The invention provides a gravity compensation device for a step-by-step expansion type solar wing ground test. The device comprises trusses, two sets of transverse guide rails, a plurality of sets ofsliding mechanisms and a swing mechanism. The two sets of transverse guide rails are installed on the upper portions of the trusses through a plurality of truss installation supports, the swing mechanisms are installed on the trusses, the multiple sets of sliding mechanisms cooperate with the two sets of transverse guide rails, and the section of each transverse guide rail is rectangular; each setof sliding mechanism comprises two transverse sliding frames, a longitudinal shaft support and a longitudinal shaft, the upper portions of the transverse sliding frames are erected on the transverseguide rails on the corresponding sides respectively and slide along the transverse guide rails of the transverse sliding frames, the swing mechanism and each longitudinal shaft are provided with a suspension assembly respectively, and the suspension assemblies slide along the longitudinal shafts and the swing mechanism. Therefore, problems that a long guide rail in a traditional large-range two-dimensional unfolding mechanism is difficult to machine, the guide rail machining and adjusting precision requirements are high, and the unfolding process is prone to being jammed are effectively solved, and the device is convenient to carry and has good economical efficiency and applicability.

    本发明提供了一种用于分步展开式太阳翼地面试验的重力补偿装置,包括桁架、横向导轨、滑动机构和摆动机构,横向导轨设置两组,且通过若干桁架安装支架安装在桁架的上部,摆动机构安装在桁架上,滑动机构设置若干组,且均与两组横向导轨配合,横向导轨的截面为矩形;每组滑动机构均包括横向滑架、纵向轴支架和纵向轴,横向滑架设置两个,横向滑架的上部分别搭设在相应侧的横向导轨上,且沿各自的横向导轨滑动,在摆动机构上及每个纵向轴上均设有一悬吊组件,悬吊组件沿纵向轴及摆动机构滑动。本发明有效解决传统大范围二维展开机构中的长导轨加工困难、导轨加工及装调精度要求高及展开过程易卡死问题,本发明便于搬运,具有良好的经济型和适用性。


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    Titel :

    Gravity compensation device for step-by-step expansion type solar wing ground test


    Weitere Titelangaben:

    一种用于分步展开式太阳翼地面试验的重力补偿装置


    Beteiligte:
    ZHAO CHUNJUAN (Autor:in) / GU SONG (Autor:in) / ZHANG DAOWEI (Autor:in) / SUN HONGYU (Autor:in) / ZHANG LEI (Autor:in) / ZHAO XIANGYU (Autor:in)

    Erscheinungsdatum :

    18.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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