Transducer Control Algorithms

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Transducer Control Algorithms Presented by George Bromfield UIA 36 th Symposium NPL London March 21, 2007

Background Need to precisely control the velocity (displacement) of ultrasonic tools (end effectors) Velocity Control of High Q Transducers Operating at or close to resonance F R For Example: Ultrasonic jack-hammer handpiece for cataract removal (Phacoemulsification) Velocity Control of Low Q Transducers Operating at or close to Anti-resonance F A For Example: Axya ultrasonic suture welding handpiece

Scope of this Presentation Piezoelectric Ceramic Aging and Stability The medical environment Novel Simple Method of Velocity Control Compensates for changes in piezo properties that occur during operational use Applicable for control algorithms based on constant current High Q transducers operating at or close to F R Comparison of Operational Performance at F R and F A Control based on constant current @ F R versus constant voltage @ F A Computer model and practical experiments

Changes in Piezo Properties (All Transducers) Piezo Aging & Stability (Berlincourt Illustrations) Permanent Changes p Material Permittivity (transducer capacitance) Aging approximately logarithmic in nature Temporary Changes t Exposure to mechanical stress, high electric field, or elevated temperature Log t After Poling Permanent and temporary changes have Material Coupling coefficient (transducer Fa - Fr) same sign (+) for permittivity For coupling coefficient the permanent change is ( ) and the temporary change is (+) Log t After Poling

hanges in Piezo Properties (Medical Transducers) Langeven style subjected to multiple steam sterilization cycles Permanent Changes p Combined effects of autoclave temperature (137 C) and bias stress Extrapolated from measured Navy Type I data (Krueger 1961) Piezo Bias Stress (MPa) 25 35 45 55 65 Fraction of initial d 33 value.9.85.77.70.65 Fraction of initial K T 33 value 1.04 1.06 1.08 1.10 1.12 Temporary Changes t Immediately after a 137 C autoclave cycle (cold water rapid cool down) Navy Type III piezo with nominal 30 MPa bias stress Coupling coefficient k increased by 5.2 % Dielectric constant (capacitance) increased by 16%

Computer Model Effects of Permanent Changes PiezoTran (based on acoustic transmission line theory) Illustrative example: Black and Decker Buzz Ultrasonic Stain Removal Transducer Model Input: Voltage adjusted to maintain a constant current = 200 ma r.m.s. Model Output Resonant frequency increases from approximately 51 khz to 52 khz as bias stress is increased

Measure Temporary Changes as a result of a steam sterilization cycle Measurement Method Laser vibrometer Power meter Signal generator Measured Data

Scope of this Presentation Piezoelectric Ceramic Aging and Stability The medical environment Novel Simple Method of Velocity Control Compensates for changes in piezo properties that occur during operational use Applicable for control algorithms based on constant current High Q transducers operating at or close to F R Comparison of Operational Performance at F R and F A Control based on constant current @ F R versus constant voltage @ F A Computer model and practical experiments

Evolving a Method of Velocity Control Assumptions Constant current Operating close to the resonance frequency Observations Tip velocity increases as piezo properties are degraded by: Age, Bias stress and High temperature cycles The increase in velocity is inversely proportional to coupling coefficient (k eff ) Implementation Apply a correction factor based on a measured value of (k eff ) Measure / calculate k eff immediately prior to, and during operational use

Methods of Measuring K eff Based on the Resonant Characteristic F R and F A k = 1 F F r a 2 k 2 ( F F ) a r F r Complex System Control Algorithm Frequency sweep from below resonance to above antiresonance Determine maximum and minimum impedance Compute k eff and apply current correction factor

Methods of Measuring K eff Based on the Clamped Non-motional Characteristic Equivalent circuit at low frequency Equivalent circuit at high frequency k = C 1 ( C + C ) 0 1 Mole s Method Based on measuring capacitance above and below resonance Calculated by substituting in the formula: C A C B k = α ( C + C ) A B Correction factor required for transducers with high gain horns

Mole Illustrative Example Measured data k = α C A C B ( C + C ) A B α = 5 k = 0.191

Evolving & Simplifying Mole Premise: Factor M is proportional to coupling coefficient k F B = 48 khz Phase = -89.7 I B = 12.65 ma F A = 55 khz Phase = -89.8 I A =7.4 ma M = I I B B + I I M = 0.512 A A

Velocity Control Using Correction Factor M M Proportional to K eff Measuring/calculating Factor M Measure current I B and I A at frequencies below and above resonance Ensure current is substantially reactive (phase angle < -89 ), widen frequency range if necessary Calculate correction Factor M using the formula: M = Calculating Factor M Scaling Factor Computer model transducer with end effector attached Simulate new and end-of-life conditions Calculate Factor M for extreme conditions Calculate current velocity ratio for extreme conditions Calculate current correction factor based on Factor M I I B B + I I A A

Velocity Control Summary Method Simple and efficient control Eliminates the need to detect F R and F A involving multiple measurements Based on measurement of current and phase below and above resonance Can be applied during a prime cycle prior to operational use Can also be applied during operational use Applications Medical, industrial and Navy transducers control system algorithms based on constant current Medical loose tip detection Based on measurement of phase

Scope of this Presentation Piezoelectric Ceramic Aging and Stability The medical environment Novel Simple Method of Velocity Control Compensates for changes in piezo properties that occur during operational use Applicable for control algorithms based on constant current High Q transducers operating at or close to F r Comparison of Operational Performance at F R and F A Control based on constant current @ F R versus constant voltage @ F A Computer model and practical experiments

Practical Experiments Simulation of Transducer Loads Air Q = 1000 O rings slid over horn Q=150 Wet chamois wrapped over horn Q = 25 Typical Phaco and Dental Handpieces Typical Ultrasonic welding transducer Measured data HP Analyzer @ 1 volt

Practical Experiments Simulation of Transducer Loads Laser vibrometer Power meter Signal generator Transducer horn displacement 3 µm p-p F R F A V volts I ma V volts I ma No Load 1.3 57 54.97 O Ring 9.0 53.3 45.7 11.3 Chamois 36 64 62 30

Computer Model Effect of changes in piezo properties @ F A and F R F A Constant Voltage Drive Relatively stable voltage/velocity ratio immune from changes in coupling coefficient Piezo k 33 Selecting a Piezo material with high k 33 is important because load is less reactive

Optimizing System Performance Constant Current Operation at or Close to F R Lowest possible drive voltage (low tan δ loss and high efficiency) Linear velocity control over a wide range of loading conditions Q factors typically range from 100 to 2000 Requires a correction factor to compensate for changes associated with age, temperature and bias stress Constant Voltage Operation at or Close to F A Operating at very high power with low Q loads <100 Linear velocity control relatively immune from changes in piezo properties caused by heat Low quiescent power in the no-load condition Very high impedance at F A

Piezo Innovations This research has been internally funded by PI and is protected by a patent application. for supplying the References US Patents 3,432,691 Oscillatory Circuits for Electro-acoustic Converter & 3,443,130 Apparatus for Limiting the Motional Amplitude of an Ultrasonic Transducer (1969) Inventor Andrew Shoh Ultrasonic Transducer Materials edited by Oskar E. Mattiat (Don Berlincourt referenced contributor). Published by Plenum Press 1971 Underwater Electroacoustic Transducers by D. Stansfield published by Peninsula Publishing M. J. Earwicker, Mathematical Modelling of Piezoelectric Transducers, and Sean Winterer for developing the PiezoTran software based on this model