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Finite element modeling for the cutting process of the titanium alloy Ti10V2Fe3Al

机译:钛合金Ti10V2Fe3Al切削过程的有限元建模

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By producing of critical components in the aerospace industry is widely used the β-titanium alloy Ti10V2Fe3Al (Ti-1023) due to its extremely high ratio of strength to density, its great resistance to fatigue, its excellent resistance to corrosion and fracture toughness. This material is characterized by significant difficulties in machining. Substantial assistance in the study of the titanium alloy Ti-1023 machinability can provide a simulation of machining by numerical modeling. This paper presents the results regarding the creation of the FEM models for the cutting processes of the titanium alloy Ti-1023. The created FEM cutting models were constantly verified with experimental tests of the kinetic machining characteristics and analyses of the chip morphology by orthogonal and oblique cutting as well as flat end milling with different depths of immersion. A Johnson-Cook model was used as material model of the workpiece and the damage mechanism of the workpiece is reproduced with the Cocroft and Latham model. The parameters of material and fracture model were determined by DOE study. Comparing the experimentally established and the simulated kinetic machining characteristics and chip morphology confirms that the created FEM models are of a good quality. The size of error for simulating the chip dimensions does not exceed 10% and ranges between 10 and 30% for simulating the resultant forces.
机译:通过生产航空航天业中的关键部件,β-钛合金Ti10V2Fe3Al(Ti-1023)由于具有极高的强度与密度比,出色的耐疲劳性,出色的耐腐蚀性和断裂韧性而被广泛使用。这种材料的特点是加工困难。钛合金Ti-1023可切削性研究的大量帮助可以通过数值建模来模拟加工。本文介绍了有关为Ti-1023钛合金切割过程创建FEM模型的结果。所创建的FEM切削模型通过动力学加工特性的实验测试不断进行验证,并通过正交和倾斜切削以及不同浸入深度的平端铣削对切屑形态进行了分析。使用Johnson-Cook模型作为工件的材料模型,并使用Cocroft和Latham模型再现了工件的损坏机理。通过DOE研究确定材料和断裂模型的参数。比较实验建立的和模拟的动力学加工特性以及切屑形态,可以确认所创建的FEM模型具有良好的质量。用于模拟切屑尺寸的误差大小不超过10%,并且在用于模拟合力的范围内介于10%和30%之间。

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