A B S T R A C T In some high-strength steels, a fatigue crack tends to occur at the interior inclusion after a long-term sequence of the cyclic loadings at low stress levels, although the crack takes place at the surface in the usual life region at high stress levels. Thus, we have the duplex S-N curves consisting of the respective S-N curves for usual life region and very highcycle regime. It is well known that a significant fracture surface having the fine granular morphology is formed around the interior inclusion at the crack initiation site. This surface area is sometimes called as 'fine granular area'. In this work, metallurgical structures around the interior inclusion at the fatigue crack initiation site were carefully observed by combining several special techniques such as focused ion beam technique and highresolution scanning electronic microscopes. Based on the current observation results, it was found that the microstructure around the interior inclusion was changed into the penny-shape fine granular layer from the usual martensitic structure during long-term cyclic loadings. Then, debondings along with the boundaries of the matrix and the fine granular layer have produced the small cracks inside the metallic material, and these interior cracks caused the final fatigue fracture after definite loading cycles of the crack propagation.Keywords bearing steel; fine acicular area (FAA); fine granular area (FGA); interior crack initiation; rotating bending; very high-cycle fatigue.
N O M E N C L A T U R Eα = stress concentration factor D = distance from definite section ΔK th = threshold value of stress intensity factor range in crack propagation N = number of cycles N f = number of cycles to failure R = stress ratio (minimum stress/maximum stress) σ = stress σ a = stress amplitude σ B = tensile strength σ w = fatigue limit
I N T R O D U C T I O NAs a common understanding in the Metal Fatigue, it is well known that ferrous metals such as structural steels reveal the clear fatigue limit at the number of stress cycles less than 10 7 cycles. 1 However, non-ferrous metals such as aluminium alloys have no fatigue limit such that the S-N curve tends to decrease continuously in the very long life region, longer than 10 7 cycles. Usually, the fatigue limit for the structural steels is proportional to the tensile strength, and we have σ w = σ B /2, approximately, in the wide variety of the strength levels. 2,3 In recent years, practical structures such as railway wheels and axles, offshore structures, energy conversion and transportation systems have been used in a long term, sometimes, beyond their original design life