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Finite Element Analysis of Drilling of Carbon Fibre Reinforced Composites

机译:碳纤维增强复合材料钻削的有限元分析

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摘要

Despite the increased applications of the composite materials in aerospace due to their exceptional physical and mechanical properties, the machining of composites remains a challenge. Fibre reinforced laminated composites are prone to different damages during machining process such as delamination, fibre pull-out, microcracks, thermal damages. Optimization of the drilling process parameters can reduces the probability of these damages. In the current research, a 3D finite element (FE) model is developed of the process of drilling in the carbon fibre reinforced composite (CFC). The FE model is used to investigate the effects of cutting speed and feed rate on thrust force, torque and delamination in the drilling of carbon fiber reinforced laminated composite. A mesoscale FE model taking into account of the different oriented plies and interfaces has been proposed to predict different damage modes in the plies and delamination. For validation purposes, experimental drilling tests have been performed and compared to the results of the finite element analysis. Using Matlab a digital image analysis code has been developed to assess the delamination factor produced in CFC as a result of drilling.
机译:尽管由于其优异的物理和机械性能,复合材料在航空航天中的应用有所增加,但是复合材料的机加工仍然是一个挑战。纤维增强的层压复合材料在加工过程中容易受到不同的损坏,例如分层,纤维拉出,微裂纹,热损伤。钻孔工艺参数的优化可以减少这些损坏的可能性。在当前的研究中,开发了碳纤维增强复合材料(CFC)钻孔过程的3D有限元(FE)模型。有限元模型用于研究切削速度和进给速度对碳纤维增强层压复合材料钻削中推力,扭矩和分层的影响。已经提出了考虑到不同定向层和界面的中尺度有限元模型来预测层和分层中的不同损伤模式。为了进行验证,已进行了实验性钻孔测试,并将其与有限元分析的结果进行了比较。使用Matlab,已经开发了数字图像分析代码,以评估由于钻探而在CFC中产生的分层因子。

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