The invention relates to the field of target drone recovery, in particular to a target drone parachute opening mechanism which comprises a shell, a parachute opening mechanism and a parachute opening mechanism. The parachute opening assembly is arranged in the shell, the parachute opening assembly comprises a rotatable parachute cover hook, a pin shaft arranged in the parachute cover hook in a penetrating mode and a return spring arranged on the pin shaft in a penetrating mode, one end of the return spring is fixed to the shell, and the other end of the return spring is fixed to the parachute cover hook; the driving assembly is arranged in the shell and abuts against the canopy hook; the canopy ring abuts against the canopy hook in a non-unlocking state; when the canopy hook rotates, the canopy ring is pushed to open the parachute. The structure can be simpler and more convenient, so that the process of recovering and opening the umbrella is more convenient.

    本申请涉及靶机回收的领域,尤其是涉及一种靶机开伞机构,其包括:外壳,内部有供装置安装的空间;开伞组件,设置在所述外壳的内部,所述开伞组件包括能够转动的伞盖钩、穿设在所述伞盖钩内部的销轴以及穿设在所述销轴上的回位弹簧,所述回位弹簧的一端与外壳相固定,另一端与所述伞盖钩相固定;驱动组件,设置在所述外壳内部,与所述伞盖钩相抵接;伞盖环,在非开锁状态下,与所述伞盖钩相抵接;当所述伞盖钩转动时,推动所述伞盖环将降落伞打开。本申请能够使结构更加简便,从而使得回收开伞的过程更加便利。


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    Titel :

    Target drone parachute opening mechanism


    Weitere Titelangaben:

    一种靶机开伞机构


    Beteiligte:
    WANG LEI (Autor:in) / CHEN TINGFEI (Autor:in) / ZHAO JIANQING (Autor:in) / XING CHENGBO (Autor:in)

    Erscheinungsdatum :

    15.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / F41J TARGETS , Ziele



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