首页|2.5维机织复合材料TCM细观分胞模型研究

2.5维机织复合材料TCM细观分胞模型研究

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从真实反映制造工艺对2.5维机织复合材料厚度方向上纱线束截面尺寸的影响出发,在传统二元分胞模型基础上提出了一种新的胞体—过渡胞,进而在细观尺度上建立了 2.5维机织复合材料三胞体模型(TCM).该模型反映了不同厚度位置经纱几何参数的差异,弥补了传统分胞方法的不足.基于TCM和刚度体积平均方法预测了几种典型2.5维机织复合材料包括弹性模量在内的力学性能,并与实验结果进行了对比.分析结果表明,基于TCM的预测结果相比传统模型预测精度更高;另外,经向弹性模量在厚度方向上呈现"马鞍"形分布;对10-6w材料,过渡单胞和内层单胞的经向弹性模量相差约6%,而传统分胞方法无法准确反映材料表层/次外层和内层材料结构及力学性能的差异.
Study on Ternary-Cell Model for 2.5 Dimensional Woven Composites
For the purpose of taking the impact of manufacturing procedure on the cross-section of fiber bundles along thickness direction into account,a Ternary-Cell microscopic model(TCM)for 2.5 dimensional(2.5-D)woven composites was proposed by in-troducing a new type of RVE(transition cell)into traditional cell partition method.Compared with conventional models,the terna-ry cell model is capable of capturing the differences of geometrical parameters of surficial,sub-surficial,and internal fiber yarns.Moreover,mechanical parameters including Moduli of several types of typical 2.5-D woven composites were predicted based on TCM as well as stiffness matrix average method.The results showed that the predictions agreed well with experimental data;in ad-dition,a characteristic"saddle-shape"curve was observed for longitudinal tensile modulus along thickness direction;and for 10-6w,the comparative error of longitudinal tensile stiffness between surface cell,transition cell,and inner cell was around 6%,which indicated the deficiency of traditional cell partition method.

2.5 Dimensional Woven CompositesCell Partition MethodStiffness PredictionMicroscopic Geome-try ModelStiffness Volume Average

刘浩龙、温卫东、崔海涛、张宏建

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上海飞机设计研究院,上海 201210

南京航空航天大学能源与动力学院,江苏 南京 210016

2.5维机织复合材料 单胞划分方法 三胞体模型 刚度预测

2024

机械设计与制造
辽宁省机械研究院

机械设计与制造

CSTPCD北大核心
影响因子:0.511
ISSN:1001-3997
年,卷(期):2024.406(12)