The invention discloses a downward throwing type attack detection unmanned aerial vehicle. The downward throwing type attack detection unmanned aerial vehicle comprises a separable housing; a first containing cavity and a second containing cavity are formed in the upper end and the lower end of the interior of the shell; a parachute pack is arranged in the first containing cavity; a brake parachute is arranged in the parachute pack; an unmanned aerial vehicle body is arranged in the second containing cavity; the unmanned aerial vehicle body comprises a vehicle body, a plurality of wings rotationally arranged on the upper portion of the vehicle body and a photoelectric pod rotationally arranged at the bottom end of the vehicle body; a connecting wire is arranged at the lower end of the brake parachute, penetrates into the second containing cavity and is connected with the top end of the vehicle body. According to the unmanned aerial vehicle, the unmanned aerial vehicle body is loaded inthe outer shell, the brake parachute is further arranged in the outer shell, the brake parachute can be used for decelerating during high-altitude throwing, the wings can be used for decelerating after the unmanned aerial vehicle body is thrown away from the shell and the connecting wire is disconnected, and power energy can be saved; the unmanned aerial vehicle is controlled by the wings to be stable in posture when approaching a target in complex terrains such as cities, a stable working environment can be provided for the photoelectric pod, a detection process is flexible, and the target is easy to discover and identify.

    本发明公开了一种下抛式探测攻击无人机,包括可分离式壳体,壳体内部的上下端设有第一容腔和第二容腔,第一容腔内设有伞包,伞包内设有减速伞,第二容腔内设有无人机本体,无人机本体包括机身、多个转动设于机身上部的机翼和转动设于机身底端的光电吊舱,减速伞的下端设有连接线,连接线穿入第二容腔内并与机身的顶端连接;本发明通过将无人机本体装载在一个外壳内,且外壳内还设有减速伞,在高空抛下的时候能够利用减速伞进行减速,在抛离壳体、断开连接线后可以利用机翼进行减速,能够节省动力能源;并且通过机翼控制无人机在城市等复杂地形中接近目标时姿态较为稳定,能够为光电吊舱提供平稳的工作环境,探测过程机动灵活,易于发现并识别目标。


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    Title :

    Downward throwing type detection attack unmanned aerial vehicle


    Additional title:

    一种下抛式探测攻击无人机


    Contributors:
    ZHANG BINGRONG (author) / XU XIAOWU (author) / YANG XIANFENG (author) / PAN QIFAN (author) / HUANG HONGYANG (author)

    Publication date :

    2020-09-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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