CANTILEVER METHOD FOR DETERMINATION OF dsi COEFFICIENT IN THIN PIEZOELECTRIC FILMS Samo Penič, Uroš Aljančič, Drago Resnik, Danilo Vrtačnik, Matej Možek, Slavko Amon Laboratory of Microsensor Structures and Electronics (LMSE), Faculty of Electrical Engineering, University of Ljubljana, Ljubljana, Slovenia Key words: piezoelectric, characterization, dsi coefficient, PZT, simulation, FEM, ANSYS Abstract: A cantilever method for characterization of thin piezoelectric films is proposed. Using the proposed cantilever method, piezoelectric coefficient dsi of thin film piezoelectric material on various samples was determined. Cantilever based characterization method provides a fast comparison of different piezoelectric material samples, since multiple samples can be mounted simultaneously on the testing structure. It is shown how, when combined with numerical simulation, piezoelectric coefficient dsi can be determined from fitting measured voltage response with simulated response. Exact knowledge of geometry and material properties of cantilever and samples proved to be important in order to determine piezoelectric coefficients with sufficient accuracy. Stainless steel cantilever was adequately characterized by measuring its Young's modulus. Silicon properties are adequately determined by published data. Mechanical properties of PZT layers are on the other hand more difficult to acquire, since they are rather dependent on the actual PZT preparation procedure and composition. Nevertheless, we expect that error here introduced is small due to very thin PZT layer compared to stainless steel cantilever and silicon substrate. To improve the proposed method, based on numerical simulation results, guard chips were mounted at the side of the cantilever to reduce stress variation over samples. Determined values of piezoelectric coefficients dsi for PZT layers under test were in reasonable agreement with results available in the literature. Metoda za določanje koeficienta d31 tankih piezoelektričnih filmov Kjučne besede: piezoelektrik, karakterizacija, ds1 koeficient, PZT, simulacija, silicij, FEM, ANSYS Izvleček: V članku je predstavljena metoda za karakterizacijo tankih piezoelektričnih plasti. Z uporabo ročice smo določili piezoelektrični koeficient dsi tankih piezoelektričnih filmov. Metoda omogoča hitro primerjavo lastnosti različnih materialov, ter s pomočjo numerične simulacije hkratno karakterizacijo parametra dsi večih vzorcev. Poznavanje geometrije in materialnih lastnosti ročice in vzorjev je ključno za natančno določitev piezoelektričnih koeficientov. Mehanske lastnosti jeklene ročice smo določili z meritvijo Youngovega modula, za mehanske lastnosti silicijevega substrata pa smo uporabili podatke v literaturi. Mehanske lastnosti tankih PZT plasti so težje dostopne, saj se razlikujejo zaradi same zgradbe PZT keramike ter njene priprave. Zaradi tanke plasti PZT materiala, ocenjujemo, da je napaka pri uporabi vrednosti za debele materiale zanemarljiva. Na osnovi simulacij smo predstavljeno metodo izboljšali z dodatnimi stranskimi čipi, ki izboljšajo homogenost stresa na vzorcih. Vrednosti za piezoelektrični koeficient dsi, ki smo jih določili s predlagano metodo, se ujemajo s podatki iz literature. 1. Introduction When designing a new product or device, proper material selection is of basic importance. Material properties are also used in numerical analysis, when predicting device behavior. In case of piezoelectric microstructures, the properties of thin film piezoelectrics are influenced by chemical composition and other parameters of piezoelectric manufacturing process. It is thus important to have means for analyzing specific samples of piezoelectric thin films. Due to unique properties of piezoelectric effect, piezoe-lectrics are important materials in micro-electromechanical system (MEMS) technology, used for actuation or sensing, energy harvesting etc. Characteristics of piezoelectrics, especially piezoelectric coefficients d, play important role in device design, simulation and behavior prediction. In general, thin film materials used in microengineer- ing behave differently than bulk, thus requiring an adequate characterization of their core properties. Several methods are in use /1/ and new ones are being developed. Selection of the appropriate material for a certain application requires comparison of different materials using datasheet specifying core information about these materials. Properties of piezoelectric materials vary with chemical composition, preparation technique e.g. sintering temperature and other effects. These influences present difficulties for comparison of different materials prepared by different methods, of different thicknesses and possibly from different producers, usually taking plain datasheet information from catalogue as a starting point. To overcome this obstacle a comparative method for characterization of different thin film piezoelectric samples bonded to a