Effects of Fatigue on the Integrity of a Friction Stir Welded Lap Joint Containing Residual Stresses

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Abstract:

This research uses a non-destructive method of neutron diffraction to measure the tri-axial residual stresses in a friction stir welded aerospace fuselage component: a stringer-to-skin lap joint. Two different specimens were examined. Fatigue testing was performed on both specimens to determine their fatigue lives. Effects of the different components of residual stresses were examines and related to fatigue performance. A combination of fractography, hardness testing, and residual stress measurement was used to predict areas of high probability of structural failure in the friction stir welded lap joints.

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[1] M. Ericsson, L.Z. Jin, R. Sandtrom, Fatigue properties of friction stir overlap welds, International Journal of Fatigue 68 (2005) 456-468.

DOI: 10.1016/j.ijfatigue.2006.02.052

Google Scholar

[2] A. Merati, M. Gallant, Friction stir lap welding of AA7075-T6 stringers on AA2024-T3 skin, (2009).

Google Scholar

[3] M. Jung, The Fatigue Characteristics of Friction Stir Welded Stiffened Panel Structure, Masters Thesis, (2007).

DOI: 10.22215/etd/2007-07731

Google Scholar

[4] O. Hatamleh, The Effects of Laser Peening and Shot Peening on Mechanical Properties in Friction Stir Welded 7075-T7351 Aluminum, ASM International 17 (2007) 688-694.

DOI: 10.1007/s11665-007-9163-7

Google Scholar

[5] P. Staron, M. Kocak, S. Williams, Residual stresses in friction stir welded Al sheets, Applied Physics A Materials Science & Processing 74 (2002) 1161-1165.

DOI: 10.1007/s003390201830

Google Scholar

[6] C.D. Dalle, Effect of Weld Imperfections and Residual Stresses on the Fatigue Crack Propagation in Friction Stir Welded Joints, Second International Conference on Friction Stir Welding Proceedings (2000) 2-10.

DOI: 10.1080/09507110801990686

Google Scholar