The invention discloses a space solar cell array sail surface unfolding mechanism, which belongs to the technical field of space solar cell arrays, and is characterized by comprising a connecting support module for connecting a satellite; the rotary unfolding module is mounted on the connecting and supporting module; the pressing and releasing module is positioned on the upper surface of the rotary unfolding module; the avoiding unfolding modules are located on the periphery of the rotary unfolding module; the avoiding unfolding module comprises M avoiding unfolding assemblies; the outer side edge of the pressing and releasing module is connected with one end of the avoiding and unfolding assembly through a disconnectable assembly. A mounting interface connected with the rotary unfolding module and the avoiding unfolding assembly is arranged on the connecting and supporting module; the other end of the avoiding unfolding assembly is connected with the connecting supporting module through a coil spring. And a flexible solar cell array sail surface is mounted in the rotary unfolding module. A system integration design scheme is adopted, and on the premise that the large folding-unfolding ratio, the large power mass ratio and the large power volume ratio are achieved, the advantages of being large in rigidity of the transmitting section and the on-orbit section, high in fundamental frequency and the like are achieved.

    本发明公开了一种空间太阳电池阵帆面展开机构,属于空间太阳电池阵技术领域,其特征在于,包括:用于连接卫星的连接支撑模块;安装在所述连接支撑模块上的旋转展开模块;位于旋转展开模块上表面的压紧释放模块;位于旋转展开模块四周的避让展开模块;所述避让展开模块包括M个避让展开组件;压紧释放模块的外侧边与避让展开组件的一端通过可断开组件连接;连接支撑模块上设有与旋转展开模块、避让展开组件连接的安装接口;避让展开组件的另一端通过卷簧与连接支撑模块连接;旋转展开模块内安装有柔性太阳电池阵帆面。本发明采用系统集成化设计方案,在实现大折展比和功率质量比与功率体积比的前提下,具有发射段与在轨段刚度大、基频高等特点。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Space solar cell array sail surface unfolding mechanism


    Weitere Titelangaben:

    一种空间太阳电池阵帆面展开机构


    Beteiligte:
    ZHU JIALIN (Autor:in) / CUI XINYU (Autor:in) / YU HUI (Autor:in) / ZHANG WEI (Autor:in) / LIN JUNYI (Autor:in) / LAN ZHICHENG (Autor:in) / ZHANG QI (Autor:in) / WU ZHICHENG (Autor:in) / TANG YIDAN (Autor:in)

    Erscheinungsdatum :

    28.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Solar sail unfolding mechanism based on traction mode control

    ZHANG FUJIAN / WU CHENCHEN / ZHANG RUMING | Europäisches Patentamt | 2023

    Freier Zugriff

    Satellite solar cell array unfolding mechanism

    LIU FENG / SUN WENMING / GUO QING | Europäisches Patentamt | 2023

    Freier Zugriff

    Centralized driving type spacecraft solar sail multi-degree-of-freedom space folding and unfolding mechanism

    SHI HAOTIAN / ZHOU CHANGCONG / YUAN KANGBO et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Thermally-driven liquid crystal solar sail unfolding device

    XU FAN / LI XINQI / ZHANG XIAOLIANG | Europäisches Patentamt | 2024

    Freier Zugriff