空间大口径单体反射镜计量卸荷支撑研制中的关键技术

董得义; 庞新源; 张学军; 樊延超; 李志来; 杨利伟; 胡海飞

doi:10.3788/OPE.20192710.2165

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空间大口径单体反射镜计量卸荷支撑研制中的关键技术

微纳技术与精密机械 | 更新时间：2020-08-13

- 空间大口径单体反射镜计量卸荷支撑研制中的关键技术
- Key technology in developing of metrology mount for large aperture monolithic space-based mirror
- 光学精密工程 2019年27卷第10期页码：2165-2179
- 作者机构：
  
  中国科学院长春光学精密机械与物理研究所，吉林长春 130033
- 作者简介：
  
  [ "董得义(1979-)，男，天津人，博士，研究员，2002年、2005年、2012年于中科院长春光学精密机械与物理研究所分别获得学士、硕士、博士学位，主要从事空间光学遥感器有限元分析、结构优化设计、力学试验等方面的研究。E-mail：s200201029@163.com" ]
  [ "庞新源(1989-)，男，汉族，吉林集安人，研究实习员，2012年、2014年于哈尔滨工业大学分别获得学士、硕士学位，主要从事空间光学遥感器结构技术及精密机械方面的研究。E-mail：pangxyciomp@sina.com" ]
  胡海飞(1984-)，男，江西瑞金人，博士研究生，助理研究员，2007年于华中科技大学获得学士学位，2010年于大连理工大学获得硕士学位，主要从事原位光学检测支撑系统设计、光机结构集成分析和优化设计等方面的研究。E-mail：huhf@ciomp.ac.cn HU Hai-fei, E-mail: haifei.hu@163.com
- 基金信息：
  
  国家973重点基础研究发展计划资助项目(2016YFB0500100);国家自然科学基金资助项目(11873007)
- DOI：10.3788/OPE.20192710.2165
  中图分类号： TH751
- 收稿日期：2019-01-17，
  
  录用日期：2019-3-28，
  
  纸质出版日期：2019-10-15
- 稿件说明：
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董得义, 庞新源, 张学军, 等. 空间大口径单体反射镜计量卸荷支撑研制中的关键技术[J]. 光学精密工程, 2019,27(10):2165-2179.

De-yi DONG, Xin-yuan PANG, Xue-jun ZHANG, et al. Key technology in developing of metrology mount for large aperture monolithic space-based mirror[J]. Optics and precision engineering, 2019, 27(10): 2165-2179.
董得义, 庞新源, 张学军, 等. 空间大口径单体反射镜计量卸荷支撑研制中的关键技术[J]. 光学精密工程, 2019,27(10):2165-2179. DOI： 10.3788/OPE.20192710.2165.

De-yi DONG, Xin-yuan PANG, Xue-jun ZHANG, et al. Key technology in developing of metrology mount for large aperture monolithic space-based mirror[J]. Optics and precision engineering, 2019, 27(10): 2165-2179. DOI： 10.3788/OPE.20192710.2165.

摘要

通过对空间大口径单体反射镜支撑技术发展现状及发展趋势的调研，总结了当前大口径单体空间反射镜支撑技术中较为成熟的技术路线。在此技术路线中，计量卸荷支撑是必须要攻克的一项核心难题。本文介绍了计量卸荷支撑的概念，并针对计量卸荷支撑研制过程中的关键技术进行了深入的讨论，包括支撑点数量、位置及支撑力大小的确定方法，支撑力执行单元的方案设计以及计量卸荷精度的保证方法等；通过对计量卸荷支撑研制过程中关键技术的总结，期望对我国空间大口径单体反射镜的研制提供借鉴意义。

Abstract

Based on the investigation of the current situation and development trend of the large aperture monolithic space-based mirror support technology

this paper summarized the relatively mature technical route in the current support technology for the large aperture monolithic space-based mirror. In this technical route

the metrology mount was a bottleneck that must be resolved. This paper introduced the concept of the metrology mount and discussed the key technologies in its development. These included methods to determine the number and position of support points

the support force

to ensure unloading accuracy

etc. Summarizing the key technologies in metrology mount development will provide reference for the development of the large aperture monolithic space-based mirror in China.

关键词

Keywords

references

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