Actuator lifetime predictions for Ni60Ti40 shape memory alloy plate actuators

Shape memory alloys (SMAs), due to their ability to repeatedly recover substantial deformations under applied mechanical loading, have the potential to impact the aerospace, automotive, biomedical, and energy industries as weight and volume saving replacements for conventional actuators. While numerous applications of SMA actuators have been flight tested and can be found in industrial applications, these actuators are generally limited to non-critical components, are not widely implemented and frequently one-off designs, and are generally overdesigned due to a lack of understanding of the effect of the loading path on the fatigue life and the lack of an accurate method of predicting actuator lifetimes. Previous efforts have been effective at predicting actuator lifetimes for isobaric dogbone test specimens. This study builds on previous work and investigates the actuation fatigue response of plate actuators with various stress concentrations through the use of digital image correlation and finite element simulations.

[1]  Dimitris C. Lagoudas,et al.  Characterization and Modeling of Thermo-Mechanical Fatigue in Equiatomic NiTi Actuators , 2014 .

[2]  Shuichi Miyazaki,et al.  Fatigue life of Ti–50 at.% Ni and Ti–40Ni–10Cu (at.%) shape memory alloy wires , 1999 .

[3]  Dimitris C. Lagoudas,et al.  Actuation fatigue life prediction of shape memory alloys under the constant-stress loading condition , 2015 .

[4]  In Lee,et al.  Shape Adaptive Airfoil Actuated by a Shape Memory Alloy and its Aerodynamic Characteristics , 2009 .

[5]  G. Scirè Mammano,et al.  Effects of Loading and Constraining Conditions on the Thermomechanical Fatigue Life of NiTi Shape Memory Wires , 2014, Journal of Materials Engineering and Performance.

[6]  James G. Boyd,et al.  Design of a Reconfigurable SMA-Based Solar Array Deployment Mechanism , 2015 .

[7]  Hisaaki Tobushi,et al.  Cyclic deformation and fatigue of a TiNi shape-memory alloy wire subjected to rotating bending , 1998 .

[8]  Darren J. Hartl,et al.  Three-dimensional constitutive model considering transformation-induced damage and resulting fatigue failure in shape memory alloys , 2014, Smart Structures.

[9]  James H. Mabe,et al.  Boeing's Variable Geometry Chevron, Morphing Aerostructure for Jet Noise Reduction , 2006 .

[10]  James H. Mabe,et al.  NiTinol performance characterization and rotary actuator design , 2004, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[11]  D. Lagoudas Shape memory alloys : modeling and engineering applications , 2008 .

[12]  Ken Gall,et al.  Cyclic deformation mechanisms in precipitated NiTi shape memory alloys , 2002 .

[13]  Dimitris C. Lagoudas,et al.  Advanced methods for the analysis, design, and optimization of SMA-based aerostructures , 2011 .

[14]  John Parthenios,et al.  Transformation fatigue and stress relaxation of shape memory alloy wires , 2007 .

[15]  Dimitris C. Lagoudas,et al.  Aerospace applications of shape memory alloys , 2007 .

[16]  E. Dragoni,et al.  Functional fatigue of NiTi Shape Memory wires for a range of end loadings and constraints , 2012 .

[17]  K. Ramaiah,et al.  Understanding the Fatigue Behaviour of NiTiCu Shape Memory Alloy Wire Thermal Actuators , 2008 .

[18]  John Yen,et al.  Design and Implementation of a Shape Memory Alloy Actuated Reconfigurable Airfoil , 2003 .

[19]  J. S. Cory,et al.  NiTi fatigue behavior , 1981 .

[20]  K. V. Van Vliet,et al.  Predicting in vivo failure of pseudoelastic NiTi devices under low cycle, high amplitude fatigue. , 2005, Journal of biomedical materials research. Part B, Applied biomaterials.

[21]  Dimitris C. Lagoudas,et al.  Effect of Processing and Loading on Equiatomic NiTi Fatigue Life and Localized Failure Mechanisms , 2013 .