Investigating the Electromechanical Coupling in Piezoelectric Actuator Drive Motor Under Heavy Load

Similar documents
Investigating the Electromechanical Coupling in Piezoelectric Actuator Drive Motor Under Heavy Load

Class-D amplifier design and performance for driving a Piezo Actuator Drive servomotor.

Power enhancement of piezoelectric transformers for power supplies.

combine regular DC-motors with a gear-box and an encoder/potentiometer to form a position control loop can only assume a limited range of angular

Active Vibration Isolation of an Unbalanced Machine Tool Spindle

Computer Numeric Control

Optimizing Performance Using Slotless Motors. Mark Holcomb, Celera Motion

Gear Transmission Error Measurements based on the Phase Demodulation

UNIVERSITY OF UTAH ELECTRICAL ENGINEERING DEPARTMENT LABORATORY PROJECT NO. 3 DESIGN OF A MICROMOTOR DRIVER CIRCUIT

Advanced Motion Control Optimizes Laser Micro-Drilling

Piezoelectric multilayer triaxial accelerometer

PART 2 - ACTUATORS. 6.0 Stepper Motors. 6.1 Principle of Operation

CHAPTER 5 FAULT DIAGNOSIS OF ROTATING SHAFT WITH SHAFT MISALIGNMENT

Basic NC and CNC. Dr. J. Ramkumar Professor, Department of Mechanical Engineering Micro machining Lab, I.I.T. Kanpur

CONTROLLING THE OSCILLATIONS OF A SWINGING BELL BY USING THE DRIVING INDUCTION MOTOR AS A SENSOR

Synchronization Control Scheme for Hybrid Linear Actuator Based on One Common Position Sensor with Long Travel Range and Nanometer Resolution

CHAPTER 6 INTRODUCTION TO SYSTEM IDENTIFICATION

Angle Encoder Modules

MEMS. Platform. Solutions for Microsystems. Characterization

Veröffentlichungen am IKFF PIEZOELECTRIC TRAVELLING WAVE MOTORS GENERATING DIRECT LINEAR MOTION

MAGNETIC LEVITATION SUSPENSION CONTROL SYSTEM FOR REACTION WHEEL

NOISE REDUCTION IN SCREW COMPRESSORS BY THE CONTROL OF ROTOR TRANSMISSION ERROR

Utilization of a Piezoelectric Polymer to Sense Harmonics of Electromagnetic Torque

Periodic Error Correction in Heterodyne Interferometry

PHASE DEMODULATION OF IMPULSE SIGNALS IN MACHINE SHAFT ANGULAR VIBRATION MEASUREMENTS

M-041 M-044 Tip/Tilt Stage

Active Vibration Control in Ultrasonic Wire Bonding Improving Bondability on Demanding Surfaces

Robot Joint Angle Control Based on Self Resonance Cancellation Using Double Encoders

NOISE AND VIBRATION DIAGNOSTICS IN ROTATING MACHINERY

DC and AC Circuits. Objective. Theory. 1. Direct Current (DC) R-C Circuit

V2018 SPINSTAND AND NEW SERVO-8 SYSTEM

Generator Advanced Concepts

PDu150CL Ultra low Noise 150V Piezo Driver with Strain Gauge Feedback

T10F. Data Sheet. Torque Flange. Special features. Installation example T10F. B en

1. INTRODUCTION. Keywords: Piezo, Mechanism, Tip-tilt, Stability, Strain gages. BSM Mechanism context

648. Measurement of trajectories of piezoelectric actuators with laser Doppler vibrometer

Smart off axis absolute position sensor solution and UTAF piezo motor enable closed loop control of a miniaturized Risley prism pair

ACTUATORS AND SENSORS. Joint actuating system. Servomotors. Sensors

3. What is hysteresis loss? Also mention a method to minimize the loss. (N-11, N-12)

Last Name Girosco Given Name Pio ID Number

NON-SELLABLE PRODUCT DATA. Order Analysis Type 7702 for PULSE, the Multi-analyzer System. Uses and Features

EE 410/510: Electromechanical Systems Chapter 5

Application of Gain Scheduling Technique to a 6-Axis Articulated Robot using LabVIEW R

UNIVERSITY OF JORDAN Mechatronics Engineering Department Measurements & Control Lab Experiment no.1 DC Servo Motor

