激光增材制造γ-TiAl合金疲劳使用系数建模与仿真

S. Raji, A. Popoola, S. Pityana, O. Popoola, N. Arthur, M. Tlotleng
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引用次数: 0

摘要

近年来,激光增材制造(LAM)技术越来越多地应用于航空航天、汽车和能源行业生产具有优异物理和机械性能的部件。本工作旨在模拟经LAM加工的γ-TiAl合金的疲劳使用系数。利用COMSOL Multiphysics 5.4软件对y-TiAl合金微观组织进行建模和仿真。这是建模来产生材料性能(密度,恒压下的热容量和导热系数)从一个单位电池的微观结构作为合金的一般代表。利用计算得到的性能对γ-TiAl合金零件的LAM加工过程进行了建模,并进行了疲劳模拟,确定了使用系数(Ke)。模型结果表明,LAM的最大Von Mises应力和瞬态温度分别为2.88 x108 Nm-2和1510 K;疲劳利用系数模型的最大Von Mises应力为2.91 x108 Nm-2,疲劳利用系数为0.35。
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Modelling and simulation of the fatigue usage factor of γ-TiAl alloy fabricated through Laser Additive Manufacturing (LAM)
Recently, laser additive manufacturing (LAM) technologies are increasingly being applied for producing components with excellent physical and mechanical properties in the aerospace, automotive and energy industries. This work is aimed at modelling the fatigue usage factor of γ-TiAl alloy fabricated through LAM. The modelling and simulation were performed using the COMSOL Multiphysics 5.4 software by developing a y-TiAl alloy microstructure. This was modelled to generate the material properties (density, heat capacity at constant pressure and thermal conductivity) from the microstructure of a unit cell as a general representation of the alloy. The computed properties were used in modelling the LAM process to fabricate γ-TiAl alloy part with subsequent fatigue simulation to determine the usage factor (Ke). From the models, the maximum Von Mises stress and transient temperature were 2.88 x108 Nm-2 and 1510 K respectively, for the LAM fabrication process; while the fatigue usage factor model showed a maximum Von Mises stress of 2.91 x108 Nm-2 and a fatigue usage factor of 0.35.
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