摘要
针对Φ510mmSiC超轻量化反射镜的研制,提出了一剖面为船型、内部为正三角形、面板加密呈正六边形的轻量化结构。当设计重量为1.85kg时,通过调整各个结构参数与另外两种相同重量的轻量化结构进行了比较。结果表明,在同样背部6点支撑作用下,该超轻量化结构在光轴指向天顶时由自重引起的面形(RMS)具有较大优势。利用Patran\Nastran有限元软件模拟计算了该超轻量化反射镜在光轴水平状态下的自重镜面变形,并对其进行了热力学及动力学特性分析。分析结果显示,该超轻量化反射镜各项指标均能满足使用要求。最终,根据设计结果试制加工了一块镜坯,初步加工后的重量约为2.2kg,面密度约为10.8kg/m2,已达到目前SiC超轻量化反射镜的先进水平。
To develop a Φ510 mm SiC ultra-lightweight mirror,this paper proposes an ultra-lightweight structure with a section in ship form,an internal structure in regular-triangle,and a face plate reinforced with regular-hexagon.When the design weight is 1.85 kg,the structure performance is compared with those of other two lightweight structures with the same weight by adjusting all structure parameters.It is shown that in the same 6 point supportings on mirror backs,this ultra-lightweight structure owns absolute advantages in the gravitational deformation of mirror surface（RMS） as comparing with other two structures when the optical axis is pointed to the zenith.Furthermore,Patran／Nastran finite element software is used to simulate and calculate the gravitational deformation of the mirror surface when the axis is pointed to the horizon,and its thermodynamic and dynamical characteristics are analyzed.The results present that all performance indexes of this ultra-lightweight mirror meet requirements of applications.Finally,according to the design,a mirror blank with a weight about 2.2 kg and surface density about 10.8 kg/m2 is fabricated.With excellent performance, it has been up to the today＇s advanced level in the SiC ultra-lightweight mirror field.
出处
《光学精密工程》
EI
CAS
CSCD
北大核心
2012年第8期1718-1724,共7页
Optics and Precision Engineering
基金
中国科学院光电技术研究所前沿部署项目(No.C09K007)