Electronic Instrumentation and Measurements

Description of options, upgrades and accessories for the laser beam stabilization system Compact

GUZIK V2002 Spinstand with XY-Positioning For Head, Headstack and Disk Testing

Department of Mechanical Engineering, College of Engineering, National Cheng Kung University

Maximizing LPM Accuracy AN 25

PI piezo Life Time Test Report. A. Bosotti, R. Paparella, F. Puricelli

CHAPTER 6 THREE-LEVEL INVERTER WITH LC FILTER

Sensors and Sensing Motors, Encoders and Motor Control

SHORT PULSE CHARACTERIZATION OF NONLINEARITIES IN POWER ULTRASOUND TRANSDUCERS.

Voltage-Versus-Speed Characteristic of a Wind Turbine Generator

GEM-P Progress Report Mechanics (July 2006)

Single Phase Permanent Magnet Low Speed Synchronous Motor

n Measuring range ,02 N m to N m n Clockwise and counter-clockwise torque n Low linearity deviation of ± 0.05 % F.S.

P-810 P-830 Piezo Actuators

PDu150CL Ultra-low Noise 150V Piezo Driver with Strain Gauge Feedback

T40FH. Torque flange. Special features. Data sheet

The units of vibration depend on the vibrational parameter, as follows:

SAGITTAL SAW BACKGROUND OF THE INVENTION

Improved direct torque control of induction motor with dither injection

Experiment 3. Performance of an induction motor drive under V/f and rotor flux oriented controllers.

Product Information. ERN 1085 Incremental Rotary Encoder with Z1 Track

Michael F. Toner, et. al.. "Distortion Measurement." Copyright 2000 CRC Press LLC. <

Position Control of AC Servomotor Using Internal Model Control Strategy

Natural frequencies of rotating disk-like structures submerged viewed from the stationary frame

Enhanced Fault Detection of Rolling Element Bearing Based on Cepstrum Editing and Stochastic Resonance

PeakVue Analysis for Antifriction Bearing Fault Detection

Bakiss Hiyana binti Abu Bakar JKE, POLISAS BHAB

CHAPTER-III MODELING AND IMPLEMENTATION OF PMBLDC MOTOR DRIVE

Channel Characteristics and Impairments

Machine Tools with an Enhanced Ball Screw Drive in Vertical Axis for Shaping of Micro Textures

Investigation on Sensor Fault Effects of Piezoelectric Transducers on Wave Propagation and Impedance Measurements

P-611.Z Piezo Z-Stage

Current-Based Diagnosis for Gear Tooth Breaks in Wind Turbine Gearboxes

DC SERVO MOTOR CONTROL SYSTEM

The Air Bearing Throughput Edge By Kevin McCarthy, Chief Technology Officer

Rotating Machinery Fault Diagnosis Techniques Envelope and Cepstrum Analyses

SKF TOROIDAL ROLLER BEARING CARB PRODUCTIVITY IMPROVEMENT AND MAINTENANCE COST REDUCTION THROUGH RELIABILITY AND SUSTAINABILITY

Introduction to Measurement Systems

A novel procedure for evaluating the rotational stiffness of traditional timber joints in Taiwan

Application Information Advanced On-chip Linearization in the A1332 Angle Sensor IC

THE STUDY OF THE SYNCHRONOUS MOTOR

T40FM. Data Sheet. Torque flange. Special features. Overall concept. B en

PiezoMike Linear Actuator

RMC S ENSOR TELEMETRY. A Sensortelemetrie M MANNER. FGP Sensors & Instrumentation

Detection of Wind Turbine Gear Tooth Defects Using Sideband Energy Ratio

Realization of Absolute Capacitive Rotary Encoder System Based on Capacitive Gate Technology

5. Transducers Definition and General Concept of Transducer Classification of Transducers

Figure 4.1 Vector representation of magnetic field.

