmanned aerial vehicle, the supporting mechanism can be adjusted according to the actual landing environment in the rescue process, the small rescue unmanned aerial vehicle is suitable for different terrains, meanwhile, energy supplementing can be conducted during landing, rescue materials can be stored in the resource storage box, the rescue materials are prevented from being affected by the external environment, and the safety is high.

    本发明涉及一种小型救援无人机,包括控制主体、若干个旋翼以及设于旋翼下方的指示灯,所述控制主体的下端连接有资源存储箱,所述旋翼上连接有自适应调节支撑机构;所述资源存储箱内设有移动槽、设于移动槽侧壁上的限位槽、设于移动槽内的储物盒、通过锁定机构和储物盒连接的封闭门、连接在储物盒侧壁上的限位块、设于移动槽上方的安装腔室和蓄电池、设于安装腔室内的第一电机、连接在第一电机输出轴上的蜗杆。该小型救援无人机,在救援过程中可以根据实际落地环境进行调节支撑机构,适用于不同的地形,同时可以在落地期间进行能源补充,且救援物资可以收纳在资源存储箱中,防止救援物资受到外界环境的影响,安全性较高。


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    Title :

    Small rescue unmanned aerial vehicle


    Additional title:

    一种小型救援无人机


    Contributors:
    MA LU (author) / HU FANGJIANG (author)

    Publication date :

    2020-10-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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