Thermo-mechanical simulation of annealing heat treatment of Ni-based GH4099 superalloy made by laser powder bed fusion

Laser powder bed fusion (LPBF) additive manufacturing (AM) unavoidably generates residual stresses due to sharp thermal gradients and the strong mechanical constraints of the substrate. These stresses can lead to large warpages and cracking of AM builds, compromising their qualification. Annealing h...

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Detalhes bibliográficos
Autores: Lu, Xufei|||0000-0002-5829-385X, Chen, Chaoyue, Zhang, Guohao, Chiumenti, Michele|||0000-0002-6286-7393, Cervera Ruiz, Miguel|||0000-0003-3437-6703, Yin, Haoliang, Ma, Liang, Lin, Xin
Tipo de documento: artigo
Data de publicação:2023
País:España
Recursos:Universitat Politècnica de Catalunya (UPC)
Repositório:UPCommons. Portal del coneixement obert de la UPC
Idioma:inglês
OAI Identifier:oai:upcommons.upc.edu:2117/398928
Acesso em linha:https://hdl.handle.net/2117/398928
https://dx.doi.org/10.1016/j.addma.2023.103703
Access Level:Acceso aberto
Palavra-chave:Manufacturing processes
Laser powder bed fusion
Residual stresses relaxation
Annealing heat treatment
Part warpages
Ni-based superalloy
Finite element simulation
Fabricació
Àrees temàtiques de la UPC::Enginyeria dels materials::Metal·lúrgia
Descrição
Resumo:Laser powder bed fusion (LPBF) additive manufacturing (AM) unavoidably generates residual stresses due to sharp thermal gradients and the strong mechanical constraints of the substrate. These stresses can lead to large warpages and cracking of AM builds, compromising their qualification. Annealing heat treatment (HT) after LPBF fabrication is an efficient solution for residual stress relaxation, allowing for the development of visco-strains above the annealing temperature. Thereby, this work is focused on the thermo-mechanical simulation of the post-HT of Ni-based GH4099 superalloy components fabricated by LPBF. To this end, several bridge structures are manufactured by LPBF, and various annealing HT conditions are analyzed. After cutting from the substrate, the warpage of all the AM-parts is measured using a 3D-scanner. The in-house software package for the numerical simulation of both the AM and the HT processes first is calibrated by matching the experimental measurements. Next, the numerical tool is used to investigate the effect of different annealing conditions (e.g. varying temperature and dwell time) on the relaxation of the residual stresses and warpage. A roadmap to select the optimal annealing parameters is established considering the actual size of the AM-components.