The invention relates to the field of satellite structure installation, and discloses a satellite plate installation structure. The satellite plate mounting structure comprises a first mounting structure, a second mounting structure, a third mounting structure and a fourth mounting structure, the first mounting structure comprises a first convex block and a first groove, the first groove comprises a first avoiding groove and a first clamping groove which are communicated with each other, and the first convex block can extend into the first avoiding groove and transversely move into the first clamping groove; the second mounting structure comprises a second convex block and a second groove, the second groove comprises a second avoiding groove and a second clamping groove which are communicated with each other, and the second convex block can extend into the second avoiding groove and transversely move into the second clamping groove after longitudinally moving; the third mounting structure comprises a third convex block and a third groove which are matched with each other; the fourth mounting structure comprises a fastener, a first connecting hole and a second connecting hole, and the fastener penetrates through the first connecting hole and is matched with the second connecting hole. The structure is simple and reliable, installation is convenient and fast, and the installation efficiency is improved.

    本发明涉及卫星结构安装领域,公开一种卫星板安装结构。所述卫星板安装结构包括第一安装结构、第二安装结构、第三安装结构和第四安装结构,第一安装结构包括第一凸块和第一凹槽,第一凹槽包括相连通的第一避让槽和第一卡槽,第一凸块能够伸入第一避让槽内,并横移至第一卡槽内;第二安装结构包括第二凸块和第二凹槽,第二凹槽包括相连通的第二避让槽和第二卡槽,第二凸块能够伸入第二避让槽内,并纵移后再横移至第二卡槽内;第三安装结构包括相配合的第三凸块和第三凹槽;第四安装结构包括紧固件、第一连接孔和第二连接孔,紧固件贯穿第一连接孔,并与第二连接孔配合。本发明结构简单可靠,安装方便快捷,提高了安装效率。


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    Title :

    Satellite plate mounting structure


    Additional title:

    一种卫星板安装结构


    Contributors:
    MOU XIA (author) / HUANG HONGZHOU (author) / ZHANG ZHENXING (author) / WANG YANG (author) / LIU YANYONG (author) / LIANG LEI (author) / LI BAOPING (author) / WANG SHI (author) / LIU RUI (author) / LIU LISHUAI (author)

    Publication date :

    2022-08-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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