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Numerical and Experimental Investigation of the Sensitivity of Carbon Nanotube and Graphene Nanocomposites to MMOD Impact Damage for Inflatable Structures

机译:碳纳米管和石墨烯纳米复合材料对充气结构MMOD冲击损伤敏感性的数值和实验研究

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Inflatable structures used for space applications are highly prone to micrometeoroid and orbital debris (MMOD) impact damages, which have the potential to affect the performance of the structures. Although multiple layers of impact resistant materials are used as shield to ensure the safety of the structures, an efficient structural health monitoring system is needed to track its damage state. In this work, we demonstrate that hybrid nanocomposites, made of carbon nanotubes (CNTs) and graphene nanoplatelets (GNPs) with an epoxy matrix, can potentially be used as impact damage detection sensors. The electrical resistance of these flexible nanocomposites is sensitive to strain and presence of damage. An improvement of the sensitivity to damage is observed in the hybrid nanocomposites, compared to monofiller CNT nanocomposites. To understand the sensing mechanisms of the nanocomposites due to damages, we use a two-dimensional percolation model with Monte Carlo simulations to model the electrical conductivity of nanocomposites with CNTs and GNPs fillers. The change in resistance due to the presence of holes in the modeled nanocomposites is examined.
机译:用于太空应用的可充气结构极易受到微流星体和轨道碎片(MMOD)的冲击破坏,这可能会影响结构的性能。尽管多层抗冲击材料被用作防护层以确保结构的安全性,但仍需要有效的结构健康监测系统来跟踪其损坏状态。在这项工作中,我们证明了由碳纳米管(CNT)和具有环氧基质的石墨烯纳米片(GNP)制成的杂化纳米复合材料可以潜在地用作冲击损伤检测传感器。这些柔性纳米复合材料的电阻对应变和损坏的存在敏感。与单填料CNT纳米复合材料相比,在杂化纳米复合材料中观察到了对损伤敏感性的改善。为了了解由于损伤而引起的纳米复合材料的传感机制,我们使用带有蒙特卡洛模拟的二维渗流模型来模拟具有CNTs和GNPs填料的纳米复合材料的电导率。检查了由于建模的纳米复合材料中存在孔而引起的电阻变化。

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