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Effect of tow gaps on impact strength of thin composite laminates made by Automated Fiber Placement: Experimental and semi-analytical approaches

机译:牵引间隙对自动化纤维放置薄复合层压板冲击强度的影响:实验和半分析方法

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摘要

Automated Fiber Placement is currently being used to manufacture large and complex composite structures. However, the final composite products may include manufacturing defects such as gaps and overlaps, which may reduce the mechanical performance of the structure. The effect of these defects on the compression strength and also medium velocity impact loading with the impact energies of 15 J 50 J have been experimentally investigated earlier. However, there is still a lack of knowledge in the study of impact response of and damage propagation in composite plates at low-velocity impact loading in the presence of the manufacturing defects. In this paper, the effect of periodically induced gaps on the low-velocity impact response of the thin composite plates has been experimentally investigated. For this purpose, quasi-isotropic Carbon/Epoxy polymer composite plates have been manufactured with AFP process, including periodical patterns of gaps, and the obtained impact responses of the plates have been compared with the results of the baseline samples. The baseline sample is a similar sample that has been manufactured by hand layup technique. Furthermore, a two degree of freedom mass-spring model is also proposed to account for the effect of the manufacturing defect on the impact response of the laminates with induced defects. The model includes a non-linear damage model to account the delamination propagation during the impact process. Ultrasonic C-Scan analysis has also been performed to capture the projected delamination pattern. Results indicate that the AFP manufacturing defects can reduce the impact resistance of the composite plates by about 17% and also has an effect on the delamination area of the samples for low levels of impact energy. Microscopic observation is further performed to investigate the interaction of manufacturing defects and damage caused by impact. It is shown that delamination initiation likely occurs in the gap area.
机译:目前用于制造大型和复杂的复合结构的自动化纤维放置。然而,最终的复合产品可以包括制造诸如间隙和重叠的制造缺陷,这可以降低结构的机械性能。这些缺陷对压缩强度的影响和中等速度冲击载荷与15J 50 J的冲击能量进行了实验研究。然而,在制造缺陷存在下,在低速冲击载荷下的复合板中的影响和损伤传播的研究仍然缺乏了知识。在本文中,经过实验研究了周期性地诱导对薄复合板的低​​速冲击响应的影响。为此目的,已经用AFP工艺制造了准各向同性碳/环氧聚合物复合板,包括间隙的周期性图案,并将板的所得冲击响应与基线样品的结果进行比较。基线样品是一种类似的样品,其是通过手动铺设技术制造的。此外,还提出了两度自由度质量弹簧模型,以解释制造缺陷对层压板与诱导缺陷的影响响应的影响。该模型包括非线性损伤模型,以考虑影响过程中的分层传播。还执行超声C扫描分析以捕获投影分层模式。结果表明,AFP制造缺陷可以将复合板的抗冲击性降低约17%,并且对水平的冲击能量的样品的分层区域也有影响。进一步进行微观观察以研究制造缺陷和抗冲击造成的损伤的相互作用。结果表明,分层启动可能发生在间隙区域中。

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