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Experimental investigation and FEA simulation of drilling of Inconel 718 alloy

机译:实验研究和FEA模拟钻孔718合金钻孔

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摘要

Drilling of Inconel alloy structures is widely used for aerospace components. Inconel 718, a high strength, thermal resistant Nickel-based alloy, is mainly used in the aircraft industries. Due to the extreme toughness and work hardening characteristics of the alloy, the problem of machining Inconel 718 is one of the ever-increasing magnitudes. This paper discusses the drilling cutting conditions on the machinability of Inconel 718. In this work, an empirical modelling is proposed for predicting the cutting force exerted during the drilling of alloy. The full factorial design is constructed based on the significant drilling process parameters. The cutting force is measured using the dynamometer. The experiments are conducted on high speed radial drilling machine at a constant depth of cut. Using the experimental results the empirical model is developed for prediction of cutting force and verification results are compared with DEFORM 3D simulation software. The validation experiments are well correlated with empirical model and simulation results for prediction cutting force. However the proposed simulation model further to be considering chatter and vibration of the machine tool structure and different drilling tool geomentry.
机译:Inconel合金结构的钻孔广泛用于航空航天部件。 Inconel 718,高强度,热阻镍基合金主要用于飞机行业。由于合金的极端韧性和工作化特性,加工Inconel 718的问题是不断增加的大小。本文讨论了钻井切割条件,即第718号的可加工性。在这项工作中,提出了一种实证建模,以预测在合金钻井期间施加的切割力。完整的因子设计基于显着的钻探过程参数构建。使用测功机测量切割力。实验在高速径向钻孔机上以恒定的切割深度进行。使用实验结果,经验模型开发用于预测切削力,并将验证结果与变形3D仿真软件进行比较。验证实验与预测切割力的经验模型和仿真结果良好。然而,所提出的仿真模型进一步考虑了机床结构和不同钻孔工具的颤动和振动。

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