Laser peening is an emerging technology for the surface treatment of metallic materials that is capable of enhancing resistance to fatigue failure. This paper describes some recent results from joint research programs conducted to generate data on residual stress and fatigue performance of laser peened materials. Specifically, we present data for residual stress imparted by laser peening and fatigue life improvement of laser peened coupons relative to as-machined coupons. These data are presented for a range of high-strength materials employed in aircraft and other demanding applications: BSTOA Ti-6A14V titanium alloy, 300M steel, MP35N Ni-Co-Cr-Mo alloy, and 7050-T7451 aluminum alloy. For each material, residual stress distributions were measured for treatment with different laser peening parameter sets. For particular laser peening parameter sets, stress versus life data were generated for as-machined and laser peened fatigue coupons, which quantifies fatigue life improvement attained by laser peening over a range of applied loads.
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ASME 2005 Pressure Vessels and Piping Conference
July 17–21, 2005
Denver, Colorado, USA
Conference Sponsors:
- Pressure Vessels and Piping Division
ISBN:
0-7918-4192-8
PROCEEDINGS PAPER
Fatigue Performance of Laser Peened Materials
Michael R. Hill,
Michael R. Hill
University of California at Davis, Davis, CA
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Theresa E. Pistochini,
Theresa E. Pistochini
University of California at Davis, Davis, CA
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Adrian T. DeWald
Adrian T. DeWald
University of California at Davis, Davis, CA
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Michael R. Hill
University of California at Davis, Davis, CA
Theresa E. Pistochini
University of California at Davis, Davis, CA
Adrian T. DeWald
University of California at Davis, Davis, CA
Paper No:
PVP2005-71793, pp. 203-207; 5 pages
Published Online:
July 29, 2008
Citation
Hill, MR, Pistochini, TE, & DeWald, AT. "Fatigue Performance of Laser Peened Materials." Proceedings of the ASME 2005 Pressure Vessels and Piping Conference. Volume 7: Operations, Applications, and Components. Denver, Colorado, USA. July 17–21, 2005. pp. 203-207. ASME. https://doi.org/10.1115/PVP2005-71793
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