一种主承力结构与贮箱支架耦合的一体化装置

By designing an integrated device that couples the main load-bearing structure with the tank support, the problem of not being able to install both the tank and the satellite antenna simultaneously in the internal structure of a small satellite was solved, achieving a simple structure, easy installation, multifunctionality, and high rigidity.

CN121493286BActive Publication Date: 2026-07-17AEROSPACE DONGFANGHONG SATELLITE

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
AEROSPACE DONGFANGHONG SATELLITE
Filing Date
2025-11-19
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing small satellite internal structure designs cannot meet the requirements of small size, light weight and compact internal space, cannot install tanks and satellite antennas at the same time, and have complex structures and are inconvenient to install.

Method used

Design an integrated device coupling the main load-bearing structure and the tank support, including a multi-functional tank support, a tank, a satellite base plate, a central partition plate and side plates, made of aluminum alloy. The tank and satellite antenna are installed through the combination of the tank support base plate flange ring, support cylinder, reinforcing ribs and antenna mounting flange, and can be used as a structural corner box and cable beam.

Benefits of technology

It improves the structural mechanical response, enhances the stability of the central partition and the space utilization of the entire satellite, simplifies the installation operation, reduces weight, and improves the rigidity and versatility of the entire satellite.

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Abstract

本发明涉及一种主承力结构与贮箱支架耦合的一体化装置,属于结构技术领域;包括多功能贮箱支架、贮箱、卫星底板、中隔板和侧板;其中,卫星底板为轴向水平放置的矩形板状结构;多功能贮箱支架为筒状结构;多功能贮箱支架轴向竖直安装在卫星底板上表面的中心;贮箱安装在多功能贮箱支架的顶部;侧板竖直安装在卫星底板的侧壁处;中隔板竖直安装在卫星底板的上表面;中隔板垂直与侧板的中部设置,且中隔板的中部设置有与多功能贮箱支架和贮箱形状对应的通孔;多功能贮箱支架和贮箱从对应通孔穿过;本发明的小卫星直属件贮箱支架,可以安装贮箱和星表天线,同时还可以充当结构角盒和电缆梁的作用,可以提高结构力学响应、结构简单、安装操作方便。
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