空间环境模拟系统光学窗口组件设计

徐明林; 解鹏

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空间环境模拟系统光学窗口组件设计

徐明林, 解鹏

文章导航 > 红外与激光工程 > 2014 > 43(S1): 30-35

徐明林, 解鹏. 空间环境模拟系统光学窗口组件设计[J]. 红外与激光工程, 2014, 43(S1): 30-35.

引用本文:

徐明林, 解鹏. 空间环境模拟系统光学窗口组件设计[J]. 红外与激光工程, 2014, 43(S1): 30-35.

Xu Minglin, Xie Peng. Design for optical window in space environment simulation system[J]. Infrared and Laser Engineering, 2014, 43(S1): 30-35.

Citation:

Xu Minglin, Xie Peng. Design for optical window in space environment simulation system[J]. Infrared and Laser Engineering, 2014, 43(S1): 30-35.

空间环境模拟系统光学窗口组件设计

徐明林,
解鹏

1.
中国科学院长春光学精密机械与物理研究所,吉林长春 130033

详细信息

作者简介:
徐明林(1988-),男,研究实习员,硕士,主要从事空间机构设计方面的工作.Email:xuminglin_hit@126.com

中图分类号: V416.8

Design for optical window in space environment simulation system

1.
Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China

摘要: 光学窗口组件作为空间环境模拟系统与外界的接口,是不可或缺的重要组成部件.空间环境模拟系统共有两类光学窗口组件,针对两类光窗组件分别进行了结构方案设计.通过强度理论公式对光窗组件进行了强度校核,采用有限元分析软件计算了压力对光学玻璃表面变形的影响,并分析了光学玻璃表面变形对光窗组件光学性能的影响.计算结果表明:工作过程中,通光口径为150 mm的光窗组件光学玻璃产生的应力为0.82 MPa;通光口径为350 mm的光窗组件光学玻璃产生的应力为3.28 MPa,均满足强度要求.利用Zemax软件分析得到,通光口径为150 mm的光窗组件波像差PV值为/8;通过计算得到通光口径为350 mm的光窗组件在170 mm~190 mm环带区域内光程差为0.8 nm,均满足光学性能要求.因此,光学窗口组件结构方案设计既满足强度和可靠性要求,又满足光学性能要求,整个光学窗口组件安全可靠.
- 光学窗口 /
- 空间环境模拟系统 /
- 波像差 /
- 光程差
Abstract: As the interface with the outside space environment simulation system, optical window is an indispensable important component parts. Space environment simulation system consists of two types of optical window. Based on both the windows, in this paper, components structure scheme design was carried out respectively. The strength theory formula was used to check the intensity of the window components; The finite element analysis software was used to calculate the effect of pressure on the optical glass surface deformation, and to analyze the impact of optical glass surface deformation results of the optical properties of the optical window assembly. The results show that aperture 150 mm, the work stress of optical window assembly is 0.82 MPa; Aperture 350 mm, the work stress is 3.28 MPa, meet the strength requirements. Zemax software was used to calculate the wavefront error(PV)of aperture 150 mm optical window assembly is /8; within 170 mm-190 mm band area, the optical path difference of aperture 350mm optical window assembly is 0.8 nm; Both of them can satisfy the requirements of optical performance. Therefore, this design meets not only the strength and reliability requirements, but also the optical performance requirements, So the design of entire window assembly is safe and reliable.
- optical window /
- space environment simulation system /
- wavefront error /
- optical path difference