Examination of Microphonic Effects in SRF Cavities

COVENANT UNIVERSITY NIGERIA TUTORIAL KIT OMEGA SEMESTER PROGRAMME: MECHANICAL ENGINEERING

SIMPLE GEAR SET DYNAMIC TRANSMISSION ERROR MEASUREMENTS

Performance Optimization Using Slotless Motors and PWM Drives

University of Jordan School of Engineering Electrical Engineering Department. EE 219 Electrical Circuits Lab

Beam Dynamics + Laser Micro Vibrometry 1

T40B. Torque Flange. Special features. Data sheet. Overall concept

Supplementary Information

Transcription:

Investigating the Electromechanical Coupling in Piezoelectric Actuator Drive Motor Under Heavy Load Tiberiu-Gabriel Zsurzsan, Michael A.E. Andersen, Zhe Zhang, Nils A. Andersen DTU Electrical Engineering Technical University of Denmark Oersteds Plads, bld. 349 Kgs. Lyngby, Denmark Email: tgzsur@elektro.dtu. Abstract The Piezoelectric Actuator Drive (PAD) is an accurate, high-torque rotary piezoelectric motor that employs piezoelectric stack actuators and inverse hypocycloidal motion to generate rotation. Important factors that determine motor performance are the proper concentric alignment between the motor ring and shaft and the similarity of the stack actuators used. This paper investigates the electromechanical coupling of these factors into the motor current through experimental means. Keywords motor, actuator, piezoelectric, piezo, stack, multilayer I. I NTRODUCTION The Piezoelectric Actuator Drive (PAD) which can be seen in Fig. 1 is a type of rotary motor that transforms the linear motion of piezoelectric stack actuators into a precise rotational motion [1]. The operating principle is illustrated in Fig. 2. The micro-mechanical toothing present in the ring and shaft, shown in Fig. 3, enables high positioning accuracy and output torque [2]. This type of toothing combined with the inherent large stiffness of the piezoelectric stack actuators makes the PAD appropriate for voltage-driven open-loop control [3]. Due to its inherent structure, the PAD motor behaves like a fully capacitive, voltage-driven rotary machine. The piezoelectric stack actuators forming the basis of motion in this motor give it a capacitive nature. This, coupled with the reversibility of the piezoelectric effect enable the stacks to act as both actuators and sensors [4]. The current flow to the motor provides information about rotor speed and position, but also indicates the quality of mechanical contact between stator and rotor through electromechanical coupling between the shaft and the stacks. The aim of this paper is to use current measurement from the piezoelectric stack actuators to describe and qualify the mechanical coupling between the motor ring and shaft under both heavy and no load conditions. Fig. 1: The Piezoelectric Actuator Drive (PAD) voltage applied to the stack produces a proportional mechanical elongation. The layers are in a parallel configuration electrically, enabling a reduced voltage level to produce the necessary electric field. Mechanically, they are in a series configuration and therefore the elongation of each layer adds up to produce larger displacement than a single element would. A widely-used model for piezoelectric structures is described in the IEEE Standard on Piezoelectricity [5]. A simplified version of the second alternative form of the constitutive equations given by the IEEE Standard are shown in (1) and (2), particularized for the dimension of actuation of a stack actuator. Stress in other directions is assumed to be null. Table I shows the quantities, their names and their units of measurement. II. M OTOR OPERATION PRINCIPLE A piezoelectric stack actuator comprises of hundreds of individual piezoelectric layers separated by thin electrodes. A 978-1-4799-6768-1/14/$31.00 2014 IEEE 538 1 F k Q D C V C D33 F x D D33 V (1) (2)

