| 注册
首页|期刊导航|上海航天(中英文)|空间螺旋展开机构的研究进展综述

空间螺旋展开机构的研究进展综述

庞雪祺 罗海军 崔琦峰 马云彬 李方舟

上海航天(中英文)2025,Vol.42Issue(3):32-41,10.
上海航天(中英文)2025,Vol.42Issue(3):32-41,10.DOI:10.19328/j.cnki.2096-8655.2025.03.005

空间螺旋展开机构的研究进展综述

A Review of Research Progress on Space Spiral Deployable Mechanisms

庞雪祺 1罗海军 2崔琦峰 1马云彬 2李方舟2

作者信息

  • 1. 宇航空间机构全国重点实验室,上海 201108||上海宇航系统工程研究所,上海 201108
  • 2. 上海宇航系统工程研究所,上海 201108
  • 折叠

摘要

Abstract

With the continuous development of space technology,such as earth remote sensing of and deep space exploration,the space structure is becoming more and more large and complex,resulting in higher requirements for the lightweight,high stiffness,high precision,high stability,and high deployment ratio of space deployable mechanisms.The space spiral deployable mechanism mainly includes the spiral tube and actuator for controlled extension and retraction(STACER)and the coilable mast.The STACER has the advantages such as small volume,lightweight,and self-driven,and the coilable mast has the advantages such as high stiffness and lightweight.As a class of deployable mechanisms,the space spiral deployable mechanism is the basis for the construction of large and complex space structures,and is currently a hot topic of research and application at home and abroad.The working principle,research progress,and application of the space spiral deployable mechanism,as the research object,are investigated and elaborated,and the research and application progress of space spiral deployable mechanisms at home and abroad is summarized.

关键词

螺旋展开机构/卷筒式伸展机构(STACER)/盘绕式伸展机构/非线性/研究现状

Key words

spiral deployable mechanism/spiral tube and actuator for controlled extension and retraction(STACER)/coilable mast/none-linearity/research status

分类

航空航天

引用本文复制引用

庞雪祺,罗海军,崔琦峰,马云彬,李方舟..空间螺旋展开机构的研究进展综述[J].上海航天(中英文),2025,42(3):32-41,10.

基金项目

国家重点研发计划资助项目(2022YFB3402800) (2022YFB3402800)

上海航天(中英文)

2096-8655

访问量0
|
下载量0
段落导航相关论文