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Low-Velocity Impact Behavior of Interlayer/Intralayer Hybrid Composites Based on Carbon and Glass Non-Crimp Fabric

机译:基于碳和玻璃非压接织物的中间层/体内混合复合材料的低速冲击性能

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摘要

Composites have gained wide use in structural applications; however, they are sensitive to impact damage. The use of hybrid composites is an effective way to overcome this deficiency. The effects of various hybrid structures of interlayer and intralayer warp-knitted fabrics with carbon and glass fibers on the low-velocity impact behavior of composite laminates were studied. Drop-weight impact tests were conducted on two types of interlayer, sandwich and intralayer hybrid composite laminates, which were compared with homogenous composite laminates. During low-velocity impact tests, the time histories of impact forces and absorbed energy by laminate were recorded. The failure modes were analyzed using the micro-CT (computed tomography) and C-scan techniques. The results revealed that the hybrid structure played an important role in peak force and the absorbed energy, and that the hybrid interface had an influence on damage modes, whereas the intralayer hybrid composite laminate damage was affected by the impact location. The intralayer hybrid laminate with C:G = 1:1 exhibited better impact resistance compared to the other hybrid structures.
机译:复合材料在结构应用中越广泛使用;然而,它们对冲击损伤敏感。使用混合复合材料是克服这种缺陷的有效方法。研究了中间层和腔内经线针织织物的各种杂交结构与碳和玻璃纤维对复合材料层压板的低速冲击行为的影响。在两种类型的中间层,夹层和腔内杂化复合层压层上进行滴重试验,与均匀复合层压板进行比较。在低速冲击试验期间,记录了抗冲击力和通过层压材料吸收能量的时间历史。使用Micro-CT(计算机断层扫描)和C扫描技术进行分析故障模式。结果表明,混合结构在峰值力和吸收能量中起着重要作用,并且杂交界面对损伤模式有影响,而血液化杂交复合层压材料损伤受冲击位置的影响。与其他杂交结构相比,具有C:G = 1:1的体内杂交层压材料表现出更好的抗冲击性。

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