The invention provides a helicopter load suspended beam bracket. The helicopter load suspended beam bracket comprises a fixed lifting assembly; the adjusting control assembly is connected with the fixed lifting assembly; the shape maintaining supporting assembly is connected with the adjusting control assembly; wherein the helicopter load suspended beam is mounted on the dimensional supporting assembly, and movement and rotation in the X direction, the Y direction and the Z direction are achieved through the fixed lifting assembly and the adjusting control assembly till the load suspended beam is jacked to a target position; according to the load suspended beam bracket with the shape capable of being finely adjusted, in the aspect of load suspended beam installation, six-degree-of-freedom precise fine adjustment and jacking installation of the load suspended beam are achieved, the bracket is convenient to operate, short in adjustment time and high in adaptability, and the load suspended beam installation and positioning time can be greatly shortened.

    本申请提供的一种直升机负载挂梁托架,包括:固定提升组件;调节控制组件,与所述固定提升组件连接;维形支撑组件,与所述调节控制组件连接;其中,直升机负载挂梁安装在维形支撑组件,通过所述固定提升组件和调节控制组件实现X方向、Y方向和Z方向的移动和旋转,直至所述负载挂梁被顶装至目标位置;本申请维形可微调的负载挂梁托架,在负载挂梁安装方面,实现了负载挂梁的6自由度精密微调、顶起安装,该托架操作方便,调整时间短、适应性强,可以大幅减少负载挂梁安装及定位时间。


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    Titel :

    Helicopter load suspended beam bracket


    Weitere Titelangaben:

    一种直升机负载挂梁托架


    Beteiligte:
    CHEN ZHIYOU (Autor:in) / CAO YUANBAO (Autor:in) / ZHU CHENGHUI (Autor:in) / YANG FENG (Autor:in) / XIONG ZHE (Autor:in)

    Erscheinungsdatum :

    08.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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