Through-Thickness Residual Stress Distribution After the Cold Expansion of Fastener Holes and Its Effect on Fracturing

Author:

O¨zdemir A. Tamer1,Edwards Lyndon2

Affiliation:

1. Materials Division, Department of Metallurgy, Faculty of Technical Education, Gazi University, Ankara, Turkey

2. Department of Materials Engineering, Faculty of Technology, Open University, Milton Keynes MK7 6AA, UK

Abstract

Many analytical and experimental techniques utilize two-dimensional analysis approach to determine residual strains and stresses at cold expanded holes. In the present work, a recently developed technique of hole drilling was used to sketch stress patterns in three-dimension at a particular orientation of split-sleeve cold expanded holes. At this orientation, similarities were obtained in between the present results and the stress distributions measured by Fourier series expansion, neutron diffraction methods and prediction of a recent finite element analysis. It is clear that after cold expansion there are significant variations in residual hoop stresses at different sections through the thickness of the plate. However, finish reaming and de-burring around the hole redistributes residual stresses such that hoop stresses adjacent to the hole along its entire length becomes more compressive and almost uniform. Finally a correlation between stress pattern and crack profile, displaying the through-thickness effect was shown.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference47 articles.

1. Mann, J. L., and Jost, G. S., 1983, “Stress Fields Associated With Fitted and Cold Expanded Holes,” Metal Forum, 6, pp. 43–53.

2. Schwarmann, L. , 1982, “On Improving Fatigue Performance of a Double Shear Lap Joint,” Int. J. Fatigue, 2, pp. 105–111.

3. Champoux, R. L., 1986, “An Overview of Cold Expansion Methods,” Fatigue Prevention and Design, J. T. Barnby, ed., Camelot Press, London, Chap. 1.

4. Lowak, H., 1981, “Zum Einfluss von Bauteilgro¨sse, Lastfolge und Last Horizon auf die Schwingfestigskeit-Steigerung Durch Mechanisch Erzeugte Eigenspannungen,” Bericht Nr. FB-157, Fraunhofer-Institut fu¨r Betriebsfestigkeit, Darmstadt.

5. Ozelton, M. W., and Coyle, T. G., 1986, “Fatigue Life Improvement by Cold Working Fastener Holes in 7050 Aluminum,” Fatigue in Mechanically Fastener Composites and Metallic Joints, ASTM STP 927, John M. Potter, ed., pp. 53–71.

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