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编织参数对轴编C/C复合材料热膨胀系数的影响

李书良 顾靖伟 李国才 史宏斌 侯晓

固体火箭技术2012,Vol.35Issue(5):670-674,5.
固体火箭技术2012,Vol.35Issue(5):670-674,5.

编织参数对轴编C/C复合材料热膨胀系数的影响

Effect of weave parameters on thermal expansion coefficient of 4D in-plane C/C composites

李书良 1顾靖伟 2李国才 2史宏斌 2侯晓2

作者信息

  • 1. 西北工业大学航天学院,西安710072
  • 2. 中国航天科技集团公司四院四十一所,固体火箭发动机燃烧、结构与内流场国防科技重点实验室,西安710025
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摘要

Abstract

The thermal expansion properties of the 4D in-plane C/C composites were predicted by combined FEM and the energy method. The validity of the prediction method is proved by comparing the prediction values with the experiment results. The effects of the changing of weave space and the diameter of fiber bundles on the thermal expansion properties of this material were predicted. The result shows that the thermal expansion coefficient (CTE) of 4D in-plane C/C composite decreases with the increase of weave space. Moreover, with the increasing diameter, the thermal expansion coefficient in axial direction decreases, while the coefficient in radical direction increases.

关键词

轴棒法多维编织C/C复合材料/编织参数/热膨胀系数/能量法/有限元法

Key words

4D-inplane C/C composites/ weave parameters/ thermal expansion coefficient/ energy based method/ finite element method

分类

航空航天

引用本文复制引用

李书良,顾靖伟,李国才,史宏斌,侯晓..编织参数对轴编C/C复合材料热膨胀系数的影响[J].固体火箭技术,2012,35(5):670-674,5.

基金项目

国家973项目(61391). (61391)

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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