The invention discloses a mounting structure of a propellant storage box for a satellite and a mounting method of the propellant storage box, the mounting structure is used for mounting the propellant storage box on a long partition plate of the satellite, and the mounting structure comprises a storage box flange support, a supporting angle box and a reinforcing oblique beam; the storage box flange bracket is connected with the propellant storage box; the storage box flange bracket is fixedly connected with the long partition plate through the supporting corner box; the reinforcing cant beams are connected with the storage box flange support and the supporting corner boxes respectively. The installation method comprises the steps that when the satellite structure is in the state that the bottom plate, the long partition plates and the top plate are installed in place, the supporting corner boxes are installed at the corresponding positions of the two long partition plates and pre-positioned; the storage box flange support is horizontally placed on a plurality of supporting angle boxes, the supporting angle boxes are adjusted, and the supporting angle boxes are fixedly connected with the long partition plates; the storage tank flange support is disassembled; the propellant storage box is installed on the storage box flange support and fixed; mounting and fixing a storage tank flange bracket on the support angle box together with the propellant storage tank; mounting a reinforcing oblique beam; and the propellant storage box is mounted and fixed.

    本发明公开了一种卫星用推进剂储箱安装结构及推进剂储箱的安装方法,该安装结构用于将推进剂储箱安装至卫星的长隔板上,包括储箱法兰支架、支撑角盒和加强斜梁;储箱法兰支架连接推进剂储箱,支撑角盒将储箱法兰支架与长隔板固定连接;加强斜梁分别连接储箱法兰支架与支撑角盒。安装方法包括卫星结构处于底板、长隔板、顶板安装到位状态,将支撑角盒安装到两块长隔板相应位置,预定位;将储箱法兰支架水平放置到多个支撑角盒上,调整支撑角盒,将支撑角盒与长隔板固定连接;拆下储箱法兰支架;将推进剂储箱安装到储箱法兰支架上并完成固定;连同推进剂储箱一起,将储箱法兰支架安装到支撑角盒上、固定;安装加强斜梁;实现推进剂储箱安装固定。


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    Title :

    Propellant storage tank mounting structure for satellite and propellant storage tank mounting method


    Additional title:

    卫星用推进剂储箱安装结构及推进剂储箱的安装方法


    Contributors:
    LIU JIANG (author) / HAN JIANBIN (author) / HU YONGQIANG (author) / XU XIN (author) / SONG KAIWEN (author) / ZHANG YUEYANG (author)

    Publication date :

    2023-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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