The invention discloses a cover shooting and parachute guiding assembly and an unmanned aerial vehicle, and relates to the technical field of aircrafts, the cover shooting and parachute guiding assembly comprises a shell mechanism and a trigger mechanism, the shell mechanism comprises a shell and a cabin cover, the shell is provided with a parachute cabin, and the cabin cover covers the parachute cabin. The triggering mechanism comprises a rotating part, an elastic part and a control switch, the rotating part is rotationally connected with the machine shell through the elastic part, the rotating part is slidably connected with the hatch cover, and the control switch is arranged on the machine shell and detachably connected to the hatch cover. When the control switch is connected with the cabin cover, the cabin cover covers the parachute cabin, and the elastic piece accumulates elastic force. When the control switch is separated from the cabin cover, the elastic piece can release elastic force to drive the rotating piece to rotate, so that the cabin cover is separated from the rotating piece through inertia sliding and drives the guiding parachute to be separated from the parachute cabin. The cover shooting and parachute guiding assembly only comprises light-weight parts such as the cabin cover, the rotating piece, the elastic piece and the control switch, the weight proportion of the cover shooting and parachute guiding assembly to the whole unmanned aerial vehicle is small, and the mounting space of effective loads such as fuel equipment of the unmanned aerial vehicle cannot be excessively occupied.

    本发明公开了一种射盖引伞组件及无人机,涉及航空器技术领域,射盖引伞组件包括机壳机构和触发机构,机壳机构包括机壳与舱盖,机壳开设有伞舱,舱盖盖设于伞舱。触发机构包括转动件、弹性件和控制开关,转动件通过弹性件转动连接机壳,转动件滑动连接舱盖,控制开关设于机壳并可拆卸连接于舱盖。当控制开关连接舱盖时,舱盖盖住伞舱且弹性件积蓄弹性力;当控制开关脱离舱盖时,弹性件能够释放弹性力驱使转动件转动,以使舱盖通过惯性滑动脱离转动件并带动引导伞脱离伞舱。本发明的射盖引伞组件仅包括舱盖、转动件、弹性件和控制开关等重量很轻的零部件,占无人机整机的重量比例小,也不会过多挤占无人机的燃料装备等有效载荷的安装空间。


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    Title :

    Cover shooting and umbrella guiding assembly and unmanned aerial vehicle


    Additional title:

    射盖引伞组件及无人机


    Contributors:
    LI XINSHENG (author) / REN ZHITONG (author) / TAN XUETONG (author)

    Publication date :

    2024-12-10


    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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