Fatigue of metallic glasses
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Abstract
The fatigue behaviour of Ni49Fe29P14B6Si2, Ni48Fe29P14B6Al3 and Pd77.5Cu6Si16.5 metallic glasses is examined. In the finite lifetime regime the relationship between stress amplitude (σa), fracture stress (σf), mean stress (σm) and cycles to failure (Nf) isσa=A(σf−σm) (2Nf) b , whereA andb are 16.9 and −0.40 respectively for reduced gauge section Ni49 strips (for σm ≲ 140 kg mm−2) and 27.0 and −0.44 for Pd base wires. These results are unusual in thatA ≫ 1. Consequently, a sharp discontinuity exists nearσa(σf−σm) −1. In a simple tensile test failure occurs at σf(=σy) and 2Nf=1; for peak stresses only a percent or so less thanσf the sample will withstand hundreds of cycles of stress. For uniform cross-section glassy metal filaments, a fatigue limit is observed at stress ratios (σa/σf) in the vicinity of 0.07 to 0.15. The fatigue limit for reduced section specimens is a factor of ∼ 2 higher. Fatigue failure of the Ni-Fe strips may occur under partially or fully plane stress or plane strain conditions, depending on sample thickness and stress. Final failure of the Pd77.5Cu6Si16.5 wires always occurs by general yielding of the remaining section.
Keywords
Fatigue Metallic Glass Fatigue Limit Stress Amplitude Metal FilamentPreview
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