DOI QR코드

DOI QR Code

Effects of Re-Peening on the Compressive Residual Stress and Fatigue Life of Al7075-T6

Al7075-T6의 압축잔류응력 및 피로 수명에 미치는 재피닝의 효과

  • Oh, Sung-Hun (Dept. of Mechanical Engineering, Graduate School of Seoul National University of Science and Technology) ;
  • Lee, Yong-Sung (Center for Energy System Research, Seoul National University of Science and Technology) ;
  • Cheong, Seong-Kyun (Dept. of Mechanical and Automotive Engineering, Seoul National University of Science and Technology)
  • Received : 2016.04.06
  • Accepted : 2016.07.06
  • Published : 2016.08.15

Abstract

The effects of re-peening on the compressive residual stress and fatigue life of Al7075-T6 were investigated. The compressive residual stress induced on the surface of components by shot peening is known to increase the fatigue life. However, the fatigue load relaxes the compressive residual stress of components. Re-peening is a technique to again induce the relaxed compressive residual stress and increase the total fatigue life of components. In this study, the re-peening process was applied to fatigue-loaded specimens. The compressive residual stress and fatigue life were examined for re-peened specimens with fatigue ratios of 30%, 50%, and 70%. The results showed that the compressive residual stress of the specimens was relaxed under the fatigue load. The re-peening process significantly increases the compressive residual stress and total fatigue life.

Keywords

References

  1. Kobayashi, M., Matsui, T., 1998, Mechanism of Creation of Compressive Residual Stress by Shot Peening, International Journal of Fatigue, 20:5 351-357. https://doi.org/10.1016/S0142-1123(98)00002-4
  2. Webster, G. A., Ezeilo, A. N., 2001, Residual Stress Distributions and Their Influence on Fatigue Lifetimes, International Journal of Fatigue, 23:1 375-383.
  3. Bergstrom J., Ericsson T., 1984, Relaxation of Shot Peening Induced Compressive Stress During Fatigue of Notched Steel Samples, Proc. of the 2nd International Conference on Shot Peening, 241-248.
  4. Eckersley J. S., 1989, Shot Peening Plays a Vital Roll in rejuvenation of Aging Aircraft, Shot Peening Theory and Application, Institute for Industrial Technology Transfer International, 241-255 France.
  5. Hammond, D. W., Meguid, S. A., 1990, Crack Propagation in the Presence of Shot-peening Residual Stress, Engineering Fracture Mechanics, 37:2 373-387. https://doi.org/10.1016/0013-7944(90)90048-L
  6. ASTM International 2015, Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials, ASTM E 466, USA.
  7. Kim, T. H., Cheong, S. K., Shin, Y. S., 2002, A Study on the Fatigue of Al7075-T6 by Shot Peening, Korea Society of Manufacturing Technology Engineers, Autumn Conference Proceedings, 335-340.
  8. Kim, J. C., Cheong, S. K., Noguchi, H., 2013, Evolution of Residual Stress Redistribution Associated with Localized Surface Microcracking in Shot-peened Medium-Carbon Steel During Fatigue Test, International Journal of Fatigue, 55 147-157. https://doi.org/10.1016/j.ijfatigue.2013.06.010
  9. Wi, J. H., 2008, A Study on the Improvement of Fatigue Characteristics of Al7075 alloy by Re-peening, A Thesis for a Master, Hanyang University, Republic of Korea.
  10. Kang, J. S., 2002, Fatigue Characteristics of Re-peened SM45C Steel, Korea Society of Mechanical Engineering, Spring Conference Proceedings, 208-213.