The invention discloses a typical microsatellite solar wing which is arranged on a satellite body and comprises a connecting mechanism and a substrate structure, the connecting mechanism is arranged on the satellite body, and the substrate structure is arranged on the connecting mechanism and used for providing an installation environment for a solar cell. The connecting mechanism comprises a hinge arranged on the star body and used for being connected with the base plate structure and a memory alloy type unlocking device arranged on the star body and used for locking the base plate structure, and the connecting mechanism is used for connecting the star body and the base plate structure. According to the typical microsatellite solar wing, the selected hinge and the unlocking device are goods shelf products, then the goods shelf products and the corresponding installation positions of the base plate are assembled through screws or pins, and the typical microsatellite solar wing has the advantages that the modular characteristic is achieved, operability is good, maintenance and replacement are easy, time and cost are saved, unlocking impact can be basically ignored, and microsatellite attitude keeping is facilitated.

    本发明公开了一种典型的微小卫星太阳翼,其设置于星体上,包括:连接机构和基板结构,连接机构设置于所述星体上,基板结构设置于所述连接结构上,用于为太阳电池提供安装环境,连接机构包括设置在所述星体上用于连接所述基板结构的合页铰链,和设置于所述星体上用于对所述基板结构锁定的记忆合金形式解锁器,连接机构用于将所述星体和所述基板结构进行连接。该典型的微小卫星太阳翼所选用铰链及解锁器均为货架产品,然后通过螺钉或销子与基板相应安装位置进行装配,具有模块化特征,可操作性好,易维修易更换,节约时间与成本,解锁冲击基本可忽略,有利于微小卫星姿态保持等优点。


    Access

    Download


    Export, share and cite



    Title :

    Typical microsatellite solar wing


    Additional title:

    一种典型的微小卫星太阳翼


    Contributors:
    FANG YUANBIN (author) / GU JUN (author) / LIU LEI (author) / HUANG HONGCHANG (author) / SHEN XUNAN (author) / LI HONGSHUAI (author) / JIA SHILEI (author) / LI ZONGHUA (author) / YANG LI (author) / CHU YUE (author)

    Publication date :

    2024-03-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Ground unfolding device for solar wing of microsatellite

    NI ZHIXUE / CHEN SHANBO / ZHANG DAOWEI | European Patent Office | 2023

    Free access

    High-rigidity unfolding mechanism for solar wing of microsatellite

    ZHANG DAOWEI / ZANG HONGDA / NI ZHIXUE et al. | European Patent Office | 2023

    Free access

    Solar wing fast mounting method suitable for flexible hinge connection of microsatellite and solar wing

    QI LIUJU / GAO YUAN / YANG JINXING et al. | European Patent Office | 2023

    Free access

    Flutter Characteristics of Typical Wing Sections of a Box Wing Aircraft Configuration

    Fazelzadeh, S. Ahmad / Scholz, Dieter / Mazidi, Abbas et al. | BASE | 2018

    Free access

    ASW concept of fixed-wing UAV and typical load

    SU Jintao | DOAJ | 2018

    Free access