三维四向编织复合材料改进模型弹性性能计算

刘振国; 商园春; 董阿鹏; 吕明云

三维四向编织复合材料改进模型弹性性能计算

北京航空航天大学航空科学与工程学院, 北京 100191

详细信息

中图分类号: TB332
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出版历程
- 收稿日期: 2013-03-27
- 网络出版日期: 2014-01-20

Elastic properties computation for three-dimensional and four-directional braided composites based on an improved model

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 针对三维四向编织复合材料，在改进的矩形截面单胞模型的基础上，考虑了相邻纤维束之间的界面粘结效应，推导了单胞的几何特性与编织工艺参数之间的数学关系，并且采用ANSYS软件建立了实体有限元模型，得到了等效弹性性能参数；之后，分析了各工艺参数对弹性模量的影响规律.通过有限元计算的材料弹性性能常数与试验数据符合较好，较为真实地模拟了该材料的细观结构，对三维编织复合材料的设计和工艺具有一定的参考价值.
- 三维四向 /
- 编织复合材料 /
- 矩形截面单胞 /
- 界面 /
- 有限元模型
Abstract: In order to study the three-dimensional and four-directional braided composites on the basis of an improved unit cell model with rectangular cross-section, the relationship between the geometric properties of the cells and the braiding parameters were deduced with considering the effects of adhesive layers between adjacent yarns. The ANSYS software was used to build a finite element model (FEM) and obtained equivalent elastic performance parameters. The effects of the main process parameters on the elastic properties were discussed. The calculation results by the finite element model coincide well with the experimental data, which can relatively truly reflect the micro-structure of this material. They have the certain reference value for the three-dimensional braided composites design and technology.
- three-dimensional and four-directional /
- braided composites /
- rectangular section /
- adhesive layers /
- finite element model (FEM)

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参考文献(13)

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