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大型空间离轴三反相机分体支撑结构设计
引用本文:宋伟阳,解鹏,王循. 大型空间离轴三反相机分体支撑结构设计[J]. 光学精密工程, 2021, 29(3): 571-581
作者姓名:宋伟阳  解鹏  王循
作者单位:中国科学院长春光学精密机械与物理研究所,吉林长春130033;中国科学院大学,北京100049;中国科学院天基动态快速光学成像技术重点实验室,吉林长春130033;中国科学院长春光学精密机械与物理研究所,吉林长春130033;中国科学院天基动态快速光学成像技术重点实验室,吉林长春130033
基金项目:国家重大科研仪器研制项目资助(No.51827806)。
摘    要:针对某1m分辨率、200 km幅宽的大尺度空间相机框架支撑结构轻质量、高刚度的设计要求,设计了一种轻型分体支撑结构.首先从大型空间离轴三反相机研制需求出发,综合比刚度、热稳定性及加工工艺等因素选择了性能良好的高体份SiCp/Al复合材料;然后以结构质量分数为约束条件,建立以基频为目标函数的拓扑优化数学模型,得到了拓扑结...

关 键 词:大型空间相机  拓扑优化  分体支撑  轻量  尺寸优化

Design of lightweight split support structure for large space off-axis three mirror camera
SONG Wei-yang,XIE Peng,WANG Xun. Design of lightweight split support structure for large space off-axis three mirror camera[J]. Optics and Precision Engineering, 2021, 29(3): 571-581
Authors:SONG Wei-yang  XIE Peng  WANG Xun
Affiliation:(Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China;University of Chinese Academy of Sciences,Beijing 100049,China;Key Laboratory of Space-based Dynamic&Rapid Optical Imaging Technology,Chinese Academy of Sciences,Changchun 130033,China)
Abstract:According to the design requirements of lightweight and high-stiffness large-scale space camera frame support structures with a 1-m resolution and 200-km width,a lightweight split support structure is designed.In this study,a high-volume SiCp/Al composite material with good performance is selected based on the development requirements of a large space off-axis three-mirror camera,including the specific stiffness,thermal stability,and processing technology.Then,with the structure mass fraction as the constraint condition,a topology optimization mathematical model is established with the fundamental frequen?cy as the objective function,and the optimal force transfer path of each split structure with clear topological results is obtained.The size of each part of the main support structure is optimized,and the optimal config?uration and design size of each split structure are obtained.After the design,the total weight of the split support structure was 227.8 kg,and the lightweight rate reached 93.9%,which meets the requirements of high lightweight and stiffness.The results of finite-element analysis and mechanical prototype test show that the split support structure meets the stiffness requirements of the whole remote sensing camera with the fundamental frequency greater than 50 Hz,and the deformation of the mirror is within the tolerance range under the working condition of 5°C,which fully satisfies the requirements of the satellite platform for optical loads.The mechanical prototype mirror assembly offset angle is less than 22°before and after the vibration test,showing its good stability,which proves the rationality and feasibility of the topology op?timization and size optimization methods.The design of the proposed split support structure has a high en?gineering practice value for the support design of large space off-axis cameras.
Keywords:large size space camera  topology optimization  split support  lightweight  size optimization
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