Effect of Lamina Thickness of Prepreg on the Surface Accuracy of Carbon Fiber Composite Space Mirrors

被引:3
|
作者
Yang, Zhiyong [1 ,2 ]
Tang, Zhanwen [2 ]
Xie, Yongjie [3 ]
Shi, Hanqiao [2 ]
Zhang, Boming [1 ]
Guo, Hongjun [2 ]
机构
[1] Beihang Univ, Sch Mat Sci & Engn, Beijing 100191, Peoples R China
[2] Aerosp Res Inst Mat & Proc Technol, Beijing 100076, Peoples R China
[3] Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710068, Shaanxi, Peoples R China
关键词
Carbon fiber composite; Space mirror; Lamina thickness of prepreg; Finite element analysis; TECHNOLOGY;
D O I
10.1007/s10443-017-9604-x
中图分类号
TB33 [复合材料];
学科分类号
摘要
Composite space mirror can completely replicate the high-precision surface of mould by replication process, but the actual surface accuracy of the replication composite mirror always decreases. Lamina thickness of prepreg affects the layers and layup sequence of composite space mirror, and which would affect surface accuracy of space mirror. In our research, two groups of contrasting cases through finite element analyses (FEA) and comparative experiments were studied; the effect of different lamina thicknesses of prepreg and corresponding lay-up sequences was focused as well. We describe a special analysis model, validated process and result analysis. The simulated and measured surface figures both get the same conclusion. Reducing lamina thickness of prepreg used in replicating composite space mirror is propitious to optimal design of layup sequence for fabricating composite mirror, and could improve its surface accuracy.
引用
收藏
页码:105 / 112
页数:8
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