ABSTRACT Title of dissertation: SELF–CONTAINED HYBRID ELECTRO- HYDRAULIC ACTUATORS USING MAGNETOSTRICTIVE AND ELECTROSTRICTIVE MATERIALS Anirban Chaudhuri, Doctor of Philosophy, 2008 Dissertation directed by: Professor Norman M. Wereley Department of Aerospace Engineering Hybrid electro-hydraulic actuators using smart materials along with flow rec- tification have been widely reported in recent years. The basic operation of these actuators involves high frequency bidirectional operation of an active material that is converted into unidirectional fluid motion by a set of valves. While theoretically attractive, practical constraints limit the efficacy of the solid-fluid hybrid actuation approach. In particular, inertial loads, fluid viscosity and compressibility combine with loss mechanisms inherent in the active material to limit the effective bandwidth of the driving actuator and the total output power. A hybrid actuator was developed by using magnetostrictive TerFeNOL-D as the active driving element and hydraulic oil as the working fluid. Tests, both with and without an external load, were carried out to measure the unidirectional performance of the actuator at different pumping frequencies and operating conditions. The maximum no-load output velocity was 84 mm/s with a 51 mm long rod and 88 mm/s with a 102 mm long rod, both noted around325Hzpumpingfrequency, whiletheblockedforcewascloseto89N.Dynamic tests were performed to analyze the axial vibration characteristics of the Terfenol-D rods and frequency responses of the magnetic circuits. A second prototype actuator employing the same actuation principle was then designed by using the electrostric- tive material PMN-32%PT as the driving element. Tests were conducted to measure the actuator performance for varying electrical input conditions and fluid bias pres- sures. The peak output velocity obtained was 330 mm/s while the blocked force was 63 N. The maximum volume flow rate obtained with the PMN-based actuator was more than double that obtained from the Terfenol-D–based actuator. Theoretical modeling of the dynamics of the coupled structural-hydraulic sys- tem is extremely complex and several models have been proposed earlier. At high pumping frequencies, the fluid inertia dominates the viscous effects and the prob- lem becomes unsteady in nature. Due to high pressures inside the actuator and the presence of entrained air, compressibility of the hydraulic fluid is important. A new mathematical model of the hydraulic hybrid actuator was formulated in time-domain to show the basic operational principle under varying operating conditions and to capture the phenomena affecting system performance. Linear induced strain behav- ior was assumed to model the active material. Governing equations for the moving parts were obtained from force equilibrium considerations, while the coupled inertia- compliance of the fluid passages was represented by a lumped parameter approach to the transmission line model, giving rise to strongly coupled ordinary differential equations. Compressibility of the working fluid was incorporated by using the bulk modulus. The model was then validated using the measured performance of both the magnetostrictive and electrostrictive-based hybrid actuators. Self-Contained Hybrid Electro-Hydraulic Actuators using Magnetostrictive and Electrostrictive Materials by Anirban Chaudhuri Dissertation submitted to the Faculty of the Graduate School of the University of Maryland, College Park in partial fulfillment of the requirements for the degree of Doctor of Philosophy 2008 Advisory Committee: Dr. Norman M. Wereley, Chair/Advisor Dr. Alison Flatau Dr. Christopher Cadou Dr. Robert M. Sanner Dr. Balakumar Balachandran (cid:13)c Copyright by Anirban Chaudhuri 2008 DEDICATION To my parents and all my teachers. ii “It is difficult to say what is impossible, for the dream of yesterday is the hope of today and the reality of tomorrow.” - Robert H. Goddard “The greatest challenge to any thinker is stating the problem in a way that will allow a solution.” - Bertrand Russell iii Acknowledgments I would like to gratefully acknowledge the contributions of my advisor, Dr. Norman Wereley, towards the successful completion of my research. He has been the ideal mentor to me; he encouraged my ideas, gave me enormous freedom to try out different approaches during both the experimental stages and the theoretical work, and was always available to discuss the progress of my research. His caring attitude towards all students is exemplary. I would also like to thank the members of my dissertation committee: Dr. Alison Flatau, Dr. Christopher Cadou, Dr. Robert Sanner and Dr. Balakumar Balachandran. They took keen interest in my work and provided valuable insights into my research, all of which resulted in an organized and complete dissertation. The work presented in this dissertation would not have been complete without contributions from my colleagues at the University of Maryland. I would like to acknowledgethehelpfromDr. Jin-HyeongYoo, whoacquaintedmewiththeactuator designs and worked with me during the first stage of testing. His inputs