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Evolution of damage during the fatigue of 3D woven glass-fibre reinforced composites subjected to tension-tension loading observed by time-lapse X-ray tomography

机译:经时延X射线断层扫描观察拉伸 - 拉伸载荷下三维玻璃纤维增​​强复合材料疲劳过程中损伤的演变

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摘要

The development of fatigue damage in a glass fibre modified layer-to-layer three dimensional (3D) woven composite has been followed by time-lapse X-ray computed tomography (CT). The damage was found to be distributed regularly throughout the composite according to the repeating unit, even at large fractions of the total life. This suggests that the through-thickness constraint provides a high level of stress redistribution and damage tolerance. The different types of damage have been segmented, allowing a quantitative analysis of damage evolution as a function of the number of fatigue cycles. Transverse cracks were found to initiate within the weft after just 0.1% of life, followed soon after (by 1% of life) by longitudinal debonding cracks. The number and extent of these multiplied steadily over the fatigue life, whereas the spacing of transverse cracks along with weft/binder debonding saturated at 60% of life and damage in the resin pockets occurred only just before final failure.
机译:在玻璃纤维改性的层到层三维(3D)机织复合材料中出现疲劳损伤之后,出现了延时X射线计算机断层扫描(CT)。发现损坏是根据重复单元有规律地分布在整个复合材料中的,即使在总寿命的很大部分也是如此。这表明,贯穿厚度约束提供了较高水平的应力重新分布和损伤容限。对不同类型的损伤进行了细分,从而可以根据疲劳循环次数对损伤演变进行定量分析。发现横向裂纹仅在寿命的0.1%内就在纬纱内引发,随后不久(寿命的1%)随即出现纵向脱胶裂纹。它们的数量和程度在疲劳寿命中稳定增长,而横向裂纹的间距以及纬线/粘结剂的脱粘在寿命的60%处达到饱和,并且树脂囊的损坏仅在最终失效之前发生。

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