欢迎登录材料期刊网

材料期刊网

高级检索

基于对三维四向编织陶瓷基复合材料 CT 扫描结果的观察和理论分析,参考现有交织模型,建立了改进的胞元三维实体模型,较为真实地反映了材料内部的细观结构。模型内部纤维束横截面沿纤维束轴向不断发生形状和面积的周期性变化,纤维束横截面呈平行四边形、五边形交替变化,不同纤维束轴线间呈交织关系,接近材料内部纤维束间打紧后的挤压变形规律。通过测算平均纱线填充因子并配合有限元法获得了纤维束及材料的弹性性能,与试验结果符合较好。有限元仿真显示在材料单胞内,纤维束承担主要载荷,纤维束与基体的某些交界处往往会出现应力集中现象,可能是发生裂纹扩展及局部破坏的主要区域。该细观应力场的获得也为分析材料破坏机理和强度提供了基础。

Based on the CT scan results of 3D four-directional braided ceramic-matrix composites and theoretical analysis,referred to the existing interlaced model,an improved 3D cell element model was established.This model truly reflects the mesoscopic structure of the internal material.The yarns’cross-section along their axes model var-ied cyclically in shape and area,yarn’s cross-sections alternate transformed form parallelograms to pentagons,each yarn’s axis presented interlaced relationships,close to the extrusion deformation law of tight yarns in materials.By measuring the average yarn packing factor and using the finite element method,the elastic properties of yarns and materials were obtained.The predicted value agrees well with the test data.The finite element simulation reveals that the yarns undertake the main load in the materials’cell model.Some of the yarns and matrixes interfaces tend to appear stress concentration phenomenon.These areas could mostly produce crack propagations and local dama-ges.The determination of the mesoscopic stress field also provides a foundation for the analysis of failure mechanism and the strength of the materials.

参考文献

[1] 刘大响.高性能航空发动机的发展对材料技术的要求[J].燃气涡轮试验与研究,1998(03):1.
[2] 张立同;成来飞;徐永东.新型碳化硅陶瓷基复合材料的研究进展[J].航空制造技术,2003(1):24-32.
[3] 庞宝君;杜善义;韩杰才.三维四向编织复合材料细观组织及分析模型[J].复合材料学报,1999(3):135-139.
[4] 卢子兴;杨振宇;刘振国.三维四向编织复合材料结构模型的几何特性[J].北京航空航天大学学报,2006(1):92-96.
[5] 刘振国;商园春;董阿鹏;陈思思.三维四向编织复合材料改进模型的细观分析[J].材料导报,2013(18):148-152.
[6] 徐焜;许希武.四步法三维矩形编织复合材料的细观结构模型[J].复合材料学报,2006(5):154-160.
[7] 冯伟;王延荣;魏大盛.三维四向编织复合材料细观建模[J].航空动力学报,2013(6):1243-1249.
[8] 朱元林;崔海涛;温卫东;徐颖;张宏建.含纤维束截面形状变化的三维编织复合材料细观模型及刚度预报[J].复合材料学报,2012(6):187-196.
[9] 李嘉禄;刘谦.三维编织复合材料中纤维束横截面形状的研究[J].复合材料学报,2001(2):9-13.
[10] 邵将 .三维编织陶瓷基复合材料刚度模型及刚度性能分析研究[D].南京航空航天大学,2008.
[11] 巩龙东;申秀丽.基于能量法的三维四向编织复合材料细观建模[J].航空动力学报,2015(1):106-113.
[12] 丁丹烨 .三维编织复合材料编织几何和力学性能的细观分析[D].南京航空航天大学,2008.
[13] L. Chen;X.M. Tao.On the microstructure of three-dimensional braided preforms[J].Composites science and technology,19993(3):391-404.
[14] 石多奇;景鑫;杨晓光.三维四向编织CMCs拉伸性能及损伤演化数值预测[J].复合材料学报,2014(6):1543-1550.
[15] Fang Guo-dong;Liang Jun;Wang Yu.The effect of yarn distortion on the mechanical properties of 3D four-directional braided composites[J].Composites, Part A. Applied science and manufacturing,20094(4):343-350.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%