TABLE I: List of constitutive equation symbols and their units Symbol Name SI Unit x Displacement m Q Stack charge C V Applied voltage V F Applied force N D 33 Piezoelectric constant m=v or C=N k Stack spring constant N=m 2 Motor shaft Motor ring Joint Piezo actuator Preload spring Welding Mount Fig. 2: PAD operating principle Two sinusoidal voltages with a 90 ı phase shift between them are applied to stack actuators placed orthogonally, as shown in Fig. 2. Thereby the motor ring moves in a circular trajectory defined by Cartesian coordinate pair.r x ;r y /, expressed by the parametric equations (3) and (4). This will, in turn, produce a rotation in the motor shaft in the opposite direction to the ring. r x D x 1 sin.2f t C 1 / (3) r y D x 2 sin.2f t C 2 / (4) Where x 1 and x 2 represent the elongation of the orthogonal stacks in m, f is the frequency of rotation in Hz and 1 and 2 are the phases in rad, with the restriction that 1 2 D =2. The trajectory produced is perfectly circular only if x 1 D x 2. This requires that the stack actuators are identical. Stack mismatch, improper shaft centering, hysteresis effects, and mechanical effects coupling into the motion will all produce deviations from circularity and in practice this will always be the case. Every full rotation of the ring will cause the shaft to step one tooth. Therefore the relationship between the electrical and mechanical angular velocities! el and! m is shown in (5), with N shaf t and N ring representing the number of teeth on Fig. 3: Microtoothing on the motor shaft. Tooth distance is 120 µm and depth is 38 µm the motor shaft and ring, respectively.! m D! el N shaf t N ring N shaf t (5) III. EXPERIMENTAL SETUP The experiments were conducted using a PAD7220 produced by Noliac A/S, shown in Fig. 5. It contains two piezoelectric stack actuators on each actuation axis. They are represented by the red and blue rectangles in the figure. Their capacitance is rated at 3.5 µf. The rated motor speed is 56.7 rpm with a gearing ratio between ring and shaft of 312. Rated torque is 4 N m. The applied sinusoidal voltages have an amplitude of 100 V and an offset of 100 V. An oscilloscope and current clamps with a bandwidth of 50 MHz were used to acquire and log the motor current. Measurements were taken with the motor running at 60 Hz electrical speed, under conditions of no load and 3 N m of load torque. A data acquisition window of 5 seconds together with a sampling rate of 200 ksa/s were used in order to capture accurate data for a full mechanical revolution. The block diagram of the test setup is presented in Fig. 4. IV. MEASUREMENT RESULTS Analysis of the measurement data yields interesting results. The acquired data was first normalized for easier comparison between the loaded and unloaded cases. Fig. 6 and Fig. 7 show 539

Signal generator Driver V x V y PAD Oscilloscope i x i y Fig. 4: Block diagram of the experimental setup Fig. 5: The PAD7720 without the black cover. The stack ends are exposed: two on the X axis (red rectangles) and two on the Y axis (blue rectangles). the trajectory of the traveling contact point between the motor ring and shaft during a mechanical quarter-circle motion. Each blue curve represents one electrical revolution and tooth step. The red pegs each represent one tooth on the shaft and help with visually keeping track of shaft position. The dotted black circles represent the ideal, undistorted trajectory. The first observation is a pronounced deviation from circularity of the trajectory which is caused by lack of hysteresis compensation. Piezoelectric stack actuators are highly hysteretic [6] [7] and this effect can readily be seen in the contact point trajectory. A second observation is the presence of a resonance in the case of the loaded motor which cannot be seen in the unloaded case. This resonance is the result of hard electromechanical coupling between the actuators and the shaft due to the high load applied to the motor shaft. This indicates that the motor is very close to its output torque limit, while also showing the absolute position of the weakest contact point the starting point of the resonance. If load is increased further, a tooth skip will occur at that point. The lack of symmetry along the first diagonal of the trajectory plot further indicates that the loading on the stack actuators is not symmetrical. Specifically, the flattened region visible in both the loaded and unloaded cases in the lower right area of Fig. 6 and Fig. 7 suggests a lack of proper centering between the ring and shaft. The current does not increase as it should, therefore the stacks are blocked and cannot expand properly in that quadrant. More information can be obtained by analyzing the singlesided amplitude spectra of the currents on both actuation axes with and without motor load. The input signals to the motor are ideally pure-tone phase-shifted sinusoids. Therefore, the ideal actuator response is also sinusoidal. The spectra, shown in Fig. 8 and Fig. 9 were computed over a full mechanical revolution of the motor shaft, meaning 312 electrical signal periods. By analyzing these signals, it becomes quickly obvious that a lot of energy is contained in the signal harmonics. The fundamental frequency mirrors the motor electrical speed (60 Hz), but harmonic components can be detected all the way down to the 92nd harmonic. This confirms the highly nonlinear response of the motor to input voltages. Furthermore, since the input signals are purely sinusoidal, the quality of the motor response can be evaluated through signal-to-noise ratio (SNR), total harmonic distortion (THD) and signal-to-noise and distortion ratio (SINAD) analyses [8]. Table II presents the values obtained for each actuator axis, with the motor both loaded and unloaded. The SNR is higher under load than in the unloaded case. This is attributed to an increase in signal value while the noise floor is constant. The difference between the two axes in each case is consistent and further enforces the conclusion that the stacks are unevenly loaded. In all cases, the absolute values of the THD and SINAD measurements are approximately equal. This suggests that most of the distortion in the signals is harmonic distortion. V. CONCLUSION The present paper uses empirical methods to investigate the effects of the electromechanical coupling between motor shaft and actuators in a PAD motor, under no load and loads of 3 N m. The information contained in the trajectory plot of the ring-shaft contact point extracted from the normalized current 540

