Data-driven surrogate modelling of residual stresses in Laser Powder-Bed Fusion

Abstract

ABSTRACTIn order to enable the industrialization of additive manufacturing, it is necessary to develop process simulation models that can rapidly predict part quality. Although multi-physics simulations have shown success at predicting residual stress, distortion, microstructure and mechanical properties of additively manufactured parts, they are generally too computationally expensive to be directly used in applications, such as optimization, controls, or digital twinning. In this study, a critical evaluation is made of how data-driven surrogate models can be used to model the residual stress of parts fabricated by Laser Powder-Bed Fusion. Residual stress data is generated by using an inherent-strain based process simulation for two families of part geometries. Three different models using varying levels of sophistication are compared: a multilayer perceptron (MLP), a convolutional neural network (CNN) based on the U-Net architecture, and an interpolation-based method based on mapping geometries onto a reference. All three methods were found to be sufficient for part design, providing mechanical predictions for a CPU time below 0.2 s, representing a runtime speed-up of at least 3900 × . Neural network-based models are significantly more expensive to train compared to using interpolation. However, the generality of models based on the U-Net architecture is attractive for applications in optimization.KEYWORDS: Laser Powder Bed Fusionadditive manufacturinggeometry parametrizationsurrogate modelsradial basis functionsneural network AcknowledgementsThe authors would like to thank Nagarajan Raghavan for useful discussions.Disclosure statementNo potential conflict of interest was reported by the author(s).Data availability statementThe data that support the findings of this study are openly available in the Mendeley data repository at http://dx.doi.org/10.17632/kkmzjr3wv7.1Additional informationFundingFinancial support was provided by the Science and Engineering Research Council, A*STAR, Singapore (Grant no. A19E1a0097).