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

  • Zhiyong Yang*
  • , Zhanwen Tang
  • , Yongjie Xie
  • , Hanqiao Shi
  • , Boming Zhang
  • , Hongjun Guo
  • *此作品的通讯作者
  • Beihang University
  • China Aerospace Science and Technology Corporation
  • CAS - Xi'an Institute of Optics and Precision Mechanics

科研成果: 期刊稿件文章同行评审

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.

源语言英语
页(从-至)105-112
页数8
期刊Applied Composite Materials
25
1
DOI
出版状态已出版 - 1 2月 2018

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