Evolution of Microstructure and Residual Stress in Hot Rolled Ti-6Al-4V Plates Subjected to Different Heat Treatment Conditions

Evolution of Microstructure and Residual Stress in Hot Rolled Ti-6Al-4V Plates Subjected to Different Heat Treatment Conditions

W. Rae, S. Rahimi

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Abstract. Hot rolled Ti-6Al-4V plate samples were taken from three different stages of an industrial heat treatment process; one as-rolled and two heat treated. This was followed by microstructure characterization using optical microscopy. Surface and through-thickness residual stress was determined using a combination of X-ray diffraction (XRD) and the contour method. Measured residual stress distributions showed similarities in distribution with that obtained for rolled Al-7050 alloy; including compressive troughs near the outer thickness on both sides, leading towards a tensile zone around the center with a local minima at the plate center thickness. Microstructure and residual stress data was then used to draw comparisons between the investigated conditions.

Keywords
Contour Method, X-Ray Diffraction, Titanium Alloy, Phase Transformation

Published online 9/11/2018, 6 pages
Copyright © 2018 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA

Citation: W. Rae, S. Rahimi, ‘Evolution of Microstructure and Residual Stress in Hot Rolled Ti-6Al-4V Plates Subjected to Different Heat Treatment Conditions’, Materials Research Proceedings, Vol. 6, pp 171-176, 2018

DOI: http://dx.doi.org/10.21741/9781945291890-27

The article was published as article 27 of the book Residual Stresses 2018

Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.

References
[1] M. G. Glavicic, D. U. Furrer, and G. Shen, “A Rolls-Royce Corporation industrial perspective of titanium process modelling and optimization: current capabilities and future needs,” J. Strain Anal. Eng., vol. 45, no. 5, 2010, pp. 329-335. https://doi.org/10.1243/03093247JSA577
[2] E. Alabort, P. Kontis, D. Barba, K. Dragnevski, and R. C. Reed, “On the mechanisms of superplasticity in Ti–6Al–4V,” Acta Mater., vol. 105, 2016, pp. 449-463. https://doi.org/10.1016/j.actamat.2015.12.003
[3] Rae, W., Lomas, Z., Jackson, M., & Rahimi, S., “Measurements of residual stress and microstructural evolution in electron beam welded Ti-6Al-4V using multiple techniques,” Mat. Char., vol. 132, 2017, pp. 10-19. https://doi.org/10.1016/j.matchar.2017.07.042
[4] Prime, M.B. and Hill, M.R., “Residual stress, stress relief, and inhomogeneity in aluminum plate”. Scripta Materialia, 2002, vol. 46, no. 1, pp.77-82. https://doi.org/10.1016/S1359-6462(01)01201-5
[5] Stefansson, N., and S. L. Semiatin. “Mechanisms of globularization of Ti-6Al-4V during static heat treatment,” Metall. Mat. Trans. A, 2003, vol. 34, no.3, pp. 691-698. https://doi.org/10.1007/s11661-003-0103-3
[6] Babu, B., & Lindgren, L. E., “Dislocation density based model for plastic deformation and globularization of Ti-6Al-4V”. Int. J. Plasticity, 2013, 50, pp. 94-108. https://doi.org/10.1016/j.ijplas.2013.04.003