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Fatigue performance of superelastic NiTi near stress-induced martensitic transformation

[Display omitted] •Fatigue of NiTi drops to 104 cycles before reaching martensitic transformation.•Early crack nucleation and fast crack growth occurs in NiTi even at low strains.•R-phase improves the low cycle fatigue of NiTi as it acts as a stress reliever.•Martensitic transformation is triggered...

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Published in:International journal of fatigue 2017-02, Vol.95, p.76-89
Main Authors: Alarcon, Eduardo, Heller, Luděk, Chirani, Shabnam Arbab, Šittner, Petr, Kopeček, Jaromír, Saint-Sulpice, Luc, Calloch, Sylvain
Format: Article
Language:English
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Summary:[Display omitted] •Fatigue of NiTi drops to 104 cycles before reaching martensitic transformation.•Early crack nucleation and fast crack growth occurs in NiTi even at low strains.•R-phase improves the low cycle fatigue of NiTi as it acts as a stress reliever.•Martensitic transformation is triggered at the crack advancing in superelastic NiTi.•Transformation strains provide additional driving force for crack opening. The structural fatigue of superelastic NiTi was studied with special attention paid to the drop in fatigue performance commonly observed at the onset of the stress-induced martensitic transformation. We processed the superelastic NiTi wires into an hourglass shape as a result of which the stress induced martensitic transformation in tension is not localized as confirmed by digital image correlation measurements. The hourglass shaped samples were subjected to force controlled pull-pull fatigue tests at two distinct temperatures selected to investigate the fatigue of NiTi with and without the R-phase transformation involved, and to capture the effect of varying critical stress for the onset of B19′ martensitic transformation. Resulting fatigue curves expressed in terms of both the stress and the strain show a first degradation of fatigue performance at stresses more than 200MPa below the onset of the martensitic transformation. Furthermore, fatigue curves showed a temperature dependence which was successfully implemented into a modified Basquin’s power law model. Notably, the fatigue life drops down to 104 cycles before the nominal loadings reach the B19′ transformation regime. We further found that fatigue life is shorter for the B2-R-phase transformation regime than for the elasticity of the parent B2 austenite phase at low stresses when strains remain below 1%, however at higher strains the B2-R-phase transforming wire is better than the elastic one. Fatigue crack observations revealed crack initiation at the surface and its propagation towards the bulk resulting in a reduction of the cross-section and substantial increase in normal stresses. Martensitic transformation was triggered during the crack growth in samples nominally loaded in elastic or R-phase transformation regimes as confirmed by in-situ infrared thermography. As the crack grows with increasing speed, the activity of transformation processes at the tip gradually increases till unstable crack growth and final rupture occurs, as confirmed by in-situ thermography and stress hysteres
ISSN:0142-1123
1879-3452
DOI:10.1016/j.ijfatigue.2016.10.005