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Finite-element analysis of residual stresses in the TС4 titanium alloy treated by laser shock peening

Authors

  • Oleg Anatol’yevich Plekhov Institute of Continuous Media Mechanics UB RAS
  • Anastasiya Andreyevna Kostina Institute of Continuous Media Mechanics UB RAS
  • Roman Igorevich Iziumov Institute of Continuous Media Mechanics UB RAS
  • Anastasiya Yur’yevna Iziumova Institute of Continuous Media Mechanics UB RAS

DOI:

https://doi.org/10.7242/1999-6691/2022.15.2.13

Keywords:

laser shock peening, residual stresses, finite-element simulation

Abstract

Laser shock peening is an effective tool for generating deep compressive residual stresses (more than 1 mm) near the surface of metallic structures. This can improve their mechanical properties and fatigue performance. For this purpose, it is necessary to find optimal laser shock parameters. In this paper, the effect of laser intensity and peening pattern on the residual stress field in a Ti-6Al-4V titanium alloy is investigated through numerical simulations. The applied approach includes two steps. In the first stage, the modeling of elasto-plastic stress waves is performed. The second stage involves a solution of static equilibrium problem for residual stress distribution taking into account plastic deformation fields. The analysis was carried out for a square plate with a thickness of 3 mm, the central part of which is subjected to a series of square laser pulses. The pulse length was the same for all considered cases, and it was equal to 3 mm. The results of the analysis demonstrate that, when the laser pulse power density increases, the maximum value of compressive stress increases as well, and tensile stresses occur on the opposite side of the sample. The application of the two-sided laser peening (no overlap) or one-sided peening (50% overlap) can eliminate this effect. An increase in the maximum compressive stress is observed on both sides of the specimen in these cases. Due to an increase in the number of layers in the case of the one-sided peening (no overlap), the maximum compressive stress and penetration depth become greater. However, tensile stresses in the volume of the sample also increase.

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Supporting Agencies
Статья подготовлена в рамках Программы создания и развития научного центра мирового уровня «Сверхзвук» на 2020–2025 годы при финансовой поддержке Министерства образования и науки Российской Федерации (соглашение № 075-15-2020-925 от 16 ноября 2020).

Author Biographies

  • Oleg Anatol’yevich Plekhov, Institute of Continuous Media Mechanics UB RAS

    дфмн, зам. директора по науке

  • Anastasiya Andreyevna Kostina, Institute of Continuous Media Mechanics UB RAS

    кфмн, нс

  • Roman Igorevich Iziumov, Institute of Continuous Media Mechanics UB RAS

    мнс

  • Anastasiya Yur’yevna Iziumova, Institute of Continuous Media Mechanics UB RAS

    кфмн, мнс

References

Braisted W., Brockman R. Finite element simulation of laser shock peening. Int. J. Fatig., 1999, vol. 21, pp. 719-724. https://doi.org/10.1016/S0142-1123(99)00035-3

Peyre P., Berthe L., Vignal V., Popa I., Baudin T. Analysis of laser shock waves and resulting surface deformations in an Al-Cu-Li aluminum alloy. J. Phys. D: Appl. Phys., 2012, vol. 45, 335304. https://doi.org/10.1088/0022-3727/45/33/335304

Ding K. Three-dimensional dynamic finite element analysis of multiple laser shock peening processes. Surf. Eng., 2003, vol. 19, pp. 351-358. https://doi.org/10.1179/026708403225007563

Peyre P., Sollier A., Chaieb I., Berthe L., Bartnicki E., Braham C., Fabbro R. FEM simulation of residual stresses induced by laser Peening. Eur. Phys. J. AP, 2003, vol. 23, pp. 83-88. https://doi.org/10.1051/epjap:2003037

Warren A.W., Guo Y.B., Chen S.C. Massive parallel laser shock peening: Simulation, analysis, and validation. Int. J. Fatig., 2008, vol. 30, pp. 188-197. https://doi.org/10.1016/j.ijfatigue.2007.01.033

Sticchi M., Staron P., Sano Y., Meixer M., Klaus M., Rebelo-Kornmeier J., Huber N., Kashaev N. A parametric study of laser spot size and coverage on the laser shock peening induced residual stress in thin aluminium samples. J. Eng., 2015, vol. 2015, pp. 97-105. https://doi.org/10.1049/joe.2015.0106

Spradlin T.J., Grandhi R.V., Langer K. Experimental validation of simulated fatigue life estimates in laser-peened aluminum. International Journal of Materials and Structural Integrity, 2011, vol. 2, pp. 74-86. https://doi.org/10.1108/17579861111108635

Keller S., Chupakhin S., Staron P., Maawad E., Kashaev N., Klusemann B. Experimental and numerical investigation of residual stresses in laser shock peened AA2198. J. Mater. Process. Tech., 2018, vol. 255, pp. 294-307. https://doi.org/10.1016/j.jmatprotec.2017.11.023

Peyre P., Chaieb I., Braham C. FEM calculation of residual stresses induced by laser shock processing in stainless steels. Modell. Simul. Mater. Sci. Eng., 2007, vol. 15, pp. 205-221. https://doi.org/10.1088/0965-0393/15/3/002

Langer K., Spradlin T.J., Fitzpatrick M.E. Finite element analysis of laser peening of thin aluminum structures. Metals, 2020, vol. 10, 93. https://doi.org/10.3390/met10010093

Hfaiedh N., Peyre P., Song H., Popa I., Ji V., Vignal V. Finite element analysis of laser shock peening of 2050-T8 aluminum alloy. Int. J. Fatig., 2015, vol. 70, pp. 480-489. https://doi.org/10.1016/j.ijfatigue.2014.05.015

Sun R.J., Zhu Y., Guo W. Effect of laser shock processing on surface morphology and residual stress field of TC17 titanium alloy by FEM method. J. Plast. Eng., 2017, vol. 24, pp. 187-193.

