航空精密制造技术2024,Vol.60Issue(3) :13-19.

基于多尺度方法的平纹机织SiC/SiC复合材料力学性能预测

Prediction of Mechanical Properties Using Multi-scale Approach for Plain Woven SiC/SiC Composites

胡元杰 陈绍雄 朱书华 徐志胜 杨发建
航空精密制造技术2024,Vol.60Issue(3) :13-19.

基于多尺度方法的平纹机织SiC/SiC复合材料力学性能预测

Prediction of Mechanical Properties Using Multi-scale Approach for Plain Woven SiC/SiC Composites

胡元杰 1陈绍雄 1朱书华 1徐志胜 1杨发建1
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作者信息

  • 1. 南京航空航天大学 航空学院,南京 210016
  • 折叠

摘要

本文基于平纹机织SiC/SiC复合材料的多尺度特性以及微观结构的周期性,建立了微观尺度(纤维尺度)和中观尺度(纱线尺度)的单胞模型,利用Abaqus软件计算得出纤维尺度模型的力学性能参数,将这些参数导入纱线尺度模型中,同时编写相应的UMAT子程序来判断材料的损伤起始和损伤演化过程,模拟了平纹机织SiC/SiC复合材料在单向拉伸时的损伤演化以及破坏过程.结果表明X向拉伸应力应变曲线与试验曲线吻合良好,有效地预测了平纹机织SiC/SiC复合材料的强度性能和损伤演化过程.

Abstract

Based on the multi-scale characteristics and the periodicity of microstructure of plain woven SiC/SiC composites,the unit cell models of microscale(fiber-scale)and mesoscale(yarn-scale)are established.The mechanical properties parameters of the microscale model were calculated by Abaqus software,which were then introduced into the yarn-scale model.The corresponding UMAT subroutine was written to judge the damage initiation and damage evolution process of the material.The damage evolution and failure process of plain woven SiC/SiC composites under uniaxial tension were simulated.The results show that the X-direction tensile stress-strain curve is in good agreement with the experimental curve.The strength properties and damage evolution of plain woven SiC/SiC composites are predicted.

关键词

多尺度/平纹机织SiC/SiC复合材料/力学性能

Key words

multi-scale/plain woven SiC/SiC composites/mechanical property

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基金项目

国家科技重大专项(Y2019-I-0018-0017)

出版年

2024
航空精密制造技术
北京航空精密机械研究所

航空精密制造技术

CSTPCD
影响因子:0.228
ISSN:1003-5451
参考文献量7
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