Non-proportional multiaxial transformation ratchetting of super-elastic NiTi shape memory alloy: Experimental observations
Introduction
NiTi shape memory alloy has been widely used in aerospace, mechanical, electronic and medical fields due to its unique shape memory and super-elastic effects. Often, the structural components and devices made by the NiTi shape memory alloy are subjected to a cyclic thermo-mechanical loading. Therefore, its cyclic deformation is a key issue which should be investigated before the fatigue life and reliability of such components and devices can be discussed reasonably. In the last two decades, many experiments had been performed to investigate the cyclic thermo-mechanical responses of NiTi shape memory alloys, as done by Gall et al., 2001, Sehitoglu et al., 2001a, Sehitoglu et al., 2001b, De la Flor et al., 2009, Zhang et al., 2008, Dayananda and Rao, 2008, Liu et al., 1999, Eggeler et al., 2004, and so on. The experimental results showed that: (1) a progressive accumulation of residual strain was resulted from the cyclic transformation (i.e., thermo-elastic martensite transformation and its reverse), and the accumulation rate of the residual strain tended to zero after certain cycles; (2) the transformation stresses and dissipation energy decreased with the increasing number of cycles; (3) the cyclic deformation will degrade the super-elasticity, shape memory effect and high dissipation energy and then cause a function failure of NiTi shape memory alloy. However, the experimental observations were mostly performed under the strain-controlled cyclic loading conditions.
It is well-known that the stress-controlled cyclic loading is a common loading condition the structural components are subjected to, too. In the stress-controlled cyclic tension-unloading tests done by Strnadel et al., 1995a, Strnadel et al., 1995b, Sehitoglu et al., 2001a, Sehitoglu et al., 2001b, Sehitoglu et al., 2006, Nasser and Guo, 2006, Predki et al., 2006, Wang et al., 2010, Saleeb et al., 2013, it was concluded that the responding peak strain and the residual strain (at zero stress point) of super-elastic NiTi shape memory alloy increased but the dissipation energy decreased remarkably during the cyclic loading. After certain cycles, a stable cyclic stress–strain response was reached. More recently, Kang et al. (2009) observed the cyclic deformation of super-elastic NiTi shape memory alloy in more details by the stress-controlled cyclic tension-unloading, tension–tension and tension–compression tests with different stress levels. They introduced the cyclic accumulation of peak and valley strains observed in the stress-controlled cyclic tests as a new term, “transformation ratchetting”, since it was mainly caused by the cyclic transformation between austenite and martensite phases. Kang et al. (2012) also discussed the interaction of transformation ratchetting and fatigue failure by performing the tests till the failure of specimens occurred. However, only the uniaxial transformation ratchetting of super-elastic NiTi shape memory was investigated by Kang et al., 2009, Kang et al., 2012, and no multiaxial transformation ratchetting has been discussed yet. It is necessary to observe the cyclic stress–strain responses of super-elastic NiTi shape memory alloy under the multiaxial stress-controlled cyclic loading conditions.
Therefore, in this work, some non-proportional multiaxial stress-controlled cyclic tests are performed to investigate the multiaxial transformation ratchetting of super-elastic NiTi shape memory alloy by comparing with the corresponding uniaxial ones. Different stress levels and multiaxial loading paths are employed in the tests in order to discuss the effects of stress level and loading path on the multiaxial transformation ratchetting. Also, the effect of peak stress hold on the multiaxial transformation ratchetting is addressed.
Section snippets
Experimental procedures
Super-elastic NiTi shape memory alloy micro-tubes (Ni, 55.9% at mass, from Jiangyin Materials Development Co. Ltd., China) are used in the cyclic tests. The austenite transformation finish temperature Af is 290 K, which is lower than the test temperature of 298 K. The original phase of the alloy is then austenite. The cylindrical specimens with an outer diameter of 2.01 mm and inner diameter of 1.68 mm are cut from the as-received micro-tubes, and their ratios of wall thickness to radius are 1:5,
Responses in uniaxial cyclic tension and cyclic pure torsion tests
Since most cyclic tension–torsion tests are performed by setting an asymmetrical stress-controlled cyclic loading in axial direction (with non-zero mean axial stress) and symmetrical one in torsional direction (with zero mean shear stress), the responses of the NiTi shape memory alloy are first observed by uniaxial cyclic tension tests with various mean stresses and stress amplitudes, and a symmetrical cyclic pure torsion test with an equivalent shear stress () amplitude of 500 MPa. In the
Discussion
From the experimental observations stated in Section 3.2.1, it is concluded that the multiaxial transformation ratchetting of super-elastic NiTi shape memory alloy is much higher than the corresponding uniaxial one (as shown in Figs. 8(c) and (d), and 11(b)). The reason why the multiaxial transformation ratchetting is much higher than the corresponding uniaxial one can be interpreted as follows:
(1) During the multiaxial cyclic loading, the directions of principle stresses will vary continuously
Conclusions
- 1.
The forward transformation starting stress (from austenite to martensite phase) of the super-elastic NiTi shape memory alloy is about 400 MPa in the axial tension, which is higher than that obtained in the monotonic pure torsion (i.e., equivalent shear stress of about 300 MPa), but the transformation hardening in the axial tension is weaker than that in the pure torsion.
- 2.
The transformation ratchetting also occurs in the multiaxial stress-controlled cyclic tests, and mainly in the direction of
Acknowledgments
Financial supports by the National Natural Science Foundation of China (11025210; 11202171) and Science Foundation for The Excellent Youth Scholars of Ministry of Education of China (2012018420012) are gratefully acknowledged. D. Song appreciates the China Scholarship Council for its support to her research stay at the Chair of Structural Mechanics, Department of Civil Engineering, Germany, from September 2012 to September 2013.
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