The embodiment of the invention provides a rapid separation mechanism for an aircraft tail parachute and an aircraft. The tail parachute comprises a tail shell and a parachute arranged in the tail shell. The rapid separation mechanism comprises an installation base, at least one unlocking assembly, and at least one driving mechanism, wherein the unlocking assembly includes a plug connector and a bayonet socket, the bayonet socket is connected with the installation base, and the plug connector is movably inserted into the bayonet socket and the tail shell; and the at least one driving mechanismis in transmission connection with the corresponding plug connector so as to drive the plug connector to be inserted into or separated from the tail shell. According to the rapid separation mechanism, the driving mechanism is used for driving the plug connector to be inserted into or separated from the tail shell, a parachute release mechanism can be stably and rapidly opened in a flying process,the structure is simple, the cost is low, and stability is greatly improved.

    本发明的实施例提供一种用于飞行器尾部降落伞的快速分离机构和飞行器。所述尾部降落伞包括尾部壳体以及设置在所述尾部壳体内的降落伞,所述快速分离机构包括:安装座;至少一个解锁组件,所述解锁组件包括插接件和插接座,所述插接座与所述安装座相连,所述插接件可移动地插设在所述插接座和所述尾部壳体中;至少一个驱动机构,所述驱动机构与对应的所述插接件传动相连,以驱动所述插接件插入或脱离所述尾部壳体。本发明的快速分离机构,利用驱动机构驱动插接件插入或脱离尾部壳体,可以实现在飞行过程中可以稳定且快速的打通降落伞释放机构,结构简单,成本较低,稳定性大大提高。


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    Titel :

    Rapid separation mechanism for aircraft tail parachute and aircraft


    Weitere Titelangaben:

    一种用于飞行器尾部降落伞的快速分离机构和飞行器


    Beteiligte:
    WANG ZHIYONG (Autor:in) / LIU HANYANG (Autor:in) / ZHANG PENG (Autor:in) / LIU QIAN (Autor:in) / TANG ZHANWEN (Autor:in)

    Erscheinungsdatum :

    2020-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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