The invention provides a method and device for stopping an external suspension of a helicopter. The device comprises a shell, a central tilting assembly, a swing triggering assembly, a high-pressure gas cylinder and a rotation control assembly. Wherein the shell is composed of a barrel body, a central tilting assembly fixing ring, a swing-stopping gas spraying pipe, an annular gas cavity, a gas inlet one-way valve, a high-pressure gas cylinder cavity, a rotation-stopping shifting fork rotating table, a rotation-stopping shifting fork rotating cavity, a gas conveying one-way valve, a swing-stopping gas spraying opening and an external connecting table; the central tilting assembly is composed of a top column, an upper spherical cavity, an upper spherical cone, a flange ring, a lower spherical cavity, a lower spherical cone, a collision ring and a balance weight cake. The swing triggering assembly is composed of a swing stopping hanging ring, a swing stopping hinge, a swing stopping shifting fork hanging column, a swing stopping shifting fork air inlet hose, a swing stopping shifting fork air injection hose, a swing stopping shifting fork and a swing stopping switch assembly. The rotation control assembly is composed of a rotation stopping shifting fork, a rotation stopping collision table, a spring, a rotation stopping air inlet pipe, a rotation stopping switch assembly, a rotation stopping air spraying pipe, a rotation stopping air spraying channel and a rotation stopping air spraying opening.

    本申请提供了一种直升机外吊挂止动的方法和装置,所述装置包括壳体、中央倾转组件、摆动触发组件、高压气瓶、旋转控制组件;其中,壳体由筒体、中央倾转组件固定环、止摆喷气管、环形气腔、进气单向阀、高压气瓶腔、止转拨叉旋转台、止转拨叉旋转腔、输气单向阀、止摆喷气口、外部连接台组成;中央倾转组件由顶柱、上部球形腔、上部球形椎、法兰环、下部球形腔、下部球形椎、碰撞环、配重饼组成;摆动触发组件由止摆挂环、止摆铰链、止摆拨叉吊柱、止摆拨叉进气软管、止摆拨叉喷气软管、止摆拨叉、止摆开关组件组成;旋转控制组件由止转拨叉、止转碰撞台、弹簧、止转进气管、止转开关组件、止转喷气管、止转喷气道、止转喷气口组成。


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    Titel :

    Method and device for stopping external suspension of helicopter


    Weitere Titelangaben:

    一种直升机外吊挂止动的方法与装置


    Beteiligte:
    LI JINSHENG (Autor:in) / WU GENCAI (Autor:in) / YANG WEIYU (Autor:in) / CAO ZIJING (Autor:in) / LI YUXIANG (Autor:in)

    Erscheinungsdatum :

    24.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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