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Residual Stress in Metal Parts Produced by Powder-Bed Additive Manufacturing Processes

机译:粉末床增材制造工艺产生的金属零件中的残余应力

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In this study, residual stresses from the electron beam additive manufacturing (EBAM) and selective laser melting (SLM) processes, due to repeated thermal cycles, were investigated. Residual stresses play a crucial role in part performance, and thus, it is critical to evaluate the process-induced residual stresses in AM parts. Ti-6Al-4V and Inconel 718 parts produced by EBAM and SLM, respectively, were studied in residual stresses using the methodology established by Carlsson et al., a mechanical instrumented indentation technique, which is based on the experimental correlation between the indentation characteristic and the residual stress. The results show that the Ti-6Al-4V EBAM parts have a compressive residual stress in both Z-plane and X-plane, while the Inconel 718 SLM parts show a tensile stress and a compressive stress in the Z-plane and X-plane, respectively. Besides, the Ti-6Al-4V parts have lower absolute value of residual stress than the Inconel 718 parts. Moreover, the Vickers hardness values of the parts built using SLM and EBAM are comparable to the literature data.
机译:在这项研究中,研究了由于重复的热循环而产生的电子束增材制造(EBAM)和选择性激光熔化(SLM)工艺产生的残余应力。残余应力在零件性能中起着至关重要的作用,因此,评估工艺引起的AM零件中的残余应力至关重要。使用机械压痕技术Carlsson等人建立的方法,研究了EBAM和SLM分别生产的Ti-6Al-4V和Inconel 718零件在残余应力下的残余应力,该方法基于压痕特性与压痕之间的实验相关性。残余应力。结果表明,Ti-6Al-4V EBAM零件在Z面和X面均具有压缩残余应力,而Inconel 718 SLM零件在Z面和X面均具有拉伸应力和压缩应力。 , 分别。此外,Ti-6Al-4V零件的残余应力绝对值比Inconel 718零件低。此外,使用SLM和EBAM制造的零件的维氏硬度值与文献数据相当。

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