首页 | 本学科首页   官方微博 | 高级检索  
     

空间引力波望远镜主反射镜系统的结构设计优化
引用本文:王辰忠,胡中文,陈忆,许明明,陈力斯.空间引力波望远镜主反射镜系统的结构设计优化[J].红外与激光工程,2020,49(7):20190469-1-20190469-10.
作者姓名:王辰忠  胡中文  陈忆  许明明  陈力斯
作者单位:1.中国科学院国家天文台南京天文光学技术研究所,江苏 南京 210042
基金项目:中国科学院战略性先导科技专项;国家自然科学基金
摘    要:针对空间引力波望远镜主反射镜系统的结构及支撑组件进行了设计与优化。主反射镜运用了侧面3点支撑对镜体进行约束,并对支撑点的选取与布局进行了研究。反射镜采用能够实现较大弯曲刚度的背部钻孔式半封闭构型,通过有限元计算结合多目标遗传算法对反射镜轻量化结构进行了参数优化,在不降低面形精度的条件下使镜体结构轻量化率达到74%。设计了一种由两个无阻隔串联式柔度单元组合而成的可调节双轴连杆型Bipod柔性铰链结构,其可对反射镜面形误差进行补偿。建立了柔性铰链并联机构作用于反射镜的数学模型,对其进行了基于MATLAB的参数取值分析,并通过有限元方法完成了对参数取值的修正。最后进行了空间热载荷条件下的反射镜面形分析,结果表明反射镜面形误差优于λ/60,满足设计要求。

关 键 词:引力波望远镜    主反射镜    柔性支撑    面形误差
收稿时间:2020-04-07

Structural design optimization of space gravitational wave telescope primary mirror system
Affiliation:1.Nanjing Institute of Astronomical Optics & Technology, National Astronomical Observatories, Chinese Academy of Sciences, Nanjing 210042, China2.CAS Key Laboratory of Astronomical Optics & Technology(Nanjing Institute of Astronomical Optics & Technology), Nanjing 210042, China3.University of Chinese Academy of Sciences, Beijing 100049, China
Abstract:The structure and supporting components of the primary mirror system of space gravitational wave telescope were designed and optimized. The side three-point support was used to restrain the mirror body with the primary mirror, and the selection and layout of support points were studied. The mirror adopted a semi-enclosed structure with back drill holes, which can achieve large bending stiffness. The lightweight structure of the mirror was optimized by finite element calculation combined with multi-objective genetic algorithm. The lightweight ratio of the mirror structure reached 74% without reducing the surface accuracy. An adjustable bi-axis bipod flexure hinge structure composed of two non-barrier series flexibility elements was designed, which can compensate the surface error of the mirror. The mathematical model of the flexible hinge parallel mechanism acting on the mirror was established, and the parameters were analyzed based on MATLAB. The parameters were corrected by finite element method. Finally, the analysis of mirror shape under space thermal load was carried out. The results show that the error of mirror shape is better than λ/60, which meets the design requirements.
Keywords:
本文献已被 万方数据 等数据库收录!
点击此处可从《红外与激光工程》浏览原始摘要信息
点击此处可从《红外与激光工程》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号