空间遥感相机碳纤维机身结构设计

郭疆; 邵明东; 王国良; 孙继明

doi:10.3788/OPE.20122003.0571

您当前的位置：

首页 >

文章列表页 >

空间遥感相机碳纤维机身结构设计

微纳技术与精密机械 | 更新时间：2020-08-12

- 空间遥感相机碳纤维机身结构设计
- Design of optical-mechanical structure made of CFC in space remote sensing camera
- 光学精密工程 2012年20卷第3期页码：571-578
- 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：
- 基金信息：
  
  中国科学院"();优秀博士学位论文、院长奖获得者科研启动专项基金"();资助项目()
- DOI：10.3788/OPE.20122003.0571
  中图分类号： V447.3
- 收稿日期：2011-02-28，
  
  修回日期：2011-03-18，
  
  网络出版日期：2012-03-22，
  
  纸质出版日期：2012-03-22
- 稿件说明：
移动端阅览
郭疆, 邵明东, 王国良, 孙继明. 空间遥感相机碳纤维机身结构设计[J]. 光学精密工程, 2012,(3): 571-578

GUO Jiang, SHAO Ming-dong, WANG Guo-liang, SUN Ji-ming. Design of optical-mechanical structure made of CFC in space remote sensing camera[J]. Editorial Office of Optics and Precision Engineering, 2012,(3): 571-578
郭疆, 邵明东, 王国良, 孙继明. 空间遥感相机碳纤维机身结构设计[J]. 光学精密工程, 2012,(3): 571-578 DOI： 10.3788/OPE.20122003.0571.

GUO Jiang, SHAO Ming-dong, WANG Guo-liang, SUN Ji-ming. Design of optical-mechanical structure made of CFC in space remote sensing camera[J]. Editorial Office of Optics and Precision Engineering, 2012,(3): 571-578 DOI： 10.3788/OPE.20122003.0571.

摘要

针对离轴三反相机光学系统对机身结构的要求

采用碳纤维复合材料制备关键部件

设计了合适的相机机身结构。设计的离轴三反相机采用的复合材料占整机重量的32%。机身结构为非对称形

光学系统中主、次镜间距为850 mm

反射镜接口定位精度要求间隔为0.005 mm、偏心为0.005 mm、倾斜为5。通过有限元软件对设计结果进行分析、优化和检验

完成了机身结构的优化设计。计算结果表明

该机身结构具有较好的刚度、较轻的重量

能够满足光学设计对间隔

偏心和倾斜的要求。对总装完成的相机进行了力学环境试验和热真空试验

结果证明了该相机机身结构在力、热等环境条件下稳定性良好

其一阶谐振频率在120 Hz以上

相机调制传递函数在0.2以上

满足离轴三反空间相机各反射镜对空间位置精度和稳定性的要求。

Abstract

For demands of optical systems in a off-axis three-mirror camera on the optical-mechanical structure

an appropriate optical-mechanical structure was designed by taking Carbon Fiber Composite(CFC) as the key components of the camera. The weight of CFC in designed camera makes up 32% that of the total system. Furthermore

this optical-mechanical structure is asymmetric

the system spacing in the primary

secondary mirror is 850 mm

and the mirror positioning accuracy demands its interval

eccentric and tilt to be 0.005 mm

0.005 mm

and 5

respectively. The Finite Element method was used to analyze and optimize the design

results show that the optical-mechanical structure has better stiffness

lighter weight

and can meet the requirements of optical system for intervals

eccentrics and tilts. A mechanics environmental test and a thermal vacuum test were performed

and results demonstrate that the optical-mechanical structure in the camera has excellent stability in mechanics

thermal and other environmental conditions

its first order harmonic frequencies are above 120 Hz

and the modulation transfer function is more than 0.2. These results prove that the proposed structure can provide reasonable spatial location and stability for the reflective mirrors in off-axis three-mirror cameras.

