选择性激光熔化制备Ti6Al4V合金拉伸疲劳性能的初步研究

Zhenhui Lu, Sandra Leong Lai San, M. Tan, J. An, Yi Zhang, C. Chua
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摘要

选择性激光熔化(SLM)是一种很有前途的增材制造方法,属于粉末床熔融(PBF)技术的范畴。它具有许多优点,如材料的通用性,效率和打印复杂零件的能力,而无需额外的加工。然而,其表面质量和疲劳性能不如传统的制造方法。与工艺相关的缺陷,如气孔、不完全熔化和未熔化的粉末,会产生应力集中区域,从而导致机械性能低下,如疲劳强度差。本研究旨在研究和优化用SLM法制备Ti6Al4V的打印工艺参数,以减少工艺缺陷,并研究其相对密度、拉伸和疲劳性能。采用SLM280打印30 μm和130 μm厚度的Ti6Al4V试样,并按照ASTM标准进行拉伸和疲劳试验。Ti6Al4V样本的相对密度由30 -µm层厚度是99.97±0.02%的相对密度(n = 8)。Ti6Al4V样本由130 -µm层厚度是99.96±0.02% (n = 8)。平均极限抗拉强度(ut)的标本30 -μm层厚度是1152.8±23.8 MPa (n = 4)。样本的平均生产130 -μm层厚度是1075.5±46.8 MPa (n = 4)。S / n Ti6Al4V样本的疲劳性能曲线打印30 -μm层厚度也获得的。本文讨论了影响slm生产零件拉伸性能的可能因素,如层厚、构建方向和后处理。利用光学显微镜、激光扫描显微镜和扫描电镜对裂纹扩展和表面质量进行了观察。这项研究的结果将有助于改进slm打印的Ti6Al4V零件,这可以潜在地应用于航空航天工业,在航空航天工业中,疲劳强度对确保安全至关重要。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Preliminary investigation on tensile and fatigue properties of Ti6Al4V manufactured by selected laser melting
Selective laser melting (SLM) is a promising additive manufacturing method that falls under the category of powder bed fusion (PBF) technology. It has many advantages such as material versatility, efficiency, and the ability to print complex parts without additional machining. However, its surface quality and fatigue properties have been found to be inferior to traditional manufacturing methods. Process-related defects such as pores, incomplete fusion, and un-melted powders give rise to areas of stress concentrations, which lead to mechanical inferiority such as poor fatigue strength. This study aims to investigate and optimize the printing process parameters for Ti6Al4V fabricated by SLM to reduce process-related defects and to investigate their relative density, tensile, and fatigue properties. Ti6Al4V specimens were printed in both 30- and 130-μm layer thicknesses using SLM280 and subjected to tensile and fatigue testing according to ASTM standards. The relative density of Ti6Al4V samples built by 30-µm layer thickness is 99.97 ± 0.02 % (n = 8). The relative density of Ti6Al4V samples built by 130-µm layer thickness is 99.96 ± 0.02 % (n = 8). The average ultimate tensile strength (UTS) of specimens with 30-μm layer thickness is 1152.8 ± 23.8 MPa (n = 4). The average UTS of specimens with 130-μm layer thickness is 1075.5 ± 46.8 MPa (n = 4). S/N curve of the fatigue performance of Ti6Al4V samples printed by 30-μm layer thickness was also obtained. Possible factors impacting the tensile property of SLM-produced parts, such as layer thickness, build orientation, and post-process, are discussed in this paper. Furthermore, crack propagation and surface quality were observed using optical microscopes, laser scanning microscopes, and scanning electron microscopes. The findings of this study will contribute to the improvement of SLM-printed Ti6Al4V parts, which can be potentially applied in the aerospace industry, where fatigue strength is critical to ensuring safety.
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