Abstract
This paper presents results from a numerical and experimental investigation motivated by the need to explore the effectiveness of residual stress relief techniques in aluminium alloy engineering components of complex geometry. Quenching is part of the heat treatment to establish mechanical properties. It can create high levels of residual stress in an engineering component. Finite element analysis (FEA) was used to predict the residual stresses generated by quenching and the location of peak residual stresses corresponding to probable in service failure sites. The residual strains and stresses were characterised using neutron diffraction techniques in components with high and low quench stresses to validate a FEA study, and also to appraise the evolution of a commercial stress relief method. An excellent correlation existed between the simulations and measurements.
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Acknowledgements
For this work, we are grateful for the use of the experimental facilities at SINQ, Paul Scherrer Institute. This research project has been supported by the European Commission under the 6th Framework Programme through the Key Action: Strengthening the European Research Area, Research Infrastructures. Contract number: RII3-CT-2003-505925.
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This research has been supported by the European Commission under the 6th Framework Programme through the Key Action: Strengthening the European Research Area, Research Infrastructures. Contract number: RII3-CT-2003-505925.
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By comparing numerical prediction with experimentally measured stresses by neutron diffraction technique, the finite element analysis (FEA) study was validated, and the effectiveness of stress relief technique explored. FEA predicted the residual stress generated by quenching and the location of peak residual stresses corresponding to probable failure sites.
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Hossain, S., Stuhr, U., Robinson, J.S. et al. Validating quench stresses in complex aluminium components. Int J Adv Manuf Technol 113, 3555–3567 (2021). https://doi.org/10.1007/s00170-021-06831-y
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DOI: https://doi.org/10.1007/s00170-021-06831-y