玻璃纤维增强原位可聚合热塑性和生物环氧基复合材料疲劳载荷失效分析

IF 7 Q2 MATERIALS SCIENCE, COMPOSITES
J.R. Pothnis , A. Hejjaji , G.S. Bhatia , A. Comer
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引用次数: 0

摘要

本实验研究了由原位可聚合热塑性塑料和生物基环氧树脂基复合材料制备的玻璃纤维增强聚合物基复合材料在拉伸-拉伸疲劳载荷下的断裂和破坏机制。对于这两种材料系统,疲劳测试的结果是0°、90°和准各向同性(QI)层压板的线性S-N曲线,以及±45°和±30°层压板配置的非线性(幂律)S-N曲线。然而,研究的主要焦点是低周和高周疲劳载荷下的失效机制。在宏观层面上,不同基体对特征失效模式的影响通常是最小的,除了损伤高度局部化的90°层合板外,所有层合板在整个规范区域都表现出分布损伤。然而,利用SEM和元素组成分析进行的微观分析显示,生物环氧树脂(界面)和热塑性塑料(内聚)在纤维基体界面附近的破坏机制存在显著差异。总的来说,这两种基质在良好的实验室条件下都表现出良好的疲劳性能,并为未来海上可再生能源结构实现更可持续的基质选择奠定了基础。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Failure analysis under fatigue loading of glass fibre reinforced in-situ polymerizable thermoplastic and Bio-epoxy based Composites
This experimental study investigates the fracture and failure mechanisms of glass fiber reinforced polymer matrix composites fabricated using an in-situ polymerizable thermoplastic and a bio-based epoxy matrix subjected to tension-tension fatigue loading. For both material systems, fatigue tests resulted in linear S-N curves for the 0°, 90° and Quasi-Isotropic (QI) laminates and non-linear (power law) S-N curves for the ±45° and ±30° laminate configurations. However, the main focus of the study was on the failure mechanisms for both the low-cycle and high-cycle fatigue loading regimes. At the macro level, the effect of the different matrices on the characteristic failure mode was generally minimal with all lay-ups exhibiting distributed damage throughout the gauge region except for the 90° laminates where damage was highly localised. However, micro level analysis conducted using SEM and elemental composition analysis revealed significantly different failure mechanisms in the vicinity of the fibre matrix interface for the bio-epoxy (interfacial) and the thermoplastic (cohesive). Overall, both matrices show promise in terms of fatigue performance under benign laboratory conditions and as a stepping stone towards achieving more sustainable matrix options for offshore renewable energy structures in the future.
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来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
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