Analysis and optimization of the active rigidity joint

The active rigidity joint is a composite mechanism using shape memory alloy and shape memory polymer to create a passively rigid joint with thermally activated deflection. A new model for the active rigidity joint relaxes constraints of earlier methods and allows for more accurate deflection predictions compared to finite element results. Using an iterative process to determine the strain distribution and deflection, the method demonstrates accurate results for both surface bonded and embedded actuators with and without external loading. Deflection capabilities are explored through simulated annealing heuristic optimization using a variety of cost functions to explore actuator performance. A family of responses presents actuator characteristics in terms of load bearing and deflection capabilities given material and thermal constraints. Optimization greatly expands the available workspace of the active rigidity joint from the initial configuration, demonstrating specific work capabilities comparable to those of muscle tissue.

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

[2]  Justin Manzo,et al.  Methodology for Design of an Active Rigidity Joint , 2009 .

[3]  G. Karst,et al.  Thermomechanical Characterization of Shape Memory Polymers , 2009 .

[4]  Matthew P. Cartmell,et al.  One-dimensional shape memory alloy models for use with reinforced composite structures , 2003 .

[5]  C. Fuller,et al.  Piezoelectric Actuators for Distributed Vibration Excitation of Thin Plates , 1991 .

[6]  Ephrahim Garcia,et al.  Optimal placement and sizing of paired piezoactuators in beams and plates , 1994 .

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

[8]  Scott R. White,et al.  Thermomechanical behavior of 55Ni45Ti nitinol , 1996 .

[9]  Cynthia Breazeal,et al.  Voice coil actuators for human-robot interaction , 2004, 2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) (IEEE Cat. No.04CH37566).

[10]  Hisaaki Tobushi,et al.  Thermomechanical constitutive model of shape memory polymer , 2001 .

[11]  Yann Pasco,et al.  Optimizing the Thickness of Piezoceramic Actuators for Bending Vibration of Planar Structures , 2007 .

[12]  M. Weinberg Working equations for piezoelectric actuators and sensors , 1999 .

[13]  S. J. Kim,et al.  Optimal design of piezoactuators for active noise and vibration control , 1991 .

[14]  C. A. Rogers,et al.  Performance and Optimization of Induced Strain Actuated Structures Under External Loading , 1994 .

[15]  Yinyin Lin,et al.  Study on the tip-deflection of a piezoelectric bimorph cantilever in the static state , 2004 .

[16]  D. Ende,et al.  Non-linear electromechanical behaviour of piezoelectric bimorph actuators: Influence on performance and lifetime , 2009 .

[17]  Craig A. Rogers,et al.  Modeling of Finite-Length Spatially-Distributed Induced Strain Actuators for Laminate Beams and Plates , 1991 .

[18]  Rachel Z. Pytel,et al.  Artificial muscle technology: physical principles and naval prospects , 2004, IEEE Journal of Oceanic Engineering.

[19]  Rick Lind,et al.  Flight Testing and Response Characteristics of a Variable Gull-Wing Morphing Aircraft , 2004 .

[20]  Francis C. Moon,et al.  Laminated piezopolymer plates for torsion and bending sensors and actuators , 1989 .

[21]  Aditi Chattopadhyay,et al.  The development of an optimization procedure for the design of intelligent structures , 1993 .

[22]  Sandro Ridella,et al.  Minimizing multimodal functions of continuous variables with the “simulated annealing” algorithmCorrigenda for this article is available here , 1987, TOMS.

[23]  Ephrahim Garcia,et al.  Design of a shape-memory alloy actuated macro-scale morphing aircraft mechanism , 2005, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[24]  Kenneth B. Lazarus,et al.  Multivariable active lifting surface control using strain actuation : Analytical and experimental results , 1997 .

[25]  E. Crawley,et al.  Use of piezoelectric actuators as elements of intelligent structures , 1987 .

[26]  T. Bailey,et al.  Distributed Piezoelectric-Polymer Active Vibration Control of a Cantilever Beam , 1985 .

[27]  Anna-Maria Rivas McGowan,et al.  Overview of the DARPA/AFRL/NASA Smart Wing program , 1999, Smart Structures.

[28]  Gary H. Koopmann,et al.  Increasing the Mechanical Work Output of an Active Material Using a Nonlinear Motion Transmission Mechanism , 2004 .

[29]  Jan G. Smits,et al.  The constituent equations of piezoelectric bimorphs , 1991 .

[30]  Daniel J. Inman,et al.  A design and analysis of a morphing Hyper-Elliptic Cambered Span (HECS) wing , 2004 .

[31]  William L. Goffe,et al.  SIMANN: FORTRAN module to perform Global Optimization of Statistical Functions with Simulated Annealing , 1992 .

[32]  Yiping Liu,et al.  Thermomechanical recovery couplings of shape memory polymers in flexure , 2003 .