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首页> 外文期刊>International Journal of Mechanical Sciences >Finite element analyses on three-point low-cyclic bending fatigue of 3-D braided composite materials at microstructure level
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Finite element analyses on three-point low-cyclic bending fatigue of 3-D braided composite materials at microstructure level

机译:3-D编织复合材料三点低周弯曲疲劳微观结构的有限元分析

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摘要

This paper presents numerical analyses of fatigue behaviors of three-dimensional (3-D) 4-step rectangular braided composite material under three-point low-cyclic bending. A microstructure model of the 3-D braided composite was established to calculate the bending fatigue deformation and failure with a finite element method (FEM). The stiffness degradation and failure morphologies were obtained from the FEM results and compared with those from experimental. The stress distributions, stress hysteresis and failures of fiber tows and resins at different parts of the 3-D braided composite material have been collected from the FEM calculations to analyze the fatigue failure mechanisms. The influences of the braided preform microstructure on the fatigue damage were discussed. It is found that the surface yarns share more loads than the yarns of the inner part. The stress concentration appeared at the regions with larger changes of fiber tow orientation angles. The fatigue damage evolutions were also used to explain the mechanical behaviors degradation. The crack generation and fatigue damages development of the braided composite appeared at early stages and followed by crack propagation afterwards. A series of damage evolution at the different loading cycles were obtained to unveil the fatigue damage mechanisms. From the investigation, the fatigue resistance of 3-D braided composite could be optimized from improving the mechanical behaviors of surface fiber tows and decreasing the change of fiber tows orientation angles.
机译:本文对三维(3-D)4步矩形编织复合材料在三点低周弯曲下的疲劳行为进行了数值分析。建立了3-D编织复合材料的微观结构模型,以有限元方法(FEM)计算弯曲疲劳变形和破坏。刚度退化和破坏形态从有限元分析结果中获得,并与实验结果进行比较。从FEM计算中收集了3-D编织复合材料不同部位的纤维束和树脂的应力分布,应力滞后以及破坏,以分析疲劳破坏机理。讨论了编织的预型件微观结构对疲劳损伤的影响。发现表面纱线比内部纱线承担更多的负载。应力集中出现在纤维束取向角变化较大的区域。疲劳损伤的演变也可以用来解释机械性能的下降。编织复合材料的裂纹产生和疲劳损伤的发展出现在早期,随后裂纹扩展。获得了在不同加载周期下的一系列损伤演变,以揭示疲劳损伤机理。通过研究,可以通过改善表面纤维束的机械性能和减少纤维束取向角的变化来优化3-D编织复合材料的疲劳强度。

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