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Nanoscopic origin of cracks in carbon fibre-reinforced plastic composites

机译:碳纤维增强塑料复合材料中的纳米镜头裂缝

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Voids and cracks can fatally degrade structural materials such as metals and ceramics but are tolerated in carbon fibre-reinforced plastic (CFRP) composites if monitored to prevent their growth to a critical size. Thus, the use of CFRPs as aeronautical structural materials requires an understanding of microscopic crack formation. However, this crack-formation mechanism remains unclear because experimental difficulties have hindered studies of relevant phenomena that occur before crack formation. Herein, we report high-resolution (~50?nm) and non-destructive three-dimensional observations of crack initiation and propagation under applied stress. This evaluation reveals that voids and cracks do not simply result from local stresses but instead occur largely through two competing nanoscale mechanisms, namely, fibre/plastic interface debonding and in-plastic crack initiation. Therefore, nanoscopic insights into these heterogeneities are essential for controlling crack initiation and determining reasonable safety margins for CFRP composite use.
机译:空隙和裂缝可以致命降低结构材料,例如金属和陶瓷,但如果监测以防止它们的生长至临界大小,则在碳纤维增强塑料(CFRP)复合材料中耐受。因此,CFRP作为航空结构材料的使用需要了解微观裂缝形成。然而,这种裂缝形成机制仍然不明确,因为实验困难已经阻碍了在裂缝形成前发生的相关现象的研究。在此,我们报告了高分辨率(〜50·nm)和施加应力下的裂纹启动和传播的非破坏性三维观察。该评估揭示了空隙和裂缝并不能仅仅由局部应力导致,而是主要通过两个竞争的纳米级机制,即纤维/塑料界面剥离和塑性裂纹启动。因此,纳米镜洞察这些异质性对于控制CFRP复合材料使用来控制裂纹引发和确定合理的安全余量是必不可少的。

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