超声冲击后处理slm制造Ti-6Al-4V的静态断裂行为

M. Burkov, A. Eremin, A. Byakov, S. Panin
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引用次数: 1

摘要

本文研究了超声波冲击法制备Ti-6Al-4V合金的工艺。SLM毛坯沿建筑方向切割,并进行超声冲击表面处理。通过数字图像相关技术(DIC)对处理后的试样进行单轴拉伸试验和原位应变监测,同时通过扫描电子显微镜(SEM)对断口进行研究。通过对实验数据的分析,揭示了后期处理对力学性能和变形特性的影响。对断口表面的扫描电镜图像的分析使我们能够区分处理过和未处理过的试样的结构对破坏模式的影响之间的差异。本文研究了超声波冲击法制备Ti-6Al-4V合金的工艺。SLM毛坯沿建筑方向切割,并进行超声冲击表面处理。通过数字图像相关技术(DIC)对处理后的试样进行单轴拉伸试验和原位应变监测,同时通过扫描电子显微镜(SEM)对断口进行研究。通过对实验数据的分析,揭示了后期处理对力学性能和变形特性的影响。对断口表面的扫描电镜图像的分析使我们能够区分处理过和未处理过的试样的结构对破坏模式的影响之间的差异。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Static fracture behavior of ultrasonic impact post-built treated SLM-manufactured Ti-6Al-4V
The paper deals with the investigation of ultrasonic impact post-build treatment of SLM-manufactured Ti-6Al-4V. SLM blanks were cut along building direction and subjected to ultrasonic impact surface treatment. Post-build treated specimens were tested by uniaxial tensile testing with in situ strain monitoring via digital image correlation technique (DIC), while the fracture surfaces were studied by scanning electron microscopy (SEM). The analysis of the experimental data allowed revealing the effect of post-build treatment on mechanical properties and on the peculiarities of deformation behavior. Analysis of SEM images of fracture surfaces allowed us to distinguish the differences between structure influence onto failure pattern both for the treated and non-treated specimens.The paper deals with the investigation of ultrasonic impact post-build treatment of SLM-manufactured Ti-6Al-4V. SLM blanks were cut along building direction and subjected to ultrasonic impact surface treatment. Post-build treated specimens were tested by uniaxial tensile testing with in situ strain monitoring via digital image correlation technique (DIC), while the fracture surfaces were studied by scanning electron microscopy (SEM). The analysis of the experimental data allowed revealing the effect of post-build treatment on mechanical properties and on the peculiarities of deformation behavior. Analysis of SEM images of fracture surfaces allowed us to distinguish the differences between structure influence onto failure pattern both for the treated and non-treated specimens.
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