The invention discloses a built-in ejection rotating cartridge case structure for an unmanned aerial vehicle catching net launcher, which comprises a first cartridge case and a second cartridge case, a cylinder is fixed at one end of the first cartridge case, a rotating device is arranged on the cylinder, the fixed end of the rotating device is fixedly connected with the cylinder, a buckle device is fixed at one end in the second cartridge case, and a locking device is fixed at the other end in the second cartridge case. The rotating device is located in the second cartridge case, the free end of the rotating device is connected with the buckling device, and at least three sets of elastic pieces are connected to the periphery of the first cartridge case. Compared with the prior art, the rotating device can enable the first cartridge case to rotate to a certain degree, the elastic piece is erected relative to the first cartridge case, ejection force can be applied to the balancing weight on the catching net in the erecting process, and the first cartridge case can drive the elastic piece to rotate, so that the structure can drive the balancing weight on the catching net to rotate after being ejected, and therefore the catching net is more attractive in appearance. And therefore, the capturing net can fly faster, the range is farther, and the capturing efficiency of the capturing net on the target unmanned aerial vehicle is improved.

    本发明公开了一种用于无人机捕捉网发射器内置弹射旋转弹壳结构,包括第一弹壳和第二弹壳,所述第一弹壳一端固定有柱体,所述柱体上设置有旋转装置且旋转装置的固定端与柱体固定连接,所述第二弹壳内一端固定于有卡扣装置,所述旋转装置位于第二弹壳内且旋转装置的自由端与卡扣装置连接,所述第一弹壳外围连接有至少三组弹片。相比现有技术,本发明的旋转装置能够第一弹壳产生一定的转动,并且弹片相对于第一弹壳竖起,在竖起的过程中,会对捕捉网上配重块施加弹射力,而又由于第一弹壳会带动弹片旋转,因此,本结构能够带动捕捉网上配重块抛射出后旋转,进而使得捕捉网能够飞得更快,射程更远,提高了捕捉网对目标无人机的捕捉效率。


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    Title :

    Built-in ejection rotary cartridge case structure for unmanned aerial vehicle catching net launcher


    Additional title:

    一种用于无人机捕捉网发射器内置弹射旋转弹壳结构


    Contributors:
    XIAO JUNBO (author) / XU QING (author) / WANG SHENG (author) / HAN YUSHAN (author) / XIANG MENGYUAN (author) / LIU SHENGTAO (author) / MA YUPENG (author)

    Publication date :

    2024-08-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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