Multi-scale fatigue damage analysis in filament-wound carbon fiber reinforced epoxy composites for hydrogen storage tanks

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES
Imen Feki , Mohammadali Shirinbayan , Samia Nouira , Robert Tie Bi , Jean-Baptiste Maeso , Cedric Thomas , Joseph Fitoussi
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Abstract

This article presents the findings of a multi-scale experimental study on carbon fiber-reinforced epoxy composites (CFRP) used in lightweight hydrogen storage pressure vessels produced via filament winding. The research employs a combination of tension-tension load-controlled fatigue tests and high-resolution physical-chemical characterization and porosity quantification to assess the impact of porosity on mechanical performance. The findings demonstrate that porosity has a detrimental impact on mechanical properties, acting as nucleation sites for damage mechanisms such as crack initiation, fiber-matrix separation and fiber breakage. At the mesoscopic level, microdefects coalesce into transverse cracks and delamination, resulting in complex failure modes under cyclic loading. The results of the tensile tests demonstrated that the orientation of the fibers has a significant impact on the mechanical behavior of the material. The ±15° configuration demonstrated superior tensile strength and modulus, while the ±30° and multilayer configurations exhibited higher ductility. The results of the fatigue testing confirmed that fiber orientation has a significant impact on fatigue life, with the ±15° configuration proving to be the most resistant. Microscopic analysis indicated that pores act as damage initiation points, accelerating failure through matrix cracking, fiber-matrix debonding, and delamination. This study highlights the need for improved porosity control during manufacturing to enhance the durability of hydrogen storage systems. Additionally, it provides valuable insights for optimizing fiber orientation to improve fatigue performance in practical applications.

Abstract Image

用于储氢罐的丝状缠绕碳纤维增强环氧树脂复合材料的多尺度疲劳损伤分析
本文介绍了对通过长丝缠绕生产的轻质储氢压力容器中使用的碳纤维增强环氧树脂复合材料(CFRP)进行多尺度实验研究的结果。研究结合了拉伸-张力负载控制疲劳试验、高分辨率物理化学表征和孔隙率量化,以评估孔隙率对机械性能的影响。研究结果表明,孔隙率对机械性能有不利影响,是裂纹萌发、纤维基质分离和纤维断裂等损伤机制的成核点。在中观层面,微缺陷会凝聚成横向裂缝和分层,从而在循环加载下产生复杂的破坏模式。拉伸试验结果表明,纤维的取向对材料的机械性能有重大影响。±15°配置表现出更高的拉伸强度和模量,而±30°和多层配置则表现出更高的延展性。疲劳测试结果证实,纤维取向对疲劳寿命有显著影响,±15°结构的抗疲劳能力最强。显微分析表明,孔隙是破坏的起始点,通过基体开裂、纤维与基体脱粘和分层加速破坏。这项研究强调了在制造过程中改进孔隙率控制以提高储氢系统耐久性的必要性。此外,它还为优化纤维取向以提高实际应用中的疲劳性能提供了宝贵的见解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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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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