Li X., He W., Luo S., Nie X., Tian L., Feng X., Li R. Simulation and experimental study on residual stress distribution in titanium alloy treated by laser shock peening with flat-top and Gaussian laser beams. Materials, 2019, vol. 12, 1343. https://doi.org/10.3390/ma12081343

Zhang X., Li H., Duan S., Yu X., Feng J., Wang B., Huang Z. Modeling of residual stress field induced in Ti–6Al–4V alloy plate by two sided laser shock processing. Surf. Coating Tech., 2015, vol. 280, pp. 163-173. https://doi.org/10.1016/j.surfcoat.2015.09.004

Kumar G.R., Rajyalakshmi G. FE simulation for stress distribution and surface deformation in Ti-6Al-4V induced by interaction of multi scale laser shock peening parameters. Optik, 2020, vol. 206, 164280. https://doi.org/10.1016/j.ijleo.2020.164280

Wang С., Li K., Hu X., Yang H., Zhou Y. Numerical study on laser shock peening of TC4 titanium alloy based on the plate and blade model. Opt. Laser Tech., 2021, vol. 142, 107163. https://doi.org/10.1016/j.optlastec.2021.107163

Xu G., Luo K.Y., Dai F.Z., Lu J.Z. Effects of scanning path and overlapping rate on residual stress of 316L stainless steel blade subjected to massive laser shock peening treatment with square spots. Appl. Surf. Sci., 2019, vol. 481, pp. 1053-1063. https://doi.org/10.1016/j.apsusc.2019.03.093

Hu Y., Gong C., Yao Z., Hu J. Investigation on the non-homogeneity of residual stress field induced by laser shock peening. Surf. Coating Tech., 2009, vol. 203, pp. 3503-3508. https://doi.org/10.1016/j.surfcoat.2009.04.029

Keller S., Horstmann M., Kashaev N., Klusemann B. Experimentally validated multi-step simulation strategy to predict the fatigue crack propagation rate in the residual stress field after shock peening. Int. J. Fatig., 2019, vol. 124, pp. 265-276. https://doi.org/10.1016/j.ijfatigue.2018.12.014

Amarchinta H. Uncertainty quantification of residual stresses induced by laser peening simulation. PhD Dissertation in Engineering. Dayton: Wright State University, 2010. 201 p.

Kim R., Suh J., Shin D., Lee K.-H., Bae S.-H., Cho D.-W., Yi W.-G. FE Analysis of laser shock peening on STS304 and the effect of static damping on the solution. Metals, 2021, vol. 11, 1516. https://doi.org/10.3390/met11101516

Johnson G.R., Cook W.H. Proc. of the 7th International Symposium on Ballistics. Hague, The Netherlands, April 19-21, 1983. Pp. 541-547.

Zerilli F.J., Armstrong R.W. Dislocation-mechanics-based constitutive relations for material dynamics calculations. J. Appl. Phys., 1987, vol. 61, pp. 1816-1825. https://doi.org/10.1063/1.338024

Khan A.S., Suh Y.S., Kazmi R. Quasi-static and dynamic loading responses and constitutive modeling of titanium alloys. Int. J. Plast., 2004, vol. 20, pp. 2233-2248. https://doi.org/10.1016/j.ijplas.2003.06.005

Kuzkin V.A., Mikhaluk D.S. Application of numerical simulation for identification of Johnson-Cook material model parameters for aluminum under high-speed loading. Vychisl. mekh. splosh. sred – Computational Continuum Mechanics, 2010, vol. 3, no. 1, pp. 32-43. https://doi.org/10.7242/1999-6691/2010.3.1.4

Hu Y., Yao Z. Numerical simulation and experimentation of overlapping laser shock processing with symmetry cell. Int. J. Mach. Tools Manuf., 2008, vol. 48, pp. 152-162. https://doi.org/10.1016/j.ijmachtools.2007.08.021

Zhao J., Dong Y., Ye C. Laser shock peening induced residual stresses and the effect on crack propagation behavior. Int. J. Fatig., 2017, vol. 100, pp. 407-417. http://dx.doi.org/10.1016/j.ijfatigue.2017.04.002

Fabbro R., Fournier J., Ballard P., Devaux D., Virmont J. Physical study of laser-produced plasma in confined geometry. J. Appl. Phys., 1990, vol. 68, pp. 775-784. https://doi.org/10.1063/1.346783

Pozdnyakov V., Keller S., Kashaev N., Klusemann B., Oberrath J. Сoupled modeling approach for laser shock peening of AA2198-T3: From plasma and shock wave simulation to residual stress prediction. Metals, 2022, vol. 12, 107. https://doi.org/10.3390/met12010107

Nam T. Finite element analysis of residual stress field induced by laser shock peening. PhD Dissertation in Mechanical Engineering. Columbus: Ohio State University, 2002. 187 p.

Published

2022-07-26

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How to Cite

Plekhov, O. A., Kostina, A. A., Iziumov, R. I., & Iziumova, A. Y. (2022). Finite-element analysis of residual stresses in the TС4 titanium alloy treated by laser shock peening. Computational Continuum Mechanics, 15(2), 171-184. https://doi.org/10.7242/1999-6691/2022.15.2.13