4.7 Article

Benchmark of a probabilistic fatigue software based on machined and as-built components manufactured in AlSi10Mg by L-PBF

期刊

INTERNATIONAL JOURNAL OF FATIGUE
卷 165, 期 -, 页码 -

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.ijfatigue.2022.107171

关键词

Additive manufacturing; Fatigue; Defects; As-built surface; Failure probability; Residual stresses

资金

  1. European Space Agency [4000120221-17-NL-LvH, ESA-TRP-TECMSP-SOW-009494, 4000133245/20/NL/AR/idb]

向作者/读者索取更多资源

The metal additive manufacturing (AM) technology offers the possibility of obtaining optimized components with reduced weight in the space and aero-nautic industries. However, this manufacturing technique often leads to internal defects, poor surface quality, and process-induced residual stresses, which greatly affect the fatigue performance and reproducibility of AMed parts. A probabilistic finite element post-processor called ProFACE was developed to assess the fatigue strength and critical locations of complex components with process-induced defects. It has been successfully used to predict the fatigue life of AlSi10Mg components and explore the variability of significant parameters affecting the fatigue strength.
The possibility to obtain optimized components with a reduced weight is the main driver of space and aero-nautic industries in seriously considering the metal additive manufacturing (AM) technology for production. Despite the incontrovertible advantages offered by this manufacturing technique, the material produced is usually affected by the presence of internal defects, a poor surface quality, and process-induced residual stresses. These features strongly affect the fatigue performance and reproducibility of AMed parts, limiting the adoption of deterministic criteria for fatigue assessment. A probabilistic approach is therefore needed for the analysis of critical and structural components. To this aim, a fully probabilistic finite element (FE) post -processor, ProFACE, was developed by part of the authors to assess the fatigue strength and critical locations of complex components in the presence of process-induced defects. A wide benchmark activity was supported by the European Space Agency (ESA) to test the software capabilities for the life prediction of components manufactured in AlSi10Mg by L-PBF. After tuning ProFACE parameters based on the results obtained on standard fatigue specimens, the software was used to estimate the fatigue life of the components obtaining a good description of the experimental dataset for both volumetric and surface defects. The software was then used to explore the effect of the variability of the most significant parameters affecting fatigue strength of AlSi10Mg AMed components.

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