The invention provides a vertical constant tension suspension device which comprises a tension mechanism, a magnetic mechanism and a control mechanism, and the control mechanism is used for controlling the distance between a top plate and a bottom plate; the tension mechanism is located between the top plate and the bottom plate and generates tension between the top plate and the bottom plate; and the magnetic mechanism is located between the top plate and the bottom plate and generates magnetic force to the two sides of the top plate and the bottom plate, the tension and the magnetic force interact, and constant force output within a set range is achieved. According to the vertical constant-tension suspension device, the technical blank of a domestic high-precision vertical constant-tension suspension device is filled up, ground simulation equipment technical support is provided for research personnel to research the operation reliability of a spacecraft in a space environment, and a high-precision microgravity simulation test can be directly carried out on the ground.

    本发明提供了一种竖直向恒拉力悬吊装置,包括拉力机构、磁力机构和控制机构,控制机构,用于控制顶板和底板之间的距离;拉力机构,位于顶板和底板之间,向顶板和底板的中间产生拉力;磁力机构,位于顶板和底板之间,向顶板和底板的两侧产生磁力,拉力和磁力互相作用,实现设定范围内的恒力输出。本发明所述的竖直向恒拉力悬吊装置,填补了国内高精度竖直向恒拉力悬吊装置的技术空白,为研究人员研究太空环境下航天器运行可靠性提供了地面模拟装备技术支撑,能直接在地面进行高精度的微重力模拟试验。


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    Titel :

    Vertical constant-tension suspension device


    Weitere Titelangaben:

    一种竖直向恒拉力悬吊装置


    Beteiligte:
    LI GUANGPING (Autor:in) / HOU WEIJIE (Autor:in) / SONG CHENG (Autor:in) / HOU YUETING (Autor:in) / HAN QIANG (Autor:in) / ZANG LIBIN (Autor:in)

    Erscheinungsdatum :

    2024-01-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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