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首页> 外文期刊>International Journal of Damage Mechanics >Impact Damage Resistance, Response, and Mechanisms of Laminated Composites Reinforced by Through-Thickness Stitching
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Impact Damage Resistance, Response, and Mechanisms of Laminated Composites Reinforced by Through-Thickness Stitching

机译:厚度拼接增强层压复合材料的冲击损伤抵抗性,响应和机理

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In this article, the study of impact damage of laminated composites reinforced by through-thickness stitching is investigated and presented in threefold. Specimens stitched with varying stitch density and stitch thread thickness are subjected to low-velocity impact via a drop-weight machine. Impact damage resistance is first studied by examining the extent of delamination area in damaged specimens using ultrasonic C-scan analysis. It is revealed that higher stitch density is more capable of impeding delamination growth by arresting cracks at closer interval and suppressing crack propagation. The use of thicker stitch thread offers slight improvement to damage resistance by marginal reduction in delamination propagation, and is more pertinent at high impact energy levels. Impact damage response is then analyzed from the impact history response curves of impacted laminates. The impact response of load - time graphs demonstrates that the onset of delamination is not influenced by stitch density and stitch thread thickness, but the maximum residual impact force is related to the delamination size of the laminates, which is sequentially related to stitch parameters. Finally, impact damage mechanisms are elucidated by employing X-ray radiography and micro-Computed Tomography to reveal subsurface damages, primarily dominated by intralaminar matrix cracks, interlaminar delamination, and stitch fiber/matrix debonding. It is revealed that stitches act as crack initiation sites, due to the presence of weak resin-rich pockets around stitch threads, thus inadvertently resulting in densely stitched composites having more stitch-induced matrix cracks upon impact loading. Contrarily, specimens with higher stitch density and thread thickness are more capable of impeding delamination growth by effectively bridging delamination cracks and arresting crack propagation. Principal mechanisms responsible for impact resistance performance of stitching namely crack arresting and crack bridging are presented and discussed.
机译:在本文中,对通过全厚度缝合增强的层压复合材料的冲击损伤进行了研究,并提出了三方面的研究。通过落锤式机器,以不同的针迹密度和针迹线厚度缝制的样本会受到低速冲击。首先通过使用超声C扫描分析检查受损样品中的分层区域的范围来研究抗冲击破坏性。结果表明,较高的线迹密度通过在较近的间隔处阻止裂纹并抑制裂纹扩展,更能够阻止分层增长。通过略微减少分层传播,使用较粗的线迹可以略微改善抗损伤性,并且在高冲击能级下更有意义。然后从冲击层压板的冲击历史响应曲线分析冲击损伤响应。载荷-时间图的冲击响应表明,脱层的开始不受线圈密度和线迹厚度的影响,但是最大残余冲击力与层压板的脱层尺寸有关,而层脱层的尺寸与线圈参数顺序相关。最后,通过使用X射线射线照相术和微型计算机断层扫描来揭示表面下的破坏,阐明了冲击破坏的机理,这些破坏主要是由层内基质裂纹,层间分层和缝线纤维/基质剥离造成的。揭示出,由于在缝线周围存在弱的富含树脂的袋,所以缝线充当裂纹起始部位,因此无意地导致在冲击载荷下紧密缝制的复合材料具有更多由缝线引起的基体裂纹。相反,具有较高针迹密度和线粗的样品通过有效地桥接分层裂纹并阻止裂纹扩展,更能够阻止分层的增长。提出并讨论了影响缝合抗冲击性能的主要机理,即止裂和桥接。

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