Kabir Mohammad Rizviul, Richter Henning
German Aerospace Center, Institute of Materials Research, Linder Höhe, 51147 Köln, Germany.
Materials (Basel). 2017 Feb 8;10(2):145. doi: 10.3390/ma10020145.
A selective laser melting (SLM)-based, additively-manufactured Ti-6Al-4V alloy is prone to the accumulation of undesirable defects during layer-by-layer material build-up. Defects in the form of complex-shaped pores are one of the critical issues that need to be considered during the processing of this alloy. Depending on the process parameters, pores with concave or convex boundaries may occur. To exploit the full potential of additively-manufactured Ti-6Al-4V, the interdependency between the process parameters, pore morphology, and resultant mechanical properties, needs to be understood. By incorporating morphological details into numerical models for micromechanical analyses, an in-depth understanding of how these pores interact with the Ti-6Al-4V microstructure can be gained. However, available models for pore analysis lack a realistic description of both the Ti-6Al-4V grain microstructure, and the pore geometry. To overcome this, we propose a comprehensive approach for modeling and discretizing pores with complex geometry, situated in a polycrystalline microstructure. In this approach, the polycrystalline microstructure is modeled by means of Voronoi tessellations, and the complex pore geometry is approximated by strategically combining overlapping spheres of varied sizes. The proposed approach provides an elegant way to model the microstructure of SLM-processed Ti-6Al-4V containing pores or crack-like voids, and makes it possible to investigate the relationship between process parameters, pore morphology, and resultant mechanical properties in a finite-element-based simulation framework.
基于选择性激光熔化(SLM)增材制造的Ti-6Al-4V合金在逐层堆积材料的过程中容易积累不良缺陷。复杂形状气孔形式的缺陷是该合金加工过程中需要考虑的关键问题之一。根据工艺参数的不同,可能会出现边界为凹形或凸形的气孔。为了充分发挥增材制造Ti-6Al-4V的潜力,需要了解工艺参数、气孔形态和最终力学性能之间的相互依存关系。通过将形态细节纳入微观力学分析的数值模型,可以深入了解这些气孔如何与Ti-6Al-4V微观结构相互作用。然而,现有的气孔分析模型缺乏对Ti-6Al-4V晶粒微观结构和气孔几何形状的真实描述。为了克服这一问题,我们提出了一种综合方法,用于对位于多晶微观结构中的具有复杂几何形状的气孔进行建模和离散化。在这种方法中,多晶微观结构通过Voronoi镶嵌进行建模,复杂的气孔几何形状通过策略性地组合不同大小的重叠球体来近似。所提出的方法为对含有气孔或裂纹状空隙的SLM加工Ti-6Al-4V的微观结构进行建模提供了一种巧妙的方式,并使得在基于有限元的模拟框架中研究工艺参数、气孔形态和最终力学性能之间的关系成为可能。