1 1 0:5 0:5 Normalized Iy 0 Normalized Iy 0 0:5 0:5 1 1 0:5 0 0:5 1 Normalized I x 1 1 0:5 0 0:5 1 Normalized I x Fig. 6: Normalized contact point trajectory plot under heavy load (blue). The dotted circle is the ideal trajectory while the red pegs represent the number of teeth passed. Fig. 7: Normalized contact point trajectory plot under no load (blue). The dotted circle is the ideal trajectory while the red pegs represent the number of teeth passed. TABLE II: Values for SNR, THD and SINAD in loaded and unloaded cases Case Heavy load No load Axis X Y X Y SNR (db) 37.895 40.625 35.079 35.897 THD (db) -17.367-18.503-17.638-20.139 SINAD (db) 17.365 18.543 17.561 20.059 measurements indicate rotor-ring misalignment as well as show the absolute position of the weakest point of contact. Further analysis of the single-sided amplitude spectra of the stack actuators together with the current signal-to-noise ratio (SNR), total harmonic distortion (THD) and signal-to-noise and distortion ratio (SINAD) calculations enforce the conclusions drawn from the time and spatial plots of the current signals. These metrics also state that most of the distortion in the signals is harmonic distortion. It was shown that the motor current carries a wealth of information about not only the loading effects on the shaft, but the quality of the mechanical assembly procedure. Moreover, the analysis can be conducted on any readily-assembled motor and therefore this a potentially useful tool in production quality assurance. [4] C. Wallenhauer, B. Gottlieb, A. Kappel, T. Schwebel, J. Rucha, and T. Lueth, Accurate load detection based on a new piezoelectric drive principle employing phase-shift measurement, Journal of Microelectromechanical Systems, vol. 16, no. 2, pp. 344 350, 2007. [5] Standard on piezoelectricity, IEEE, 1988. [6] L. Juhasz, J. Maas, and B. Borovac, Parameter identification and hysteresis compensation of embedded piezoelectric stack actuators, Mechatronics, vol. 21, no. 1, pp. 329 338, 2011. [7] G. T. Zsurzsan, C. Mangeot, M. A. E. Andersen, Z. Zhang, and N. A. Andersen, Piezoelectric stack actuator parameter extraction with hysteresis compensation, Power electronics and applications, 16th European Conference on, in press. [8] C. Karandjeff, C. Hannaford, R. Liggiero, S. Max, and S. J. Tilden, Measuring snr, sinad, and thd quickly, EE Evaluation Engineering, vol. 50, no. 10, pp. 18, 20 1, 2011. REFERENCES [1] A. Kappel, B. Gottlieb, and C. Wallenhauer, Piezoelectric actuator drive (pad), AT-AUTOMATISIERUNGSTECHNIK, vol. 56, no. 3, pp. 128 135, 2008. [2] J. Rucha, H. Liess, J. Heinzl, A. Kappel, T. Schwebel, and B. Gottlieb, Applicability of a piezo actuator drive as a sensorless high precision drive, 10th International Conference on New Actuators, 2006. [3] R. Zeichfussl, B. Gottlieb, C. Wallenhauer, S. Herzig, A. Kappel, and T. Luth, A method for auto-adjustment of a new piezoelectric drive, in Mechatronics, 2009. ICM 2009. IEEE International Conference on, April 2009, pp. 1 6. 541

I x I y 10 1 10 2 10 3 10 4 Frequency (Hz) Fig. 8: Single-Sided Amplitude Spectra of I x.t/ and I y.t/ under heavy load I x I y 10 1 10 2 10 3 10 4 Frequency (Hz) Fig. 9: Single-Sided Amplitude Spectra of I x.t/ and I y.t/ with no load 542