have been invaluable and I have learnt a lot about practical mechanical design from him. I would also like to thank Dr. Shaju John for introducing me to rheology; he had great faith in the model that I later developed and played an important role in tailoring it for MR-based devices. I would also like to thank Michael Perna of the machine shop for his help in fabrication of the numerous actuator parts. I also appreciate the advice from Dr. Jayant Sirohi regarding the theoretical model. ImadeseveralnewfriendsduringmystayatMarylandandtheircompanionship iv madesurethatgraduatestudentlifedidnotbecome“allworkandnoplay”. Aspecial word of thanks to all my outstanding officemates - Dr. Wei Hu, Ben Woods, Nick Wilson, Ted Bubert, Robbie Vocke, Dr. Atulasimha Jayasimha, Supratik Datta, Dr. Greg Hiemenz, Grum Gnatu, Amy Ahure, Min Mao, Chaitanya Mudivarthi, Dr. Keejoo Lee and Dr. Young Tai Choi - you have all helped me from time to time and also livened up the lab. The helicopter design experience will never be forgotten - Ben Hein, Nick Rosenfeld, the Eric trio (Parsons, Schroeder and Silberg), Tim Beasman, Anne Brindejonc, Dr. Nagaraj, Dr. Tischenko and Dr. Inderjit Chopra - I learnt a lot from all of you. Shishir Murarka and Ayan Sengupta were my apartment-mates during the bachelor days and they are two of my closest friends today. I gratefully acknowledge the financial support from the project sponsors: US ArmyResearchOfficeunderaPhase2STTRcontract(Dr. GaryAnderson, Technical Monitor), the US Army Aviation Applied Technology Directorate under a Phase 1 SBIR Contract (Dr. Louis Centolanza, Technical Monitor) and the Office of Naval Research MURI grant (Jan Lindberg, Technical Monitor). I am also thankful to Dr. Gang Wang and Dr. Peter Chen of Techno-Sciences, Inc., for their help. My family has provided strong emotional and mental support during all my years as a graduate student. This dissertation is dedicated to my parents who made me a confident person and inspired me to always work with dedication and patience. They instilled a strong sense of independence in me and supported all my career decisions. My younger brother, Apu, maintains an excellent mix of studies and extra- curricular activities and inspired me to do the same. My wife, Sneha, is my endless source of motivation; her love and care have kept me strong and focused all these v years. Although she denies it, she deserves an equal share of the sense of achievement at the completion of the dissertation and I am truly fortunate to have her by my side. We did it !! vi Table of Contents List of Figures x List of Tables xvi List of Notations xvi 1 Introduction 1 1.1 Smart materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 1.1.1 Magnetostrictives . . . . . . . . . . . . . . . . . . . . . . . . . 17 1.1.2 Electrostrictives . . . . . . . . . . . . . . . . . . . . . . . . . . 23 1.2 Survey of smart actuator models . . . . . . . . . . . . . . . . . . . . . 31 1.2.1 Modeling of active material behavior . . . . . . . . . . . . . . 32 1.2.2 Static and quasi-static models . . . . . . . . . . . . . . . . . . 45 1.2.3 Dynamic actuator models in frequency domain . . . . . . . . . 52 1.2.4 Dynamic actuator models in time domain . . . . . . . . . . . 61 1.2.5 Use of CFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 66 1.3 Motivation and objectives of current research . . . . . . . . . . . . . . 68 1.4 Outline of Dissertation . . . . . . . . . . . . . . . . . . . . . . . . . . 71 2 Design and Testing of a Magnetostrictive Hydraulic Actuator 73 2.1 Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73 2.2 Actuator Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74 2.3 Experimental Setup . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78 2.3.1 Hybrid Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . 78 2.3.2 Input . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85 2.4 Test Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 87 2.4.1 No-Load Tests . . . . . . . . . . . . . . . . . . . . . . . . . . . 87 2.4.2 External Load Tests . . . . . . . . . . . . . . . . . . . . . . . 98 2.4.3 Characteristics of Driving Magnetic Circuit . . . . . . . . . . 103 2.5 Dynamic Tests . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 106 2.5.1 Experimental Data . . . . . . . . . . . . . . . . . . . . . . . . 106 2.5.2 Magnetic path calculations . . . . . . . . . . . . . . . . . . . . 113 2.5.2.1 Reluctance method . . . . . . . . . . . . . . . . . . . 113 2.5.2.2 FEA of Magnetic Circuit . . . . . . . . . . . . . . . . 116 2.6 Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 119 3 Dynamic Modeling of a Hybrid Electro-Hydraulic Actuator 121 3.1 Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 121 3.2 Actuator Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . 130 3.3 Characteristics of Driving Magnetic Circuit . . . . . . . . . . . . . . . 133 3.4 System Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 135 3.4.1 Pump piston and Output piston . . . . . . . . . . . . . . . . . 135 3.4.2 Pumping chamber and output cylinder . . . . . . . . . . . . . 141 vii
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