S Rangaraj, S S I Ahmed, A Davis, P J Withers, A Gholinia
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引用次数: 0
摘要
通过增材制造(AM)生产的合金具有很大的优势,特别是在控制材料利用率和精确控制加工参数方面,从而实现了材料性能的微调。然而,AM 材料的晶粒结构通常比较复杂,受到凝固动力学、加工参数、热梯度和残余应力等因素的影响。疲劳分析表明,由于夹杂缺陷,AM 材料的分布相当不均匀,这限制了其作为结构部件的应用。本研究分析了选择性激光熔化(SLM)AlSi10Mg 合金的疲劳失效样品,样品的水平方向和垂直于构建方向,以了解裂纹的传播路径。在这里,我们使用 X 射线计算机断层扫描 (CT) 来检查内部孔隙率,并辅以电子反向散射衍射 (EBSD) 测绘,发现疲劳裂纹正是从内部孔隙率开始的。这使我们认识到复杂的晶粒微结构在控制疲劳裂纹扩展方面的关键作用。
Understanding fatigue crack propagation pathways in Additively Manufactured AlSi10Mg
Alloys produced through additive manufacturing (AM) offer substantial advantages, particularly in controlling material utilisation and precisely manipulating processing parameters, resulting in finely tuned material properties. However, the grain structure of AM material is typically complex, influenced by factors such as solidification dynamics, processing parameters, thermal gradients, and residual stress. Fatigue analysis shows considerable scatter due to entrained defects which limits their use as structural components. In this study, fatigue-failed samples from selective laser melted (SLM) AlSi10Mg alloy, oriented horizontal and vertical to the build direction were analysed to understand crack propagation paths. Here X-ray Computed Tomography (CT) was used to examine internal porosity from which fatigue cracks initiate, complemented by electron backscattered diffraction (EBSD) mapping. This enabled us to recognize the crucial role of the complex grain microstructure in controlling fatigue crack propagation.