The invention discloses a high-rigidity and high-damping satellite platform configuration, which belongs to the field of overall design of spacecrafts and comprises a satellite-rocket butt joint ring used for being in butt joint with a rocket adapter; a mounting plate, wherein one side of the mounting plate is fixedly connected with the satellite-rocket butt joint ring, the other side of the mounting plate is fixedly connected with an optical load plate, and the optical load plate bears an optical load; damping layers which are laid on the outer surface of the optical loading plate and the outer wall of the satellite-rocket butt joint ring; a restraint layer which is laid on the outer surface of the damping layer; the mounting plate comprises a butt joint plate, a partition plate, an outer plate and an optical load plate; the partition plate is of a #-shaped structure, the outer plate is arranged on the periphery of the partition plate, the butt joint plate, the partition plate, the outer plate and the optical load plate are all aluminum honeycomb sandwich plates, and embedded parts are embedded in the single-machine equipment installation position and the rigidity reinforcing position of the aluminum honeycomb sandwich plates. The high-rigidity and high-damping satellite platform configuration has advantages of convenient single equipment configuration and installation, and high space utilization ratio. On the premise that the system is high in rigidity and small in additional mass, structural damping is effectively increased so as to attenuate vibration response of all components of the system.

    本发明公开了一种高刚度高阻尼卫星平台构型,属于航天器总体设计领域,本发明包括星箭对接环,其用于与火箭适配器对接;安装板,其一侧与星箭对接环固定连接,其另一侧固连有光学载荷板,光学载荷板承载光学载荷;光学载荷板外表面和星箭对接环外壁均敷设有阻尼层;阻尼层外表面敷设有约束层,安装板包括对接板、隔板、外板以及光学载荷板;隔板呈井字形结构,隔板四周布置有外板,对接板、隔板、外板以及光学载荷板均为铝蜂窝夹层板,铝蜂窝夹层板单机设备安装位置及刚度加强位置均预埋有埋件,本发明具有单机设备布局安装方便,空间利用率大,在系统高刚度和附加质量较小的前提下,有效增大结构阻尼以衰减系统各部组件振动响应的有益效果。


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    Title :

    High-rigidity and high-damping satellite platform configuration


    Additional title:

    一种高刚度高阻尼卫星平台构型


    Contributors:
    XIAO JUNKAI (author) / ZHANG LEI (author) / ZHENG XIAOFENG (author) / GU SONG (author) / CHEN SHANBO (author) / GAO FEI (author)

    Publication date :

    2021-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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