Fatigue Apparatus for Geometrically Complex Non-Standardized Specimens
Marcelino P. Nascimento and Herman J.C. Voorwald
Affiliation: Department of Materials and Technology, State University of Sao Paulo-UNESP/FEG, 333, Ariberto Pereira da Cunha Ave., CEP 12500-000, Guaratingueta City, Sao Paulo State, Brazil.
Standard Test Methods (e.g. ASTM, DIN) for materials characterization in general, and for fatigue in particular, do not contemplate specimens with complex geometries, as well as the combination of axial and in-plane bending loads in their methodologies. The present study refers to some patents and the new configuration or configurations of specimens (non-standardized by the “status quo” of test methods) and a device developed to induce axial and bending combined forces resultants from axial loads applied by any one test equipment (dynamic or monotonic) which possesses such limitation, towards obtaining more realistic results on the fatigue behavior, or even basic mechanical properties, from geometrically complex structures. Motivated by a specific and geometrically complex aeronautic structure (“motor-cradle”), non-standardized welded tubular specimens made from AISI 4130 steel were fatigue-tested at room temperature, by using a constant amplitude sinusoidal load of 20 Hz frequency, load ratio R = 0.1 with and without the above referred auxiliary fatigue apparatus. The results showed the fatigue apparatus was efficient for introducing higher stress concentration factor at the welded specimen joints, consequently reducing the fatigue strength when compared to other conditions. From the obtained results it is possible to infer that with small modifications the proposed apparatus will be capable to test a great variety of specimen configurations such as: squared tubes and plates with welded or melted junctions, as well as other materials such as aluminum, titanium, composites, polymeric, plastics, etc.
Keywords: Fatigue apparatus, non-standardized specimens, welded tubular specimens, hot-spot stress concentration factor, combined in-plane bending moment and axial loadings
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