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Impact damage growth in carbon fibre aluminium laminates

机译:碳纤维铝层压板的冲击损伤增长

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摘要

The paper presents an analysis of the response of fibre metal laminate based on aluminium and carbon fibre reinforced polymer to low-velocity impact. The comparison of the force time dependencies with the actual effects of the indenter laminate system (using high-speed cameras) contributed to the identification of the representative points and ranges that determine characteristic changes in the laminate structure in terms of damage and specific forms of its degradation. The authors proposed five damage states of aluminium-carbon laminate during low-velocity impact. The initial stages of the damage is associated with internal degradation and plastic deformation of the laminate until the impact resistance of the fibre metal laminates indicated by the authors. Matrix cracks, delaminations between composite layers with different orientation, as well as delaminations at the metal/composite interface are the characteristic damage modes. The catastrophic failure with cracking of the aluminium layers and composite materials and impactor penetration of the hybrid laminate are the next stages. Identifying damage initiation, propagation and its stages in live-time analysis of an aluminium-carbon laminate under impact may lead to making progress in this kind of laminates and understanding and interpretation of the impact phenomena. (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文分析了基于铝和碳纤维增强聚合物的纤维金属层压板对低速冲击的响应。力时间依赖性与压头层压系统(使用高速相机)的实际效果的比较有助于识别代表点和范围,这些点和范围确定层压结构在损伤及其特定形式方面的特征变化降解。作者提出了铝-碳层压板在低速冲击过程中的五个破坏状态。损坏的初始阶段与层压板的内部降解和塑性变形有关,直到作者指出的纤维金属层压板的耐冲击性为止。基质裂纹,具有不同方向的复合层之间的分层以及金属/复合材料界面的分层是典型的破坏模式。铝层和复合材料开裂以及混合层压板冲击器穿透的灾难性破坏是下一个阶段。在冲击下的铝-碳层压板的实时分析中,识别损伤的产生,传播及其阶段可能会导致这种层压板的发展以及对冲击现象的理解和解释。 (C)2017 Elsevier Ltd.保留所有权利。

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