航空学报 > 2007, Vol. 28 Issue (2): 294-300

小编织角三维编织复合材料拉伸强度模型

徐焜,许希武,田静   

  1. 南京航空航天大学 结构强度研究所
  • 收稿日期:2005-12-07 修回日期:2006-04-17 出版日期:2007-03-10 发布日期:2007-03-10
  • 通讯作者: 许希武

A Model for Tensile Strength Prediction of Low Angel 3D Braided Composites

XU Kun,XU Xi-wu,TIAN Jing   

  1. Research Institute of Structures and Strength,  Nanjing University of Aeronautics and Astronautics
  • Received:2005-12-07 Revised:2006-04-17 Online:2007-03-10 Published:2007-03-10
  • Contact: XU Xiwu

摘要:

采用离散化方法,基于等应变及等应力混合平均思想,结合桥联模型,建立了四步法小编织角三维四向矩形编织复合材料的拉伸强度模型。该模型不仅可以获得材料的等效弹性性能,而且能直接得到各组分材料(纤维束中纤维和基体、纤维束外基体)的细观应力分布,并基于纤维和基体失效准则,揭示了材料在单向拉伸载荷作用下的失效机理并预报了材料拉伸强度。数值分析结果与实验数据基本吻合,证明了该模型的有效性,经讨论材料主要工艺参数对拉伸强度和应力分布的影响,得到了一些有参考价值的结论。

关键词: 三维编织, 复合材料, 小编织角, 拉伸强度, 桥联模型

Abstract:

A model to predict the uniaxial tensile strength of the 4-step 3D braided rectangular composite with low braiding angle is established. By the scheme of discretization, the iso-strain and iso-stress mixed averaging assumptions are applied to analyze the elastic mechanical properties of the material. Coupled with the bridging model, the stress distribution in the fibers and matrix are obtained. Based on the failure criteria of the constituents of the material, failure mechanism of the materials under the tensile load is disclosed and the model predictes the tensile strength is efficient.

Key words: 3D , braided,  , composite,  , low , braiding , angle,  , tensile , strength,  , bridging , micromechanics , model

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