The invention discloses a missile and unmanned aerial vehicle body separation device and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles and missiles, the missile and unmanned aerial vehicle body separation device comprises a missile body flange, and one side of the missile body flange is used for being connected with the tail of a missile; one side of the airframe flange is used for being connected with the end part of an unmanned aerial vehicle airframe; the bag belt assembly comprises a bag belt and a plurality of clamping blocks, the bag belt is connected through a cut-off structure to form an annular structure, when the bag belt forms the annular structure, the clamping blocks are distributed on the inner side of the annular structure in the circumferential direction, and clamping grooves are formed in the inner peripheries of the clamping blocks; the separation spring is arranged between the projectile body flange and the machine body flange, and after the separation spring is compressed, the projectile body flange and the machine body flange can be contained in the clamping groove; the pulling spring is arranged between the wrapping tape assembly and the end part of the unmanned aerial vehicle body; according to the separation device, the missile and the unmanned aerial vehicle body can be rapidly separated through the cut-off structure, and the rapid strike function of the missile and unmanned aerial vehicle integrated aircraft is achieved.

    本发明公开了一种导弹与无人机机体分离装置及无人机,涉及无人机及导弹技术领域,包括:弹体法兰,弹体法兰的一侧用于与导弹的尾部连接;机体法兰,机体法兰的一侧用于与无人机机体的端部连接;包带组合体,包带组合体包括包带和多个卡块,包带通过可切断结构连接形成环形结构,当包带形成环形结构时多个卡块在环形结构的内侧沿周向分布,卡块的内周上设置有卡槽;分离弹簧,分离弹簧设置在弹体法兰与机体法兰之间,分离弹簧压缩后,卡槽内能够容纳弹体法兰和机体法兰;拉拽弹簧,拉拽弹簧设置在包带组合体与无人机机体的端部之间;该分离装置通过可切断结构实现导弹与无人机机体快速分离,实现导弹与无人机一体化飞行器的快速打击功能。


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    Title :

    Missile and unmanned aerial vehicle body separation device and unmanned aerial vehicle


    Additional title:

    一种导弹与无人机机体分离装置及无人机


    Contributors:
    WANG YANWEI (author) / WANG ZONGHUI (author) / SHI XUDONG (author) / MA CUNWANG (author)

    Publication date :

    2022-07-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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