The invention discloses a small unmanned aerial vehicle parachuting device. The device comprises a parachute, a shell and a fixing belt, a shell cover is arranged at the top end of the shell, the parachute and a spraying groove are formed in the shell, a fixing belt connecting clamping groove is formed in the side face of the shell, a USB charging port and a switch button are arranged on the backface of the shell, and a shell base is connected with a control circuit board and a battery; and a connecting clamping piece is arranged on the fixing belt. When an unmanned aerial vehicle breaks downand falls off, damage to the unmanned aerial vehicle can be effectively reduced. The device has the characteristics of small size, simple structure, portability, intelligent detection, high parachuteopening speed, long standby time, low cost and the like.

    本发明公开了一种小型无人机伞降装置,包括降落伞、外壳、固定带,其中外壳顶端有外壳盖,外壳内有降落伞和喷射槽,外壳侧面有固定带连接卡槽,外壳背面有USB充电口和开关按钮,外壳底座连接着控制电路板和电池;固定带上有连接卡件。其有益效果在于,当无人机发生故障跌落时,能有效的减小对无人机的损害。具有体积小、结构简单、轻便易携带、智能检测、开伞速度快、待机时间长、成本低等特点。


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    Titel :

    Small unmanned aerial vehicle parachuting device


    Weitere Titelangaben:

    一种小型无人机伞降装置


    Beteiligte:
    ZHOU LIANGYU (Autor:in) / WU YOU (Autor:in) / WANG ZHIHENG (Autor:in)

    Erscheinungsdatum :

    09.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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