This paper examines the effects of laser peening on Alloy 22 (UNS N06022), which is the proposed material for use as the outer layer on the spent-fuel nuclear waste canisters to be stored at Yucca Mountain. Stress corrosion cracking (SCC) is a primary concern in the design of these canisters because tensile residual stresses will be left behind by the closure weld. Alloy 22 is a nickel-based material that is particularly resistant to corrosion; however, there is a chance that stress corrosion cracking could develop given the right environmental conditions. Laser peening is an emerging surface treatment technology that has been identified as an effective tool for mitigating tensile redisual stresses in the storage canisters. The results of laser-peening experiments on Alloy 22 base material and a sample 33 mm thick double-V groove butt-weld made with gas tungsten arc welding (GTAW) are presented. Residual stress profiles were measured in Alloy 22 base material using the slitting method (also known as the crack-compliance method), and a full 2D map of longitudinal residual stress was measured in the sample welds using the contour method. Laser peening was found to produce compressive residual stress to a depth of 3.8 mm in 20 mm thick base material coupons. The depth of compressive residual stress was found to have a significant dependence on the number of peening layers and a slight dependence on the level of irradiance. Additionally, laser peening produced compressive residual stresses to a depth of 4.3 mm in the 33 mm thick weld at the center of the weld bead where high levels of tensile stress were initially present.
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October 2004
Research Papers
Assessment of Tensile Residual Stress Mitigation in Alloy 22 Welds Due to Laser Peening Available to Purchase
Adrian T. DeWald,
Adrian T. DeWald
Department of Mechanical and Aeronautical Engineering, University of California, One Shields Avenue, Davis, CA 95616
Laser Science and Technology, Lawrence Livermore National Laboratory, PO Box 808, Livermore, CA 94550
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Jon E. Rankin,
Jon E. Rankin
Laser Science and Technology, Lawrence Livermore National Laboratory, PO Box 808, Livermore, CA 94550
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Michael R. Hill,
e-mail: address: mrhill@ucdavis.edu
Michael R. Hill
Department of Mechanical and Aeronautical Engineering, University of California, One Shields Avenue, Davis, CA 95616
**
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Matthew J. Lee,
Matthew J. Lee
Department of Mechanical and Aeronautical Engineering, University of California, One Shields Avenue, Davis, CA 95616
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Hao-Lin Chen
Hao-Lin Chen
Laser Science and Technology, Lawrence Livermore National Laboratory, PO Box 808, Livermore, CA 94550
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Adrian T. DeWald
Department of Mechanical and Aeronautical Engineering, University of California, One Shields Avenue, Davis, CA 95616
Laser Science and Technology, Lawrence Livermore National Laboratory, PO Box 808, Livermore, CA 94550
Jon E. Rankin
Laser Science and Technology, Lawrence Livermore National Laboratory, PO Box 808, Livermore, CA 94550
Michael R. Hill
**
Department of Mechanical and Aeronautical Engineering, University of California, One Shields Avenue, Davis, CA 95616
e-mail: address: mrhill@ucdavis.edu
Matthew J. Lee
Department of Mechanical and Aeronautical Engineering, University of California, One Shields Avenue, Davis, CA 95616
Hao-Lin Chen
Laser Science and Technology, Lawrence Livermore National Laboratory, PO Box 808, Livermore, CA 94550
Contributed by the Materials Division for publication in the JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY. Manuscript received by the Materials Division July 21, 2003; revision received February 26, 2004. Associate Editor: S. Mall.
J. Eng. Mater. Technol. Oct 2004, 126(4): 465-473 (9 pages)
Published Online: November 9, 2004
Article history
Received:
July 21, 2003
Revised:
February 26, 2004
Online:
November 9, 2004
Citation
DeWald, A. T., Rankin, J. E., Hill, M. R., Lee, M. J., and Chen, H. (November 9, 2004). "Assessment of Tensile Residual Stress Mitigation in Alloy 22 Welds Due to Laser Peening ." ASME. J. Eng. Mater. Technol. October 2004; 126(4): 465–473. https://doi.org/10.1115/1.1789957
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