含孔复合材料层合板拉伸失效分析研究
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沈阳航空航天大学机电工程学院,沈阳航空航天大学机电工程学院,沈阳航空航天大学航空制造工艺数字化国防重点实验室

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V258

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辽宁省教育厅项目(L201611)和沈阳市科技计划项目(18-013-0-25)


Study on Tensile Failure Analysis of Composite Laminates with a Hole
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College of Electromechanical Engineering,Shenyang Aerospace University,,,

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    摘要:

    对国产T700/双马树脂基复合材料的含孔层合板进行了拉伸失效分析研究,分析了不同开孔直径和开孔形状对复合材料层合板拉伸性能的影响,利用有限元软件ABAQUS建立逐渐损伤失效模型,对复合材料层合板的拉伸强度进行数值模拟。研究结果表明:对于不同开孔直径的复合材料层合板,随着圆孔直径的增大,拉伸强度显著下降,对于不同开孔形状的复合材料层合板,含圆孔的层合板拉伸强度最大,然后依次是椭圆孔、方形孔、菱形孔,层合板的断裂模式都为过孔破坏。数值模拟得到的强度值与试验测量的强度值吻合较好,为含孔复合材料层合板的强度预测提供了一种有效的方法。

    Abstract:

    The tensile failure analysis of the perforated laminates of domestic T700/double horse resin matrix composite laminates was carried out. The effects of different hole diameter and hole shape on the tensile properties of composite laminates were analyzed. The finite element software ABAQUS was used to establish the tensile failure analysis. The failure model was gradually damaged, and the tensile strength of the composite laminates was numerically simulated. The results show that for composite laminates with different hole diameter, the tensile strength decreases significantly with the increase of the diameter of the circular pores. For composite laminates with different hole shape, the tensile strength of laminates with round holes is the largest, and then the elliptical, square and rhombic holes are in turn, the fracture mode of the laminate is the failure of the via. The intensity value obtained by numerical simulation agrees well with the measured strength value, which provides an effective method for strength prediction of porous composite laminates.

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许良,何懿,马少华,等. 含孔复合材料层合板拉伸失效分析研究[J]. 科学技术与工程, 2018, 18(34): .
xu liang, he yi,,et al. Study on Tensile Failure Analysis of Composite Laminates with a Hole[J]. Science Technology and Engineering,2018,18(34).

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  • 收稿日期:2018-08-05
  • 最后修改日期:2018-09-10
  • 录用日期:2018-09-26
  • 在线发布日期: 2018-12-20
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