编织复合材料损伤演化模型:最新进展

IF 4.03
Chen Wang, Anish Roy, Vadim V. Silberschmidt, Zhong Chen
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引用次数: 15

摘要

用机织或编织纺织品增强的复合材料由于纱线交织,具有很高的结构稳定性和优异的损伤容忍度。编织复合材料具有高刚度重量比和高强度重量比,在航空航天和汽车部件以及运动防护装备中具有吸引力。在这些潜在的应用中,组件通常会受到多向静态、冲击和疲劳载荷的影响。为了加强此类应用的材料分析和设计,了解编织复合材料的力学行为和开发预测能力变得至关重要。近年来,新的建模技术的发展取得了重大进展,使编织复合材料的静态和动态响应得以阐明。然而,由于其独特的交错几何结构和复杂的破坏模式,对构件的损伤起始和演化进行预测仍然是一个挑战。因此,全面的文献分析,在这项工作中提出的重点是回顾最先进的编织复合材料的渐进损伤分析与有限元模拟。近年来,系统地介绍了编织复合材料的力学性能、冲击响应和疲劳分析模型。本文综述了应用于纱线和复合材料单元胞的失效准则和损伤演化规律的重要性、优点和局限性。为今后编织复合材料的有限元模拟研究提供了良好的参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Modelling of Damage Evolution in Braided Composites: Recent Developments

Modelling of Damage Evolution in Braided Composites: Recent Developments

Composites reinforced with woven or braided textiles exhibit high structural stability and excellent damage tolerance thanks to yarn interlacing. With their high stiffness-to-weight and strength-to-weight ratios, braided composites are attractive for aerospace and automotive components as well as sports protective equipment. In these potential applications, components are typically subjected to multi-directional static, impact and fatigue loadings. To enhance material analysis and design for such applications, understanding mechanical behaviour of braided composites and development of predictive capabilities becomes crucial. Significant progress has been made in recent years in development of new modelling techniques allowing elucidation of static and dynamic responses of braided composites. However, because of their unique interlacing geometric structure and complicated failure modes, prediction of damage initiation and its evolution in components is still a challenge. Therefore, a comprehensive literature analysis is presented in this work focused on a review of the state-of-the-art progressive damage analysis of braided composites with finite-element simulations. Recently models employed in the studies on mechanical behaviour, impact response and fatigue analyses of braided composites are presented systematically. This review highlights the importance, advantages and limitations of as-applied failure criteria and damage evolution laws for yarns and composite unit cells. In addition, this work provides a good reference for future research on FE simulations of braided composites.

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