Evaluation of Residual Stresses Introduced by Laser Shock Peening in Steel using Different Measurement Techniques

Evaluation of Residual Stresses Introduced by Laser Shock Peening in Steel using Different Measurement Techniques

D. Glaser, M. Newby, C. Polese, L. Berthe, A.M. Venter, D. Marais, J.P. Nobre, G. Styger, S. Paddea, S.N. van Staden

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The development of a residual stress engineering technology such as laser shock peening (LSP) requires evaluation of the process by quantification of the desired effect. Applications of LSP for turbine blade integrity enhancement due to expected deeper compressive residual stresses with lower surface roughness compared to conventional shot peening (SP), have resulted in the analysis of LSP on 12CrNiMoV steel samples. The investigation compares different residual stress measurement techniques such as energy dispersive synchrotron X-ray diffraction (SXRD), laboratory X-ray diffraction (XRD) with sequential electro-polishing, neutron diffraction (ND), incremental-hole drilling (IHD), and the contour method (CM). This study highlights the benefits and opportunities of using complimentary residual stress measurement techniques in order to gain insight into the residual stresses within a material.

Keywords
Laser Shock Peening, Residual Stress, Synchrotron Diffraction, Incremental-Hole Drilling, Neutron Diffraction, Contour Stress Measurement

Published online 4/20/2018, 6 pages
Copyright © 2018 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA

Citation: D. Glaser, M. Newby, C. Polese, L. Berthe, A.M. Venter, D. Marais, J.P. Nobre, G. Styger, S. Paddea, S.N. van Staden, ‘Evaluation of Residual Stresses Introduced by Laser Shock Peening in Steel using Different Measurement Techniques’, Materials Research Proceedings, Vol. 4, pp 45-50, 2018

DOI: http://dx.doi.org/10.21741/9781945291678-7

The article was published as article 7 of the book

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] K. Ding and L. Ye, Laser shock peening performance and simulation, Woodhead Publishing Limited, Cambridge, England, 2006. https://doi.org/10.1201/9781439823620
[2] M.N. James, M. Newby, D.G. Hattingh and A. Steuwer, Shot-peening of steam turbine blades: residual stresses and their modification by fatigue cycling, Procedia Engineering 2.1 (2010) 441-451. https://doi.org/10.1016/j.proeng.2010.03.048
[3] M.G. Moore and W. P. Evans, Mathematical correction for stress in removed layers in X- ray diffraction residual stress analysis. No. 580035. SAE Technical Paper, 1958.
[4] P.V. Grant, J.D. Lord and P.S. Whitehead, The Measurement of Residual Stresses by the Incremental Hole Drilling Technique. NPL Materials Centre. Measurement Good Practice. Guide, (53).
[5] M. Newby, D. Glaser and C. Polese, Laser Shock Peening Process Development for Turbine Blade Refurbishment Applications Using a Commercial “Mid-Range” Energy Laser”, 6th ICLPRP, Nov 2016, Skukuza, SA.
[6] M. T. Hutchings, P. J. Withers, T. M. Holden and T. Lorentzen, Introduction to the characterization of residual stress by neutron diffraction, CRC press, 2005.