[1]
[2]	Pi Guiying, Shi Qingguo. Analysis on domestic and international space environment simulation test conditions[J]. Environmental Technology, 2013(4): 41-42. (in Chinese). 皮桂英, 石庆国. 国内外空间环境模拟试验条件分析[J]. 环境技术, 2013(4): 41-42.
[3]	Li Ming, Wu Qingwen, Yu Fei. Optimization of optical window glass thickness based on the thermal optical analysis[J]. Acta Optica Sinaica, 2010, 30(1): 210-213. (in Chinese). 黎明, 吴清文, 余飞. 基于热光学分析的光学窗口玻璃厚度的优化[J]. 光学学报, 2010, 30(1): 210-213.
[4]
[5]	Zhao Lixin. Thermal-optical evaluation to optical windows of space camera[J]. Acta Optica Sinaica, 1988, 18(10):1440-1444. (in Chinese) 赵立新. 空间相机光学窗口的热光学评价[J]. 光学学报, 1998, 18(10): 1440-1444.
[6]
[7]	Chen Hua, Shi Zhenguang, Sui Yongxin, et al. Thermal deformation analysis of optical surface caused by environmental temperature during intrferometric testing[J]. Acta Optica Sinaica, 2011(1): 135-139. (in Chinese) 陈华, 史振广, 隋永新, 等. 干涉检测中环境温度引起的镜面变形分析[J]. 光学学报, 2011(1): 135-139.
[8]
[9]	Bames W P, Jr. Some effects of aerospace thermal environments on high-acuity optical systems[J]. Appl Opt, 1966, 5(5): 671-675.
[10]
[11]	Pearson E, Stepp L. Response of large optical mirror to thermal distributions[C] //SPIE, 1987, 748: 215-228.
[12]
[13]	Noreen Harned, Robert Harped, Ramsey Melugin. Alignment and evaluation of the cryogenic corrected infrared astronomical satellite(IRAS)telescope[J]. Opt Eng, 1981, 20(2):202195.
[14]
[15]	Pepi J W, Barnes W P. Thermal distortion of a thin low expansion fused silica mirror[C] //SPIE, 1983, 450: 40-49.
[16]
[17]	Yang Jiawen, Huang Qiaolin, Han Youmin. Application and simulation in fitting optical surface with Zernike polynomial[J]. Spacecraft Recovery Remote Sensing, 2010, 31(5): 49-55. (in Chinese) 杨佳文, 黄巧林, 韩友民. Zernike多项式在拟合光学表面面形中的应用及仿真[J]. 航天返回与遥感, 2010, 31(5): 49-55.
[18]
[19]	Shan Baozhong, Wang Shuyan, Niu Hanben, et al. Zernike polynomial fitting method and its application[J]. Opt Precision Engineering, 2012, 10(3): 318-323. (in Chinese) 单宝忠, 王淑岩, 牛憨笨, 等. Zernike多项式拟合方法及应用[J]. 光学精密工程, 2002, 10(3): 318-323.

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空间环境模拟系统光学窗口组件设计

徐明林,
解鹏

1. 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:
徐明林(1988-),男,研究实习员,硕士,主要从事空间机构设计方面的工作.Email:xuminglin_hit@126.com

收稿日期: 2014-10-17
修回日期: 2014-11-20
刊出日期: 2015-01-25

中图分类号: V416.8

关键词:

摘要: 光学窗口组件作为空间环境模拟系统与外界的接口,是不可或缺的重要组成部件.空间环境模拟系统共有两类光学窗口组件,针对两类光窗组件分别进行了结构方案设计.通过强度理论公式对光窗组件进行了强度校核,采用有限元分析软件计算了压力对光学玻璃表面变形的影响,并分析了光学玻璃表面变形对光窗组件光学性能的影响.计算结果表明:工作过程中,通光口径为150 mm的光窗组件光学玻璃产生的应力为0.82 MPa;通光口径为350 mm的光窗组件光学玻璃产生的应力为3.28 MPa,均满足强度要求.利用Zemax软件分析得到,通光口径为150 mm的光窗组件波像差PV值为/8;通过计算得到通光口径为350 mm的光窗组件在170 mm~190 mm环带区域内光程差为0.8 nm,均满足光学性能要求.因此,光学窗口组件结构方案设计既满足强度和可靠性要求,又满足光学性能要求,整个光学窗口组件安全可靠.

English Abstract

Design for optical window in space environment simulation system

1. Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China

Received Date: 2014-10-17
Rev Recd Date: 2014-11-20
Publish Date: 2015-01-25

Keywords:

Abstract: As the interface with the outside space environment simulation system, optical window is an indispensable important component parts. Space environment simulation system consists of two types of optical window. Based on both the windows, in this paper, components structure scheme design was carried out respectively. The strength theory formula was used to check the intensity of the window components; The finite element analysis software was used to calculate the effect of pressure on the optical glass surface deformation, and to analyze the impact of optical glass surface deformation results of the optical properties of the optical window assembly. The results show that aperture 150 mm, the work stress of optical window assembly is 0.82 MPa; Aperture 350 mm, the work stress is 3.28 MPa, meet the strength requirements. Zemax software was used to calculate the wavefront error(PV)of aperture 150 mm optical window assembly is /8; within 170 mm-190 mm band area, the optical path difference of aperture 350mm optical window assembly is 0.8 nm; Both of them can satisfy the requirements of optical performance. Therefore, this design meets not only the strength and reliability requirements, but also the optical performance requirements, So the design of entire window assembly is safe and reliable.