The invention provides a solar wing fast-assembly method suitable for microsatellite flexible hinge connection and a solar wing, and the solar wing fast-assembly method comprises the following steps: step 1, a hinge is pre-formed into a required angle through a hinge forming tool, and a hinge positioning tool is mounted at a formed hinge interface through a fastener; 2, plate sleeves of the solar wing substrates are installed on the upper faces and the lower faces of the positions, where the locking devices are installed, of the inner solar wing substrate, the middle solar wing substrate and the outer solar wing substrate respectively, and force measurement is conducted on fasteners for locking the plate sleeves after positioning is conducted through pins; 3, the outer solar wing substrate and the middle solar wing substrate are installed above the solar wing simulation wall through positioning pins and limiting columns, and then the inner solar wing substrate where the SADA connecting frame is installed in advance is installed above the middle solar wing substrate through the positioning pins. The method has the beneficial effects that the precision of the hinge mounting position is ensured by adopting flexible hinge pre-forming, solar wing substrate mounting hinge embedded parts and scribed line positioning.

    本发明提供了一种适用于微小卫星柔性铰链连接的太阳翼快装方法和太阳翼,该太阳翼快装方法包括以下步骤:步骤1,将铰链通过铰链成形工装预先成形成所需要角度,并在成形的铰链接口用紧固件安装铰链定位工装;步骤2,在内太阳翼基板、中间太阳翼基板和外太阳翼基板安装锁紧装置的通孔处上下面分别安装太阳翼基板的板套,通过销钉定位后对锁紧板套的紧固件进行测力;步骤3,将外太阳翼基板和中间太阳翼基板通过定位销和限位柱安装在太阳翼模拟墙上方,然后通过定位销将提前安装SADA连接架的内太阳翼基板安装在中间太阳翼基板上方。本发明的有益效果是:本发明采用柔性铰链预成形,太阳翼基板安装铰链埋件加刻线定位保证铰链安装位置精度。


    Access

    Download


    Export, share and cite



    Title :

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


    Additional title:

    适用于微小卫星柔性铰链连接的太阳翼快装方法及太阳翼


    Contributors:
    QI LIUJU (author) / GAO YUAN (author) / YANG JINXING (author) / DAI JIANFENG (author) / YE ZHENGWEI (author) / YANG CHUNLONG (author) / WU SHICHEN (author) / LIN RU (author) / JIA YUANMEI (author)

    Publication date :

    2023-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Typical microsatellite solar wing

    FANG YUANBIN / GU JUN / LIU LEI et al. | European Patent Office | 2024

    Free access

    Solar wing unfolding hinge based on four-bar mechanism and solar wing

    LI TENG / ZHANG BOWEN / SUN ZHENGLU et al. | European Patent Office | 2024

    Free access

    Flexible solar wing

    LI ZHAO / HUANG JIA / GENG SHENGWEI et al. | European Patent Office | 2025

    Free access

    Connection assembly for wing, wing for aircraft and wing mounting method

    KREY DENNIS / HUBER ALEXANDER / SCHLIPF BERNHARD et al. | European Patent Office | 2021

    Free access

    Ground unfolding device for solar wing of microsatellite

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

    Free access