关键词

Keywords

references

颜昌翔,许杰,彭岩. 离轴三反空间光学望远系统的杂散光抑制 [J]. 光学精密工程, 2010, 18(2): 289-293. YAN CH X, XU J, PENG Y. Stray light suppression of three-mirror off-axis space optical telescope [J]. Opt. Precision Eng., 2010, 18(2): 289-293. (in Chinese)[2] 李威,刘宏伟,郭权锋,等. 空间相机主次镜间的薄壁筒和支杆组合支撑结构 [J]. 光学精密工程, 2010, 18(12): 2633-2641. LI W, LIU H W, GUO Q F, et al.. Combined supporting structure of thin wall joint cylinder and supporting bar between primary mirror and second mirror in space camera [J]. Opt. Precision Eng., 2010, 18(12): 2633-2641. (in Chinese)[3] 常军, 姜会林,翁志成,等. 大视场、长焦距空间光学系统的设计 [J].兵工学报, 2003, 24(1): 42-44. CHANG J, JIANG H L WENG ZH CH, et al.. Design of wide angle space optical systems of long focal length [J]. Acta Armamentarii, 2003, 24(1): 42-44. (in Chinese)[4] 伍和云, 王培纲. 离轴反射式光学系统设计 [J]. 光电工程, 2006, 33(1): 34-37. WU H Y, WANG P G. Designs of reflective off-axis system [J]. Opto Electronic Engineering, 2006, 33(1):34-37. (in Chinese)[5] 姜会林. 关于二级光谱问题的探讨 [J]. 光学学报,1982(3): 225-232. JIANG H L. On the secondary spectrum [J]. Acta Optica Sinica, 1982(3): 225-232. (in Chinese)[6] JURANEK H J, SAND R, SCHWEIZER J, et al.. Off axis telescope the future generation of earth observation telescopes [J].SPIE, 1998, 3439:104-115.[7] KORSCH D C. Reflective optics[J]. SPIE, 1987, 751:230-235.[8] 潘君骅. 具有三个二次曲面反射镜的光学系统研究 [J]. 光学学报, 1988(8):717-721. PAN J Y. A study of the optical system with three mirrors of second order surface [J]. Acta Optica Sinica, 1988(8):717-721. (in Chinese)[9] 薛旭成,石俊霞,吕恒毅,等. 空间遥感相机TDICCD积分级数和增益的优化设置 [J]. 光学精密工程, 2011, 19(4): 857-863. XUE X CH, SHI J X, LV H Y, et al.. Optimal set of TDI CCD integration stages and gains of space remote sensing cameras [J]. Opt. Precision Eng., 2011, 19(4): 857-863. (in Chinese)[10] 郑耿峰,张柯,韩双丽,等. 空间TDICCD 相机动态成像地面检测系统的设计 [J]. 光学精密工程, 2010, 18(3): 623-629. ZHENG G F, ZHANG K, HAN SH L, et al.. Design of test system for motion images of space TDICCD cameras[J]. Opt. Precision Eng., 2010, 18(3): 623-629. (in Chinese)[11] 马天波,郭永飞,李云飞. 科学级TDICCD相机的行频精度 [J]. 光学精密工程, 2010, 18(9): 2028-2035. MA T B, GUO Y F, LI Y F. Precision of row frequency of scientific grade TDICCD camera [J]. Opt. Precision Eng., 2010, 18(9): 2028-2035. (in Chinese)[12] 刘磊,高明辉,李丽富,等. 大视场空间相机轻型遮光罩的研制 [J]. 光学技术, 2009, 35(6): 822-824. LIU L, GAO M H, LI L F, et al.. Development of light baffle of space camera with large field of view [J]. Optical Technique, 2009, 35(6): 822-824. (in Chinese)[13] 丁亚林,田海英,刘立国,等. 一种提高碳纤维复合材料框架结构应用性能的结构技术 [J]. 光学精密工程, 2003, 11(3): 287-290. DING Y L, TIAN H Y, LIU L G, et al.. Use of pre-embedded parts to improve the performance of carbon fibre framework [J]. Opt. Precision Eng., 2003, 11(3): 287-290. (in Chinese)[14] 田海英. 碳纤维复合材料应用于航天光学遥感器遮光镜筒 [J]. 光学技术, 2003, 29(6): 704-706. TIAN H Y. Carbon fibre composite material used in space optical instrument [J]. Optical Technique, 2003, 29(6): 704-706. (in Chinese)[15] 解永杰,张禹康,陈荣利,等. 小挠度碳纤维复合材料镜筒设计 [J]. 应用光学, 2007, 28(6): 728-731. XIE Y J, ZHANG Y K, CHEN R L, et al.. Structure design of little distortion CFC lens barrel in space telescope [J]. Journal of Applied Optics, 2007, 28(6): 728-731. (in Chinese)[16] 李威,刘宏伟. 空间光学遥感器中碳纤维复合材料精密支撑构件的结构稳定性 [J]. 光学精密工程, 2008, 16(11): 2173-2179. LI W, LIU H W. Structure stability of precision component made of carbon fiber composite in space optical remote sensor [J]. Opt. Precision Eng., 2008, 16(11): 2173-2179. (in Chinese)[17] 王晓洁,惠雪梅,尤丽虹,等. M40J/改性氰酸酯复合材料耐水性能研究 [J]. 宇航学报, 2010, 31(1): 244-248. WANG X J, HUI X M, YOU L H, et al.. Studying water uptake effects on M40J carbon fiber/modified cyanate ester composite [J]. Opt. Precision Eng., 2010, 31(1): 244-248. (in Chinese)[18] 王永宪,王兵,任建岳. 空间相机碳纤维支撑结构改进及拓扑优化设计 [J]. 红外与激光工程, 2009, 38(4): 702-704. WANG Y X, WANG B, REN J Y. Improvement of carbon fibre support structure and topology optimization design for space camera [J]. Infrared and Laser Eng., 2009, 38(4): 702-704. (in Chinese)[19] 林再文. 碳纤维增强复合材料在空间光学结构中的应用 [J]. 光学精密工程, 2007, 15(8): 1181-1185. LIN Z W. Application of carbon fibre reinforced composite to space optical structure wide coverage and high resolution [J]. Opt. Precision Eng., 2007, 15(8): 1181-1185. (in Chinese)[20] 盛磊. 轻型空间相机遮光罩组件的研制 [J]. 航天返回与遥感, 2006, 2: 41-45. SHENG L. Development of light baffle of space camera [J]. Spacecraft Recovery & Remote Sensing, 2006, 2: 41-45. (in Chinese)

浏览量

402

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

小卫星用反作用飞轮系统设计

大口径空间遥感相机主反射镜支撑设计