一种轻小型舱外试验载荷支持装置

By designing a lightweight and compact external test payload support device, the problem of low cost-effectiveness of lightweight and compact payload mounting in existing technologies has been solved, achieving efficient mechanical connection and resource support for the payload and reducing implementation costs.

CN117087879BActive Publication Date: 2026-07-17LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
Filing Date
2023-08-08
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing load adapters are mainly used for larger-sized and heavier extravehicular loads, resulting in low cost-effectiveness for mounting small and light loads, high manufacturing and design thresholds, high implementation costs, and the need to perform functions such as robotic arm transfer and thermal control and power supply for extravehicular operations independently.

Method used

A lightweight, compact external test load support device was designed, comprising a mechanical mounting plate, an extended top plate, and a multi-functional column. It is equipped with multiple mounting interfaces, enables automatic loading and unloading of loads via a robotic arm, and provides power supply and information resource connectivity, supporting the integration of multiple lightweight, compact loads.

Benefits of technology

It enables mechanical connection and resource support for lightweight payloads, simplifies the process of payloads entering and leaving the cabin, reduces implementation costs, and improves the efficiency and flexibility of payload loading.

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Abstract

本申请涉及空间应用设备技术领域,具体而言,涉及一种轻小型舱外试验载荷支持装置,包括机械安装板、扩展顶板以及多功能柱,其中:多功能柱为盒体结构,内部设置有电气控制组件,底面固定在机械安装板上;扩展顶板固定在多功能柱的顶面上;机械安装板的顶面设置有第一安装接口,底面设置有第二安装接口;多功能柱的前侧面设置有第三安装接口,后侧面设置有第四安装接口,多功能柱的左侧面和右侧面设置有第五安装接口;扩展顶板的底面设置有第三安装接口,扩展板的顶面设置有第四安装接口。本申请与不同尺寸的轻小型试验载荷连接,可以由机械臂实现整体装置的自动进出舱,解决了装置及其携带的轻小型试验载荷进出舱及与空间站的结构连接的需求。
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