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A computational reduction model for appraising structural effects in selective laser melting manufacturing: A methodical model reduction proposed for time-efficient finite element analysis of larger components in Selective Laser Melting

机译:用于评估选择性激光熔化制造中的结构效果的计算简化模型:为选择性激光熔化中大型零件的高效时效有限元分析提出的方法化模型简化

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摘要

Selective Laser Melting (SLM) of metallic powders, especially of high-strength nickel based alloys, allows for the manufacturing of components of high shape complexity and load capacity. However, due to high temperature gradients, induced during laser processing, the structural properties and geometrical accuracy of components can be affected. This paper aims to analyse different modelling approaches of the thermo-mechanical effects in SLM manufacturing of aero-engine components, in order to determine in advance possible shape distortions. Hereby, a methodical model reduction is proposed and evaluated to allow the finite element analysis of larger components with reasonable computational time. Major process characteristics such as heat input, molten region geometry (i.e. macrographs), material deposition (i.e. layer thickness), temperature dependent material and powder properties, phase transformation, process sequences and convection effects are taken into consideration. The proposed model reduction aims to decrease time consuming modelling effort and high computation duration and yet provide reliable structural results.
机译:金属粉末,特别是高强度镍基合金的选择性激光熔化(SLM),允许制造形状复杂度和负载能力高的组件。但是,由于在激光加工过程中引起的高温梯度,可能会影响组件的结构特性和几何精度。本文旨在分析航空发动机部件SLM制造中热机械效应的不同建模方法,以便提前确定可能的形状变形。因此,提出了一种有条理的模型简化方法,并进行了评估,以允许使用合理的计算时间对较大部件进行有限元分析。考虑了主要的工艺特征,例如热量输入,熔融区域的几何形状(即宏观图),材料沉积(即层厚度),与温度有关的材料和粉末性质,相变,工艺顺序和对流效应。提出的模型简化旨在减少耗时的建模工作和高计算持续时间,同时提供可靠的结构结果。

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