stainless steel cantilever is proposed. The relative response of different piezoelectric samples to the same mechanical stress gives immediate comparison of their basic properties such as sensitivity and linearity. Furthermore, coupling the measured results with numerical simulation based on finite element method (FEM) enables determination of absolute value for piezoelectric coefficient d3i. The paper presents in detail the proposed technique for thin film piezoelectrics characterization and introduces a comparative method for simultaneous evaluation of multiple piezoelectric samples based on numerical simulation in combination with measured results. The result of this characterization is the absolute value of d3i coefficient for multiple samples and comparison of piezoelectric response to mechanical stimulus. The method is practically tested on different thin film Lead Zirconate Titanate (PZT) chip samples prepared on silicon substrates. Measured results are matched with numerical simulation and piezoelectric coefficients are determined using ANSYS finite element analysis software. 2. Basic properties of piezoelectrics Piezoelectrics are materials that respond to the applied mechanical stress with electric voltage on the electrodes. This is called the direct piezoelectric effect, which serves as a basis for sensors and generators. The effect can be reversed and it is then called converse or inverse piezoelectric effect. Here mechanical strain is induced when voltage is applied. The response is dependent on the polarity of applied voltage and can therefore vary between elongation and contraction. Equations that describe electromechanical relations in a piezoelectric material are given in Voight notation with relations /2/ (1) Where {T} is stress tensor, {S} strain tensor, {E} electric field vector and {D} electric displacement vector. Material properties are described with stiffness matrix [c] which includes information about Young's modulus Y and Poisson ratio G of the material, with piezoelectric stress matrix [e] (superscript T denotes matrix transpose) related to piezoelectric strain matrix [d] and with permittivity matrix [n]. Piezoelectric strain coefficients dij and piezoelectric stress coefficients Sij are related with stiffness coefficients Cij by matrix equation [e] = [c] [d]. Piezoelectrics can be used for sensing or actuation, depending on whether the applied input load is mechanical or electrical, respectively. The two modes of operation can also be used interchangeably which makes piezoelectrics extremely versatile electromechanical materials since the same structure can act as a sensor or an actuator. Though the effect is reversible, certain considerations must be taken into account during the design of the structure /3/. 3. Piezoelectrics characterization 3.1 Bulk piezoelectrics characterization A complete characterization process of bulk piezoelectric material includes determination of stiffness coefficients Cij (including Young's modulus Y and Poisson ratio g), permittivity (nii) and piezoelectric coefficients (dij). Most widely used method adopted as IEEE standard for piezoelectric characterization is the resonance method /4/. For such characterization, piezoelectric material is prepared as a flat rectangular plate between two electrodes, forming a capacitor. The capacitor impedance Z is measured at different frequencies. From Z(f) diagram, the resonant (fr) and anti-resonant (fa) frequencies are found. Then, the elastic compliance (inverse stiffness matrix) and piezoelectric coefficients for practical purposes usually d3i and d33 can be derived /1/. Direct methods for determining piezoelectric coefficients dij include deformation measurements when voltage is applied to the electrodes. These methods are used to quantify the direct and converse piezoelectric effect. Direct methods are also used to investigate the behavior of the piezoelectric material in terms of hysteresis and nonlinear-ity, thermal behavior and aging. Mechanical deformation measurement of piezoelectric sample vs. applied voltage is used to determine piezoelectric coefficients dij, calculated from relation in Voight notation Sj = dij Ei /1/. A different method for measuring piezoelectric coefficients dij is based on direct piezoelectric effect. Here, sample is mechanically loaded, therefore the bounded electric charge becomes free, ready to flow out from the electrodes /5/. Electrodes are short circuited and electric displacement D is measured. Piezoelectric coefficient dij is here calculated from equation in Voight notation Di = dij Tj /1/. In order to determine the relative permittivity nr, capacitance measurements are carried out at low frequency, usually 1 kHz and for low AC voltage excitation levels, ranging few mV /1/. The relative dielectric constant is then calculated as Ct V (2) where t is thickness of piezoelectric layer, A electrode area, C measured capacitance and no permittivity of free space. 3.2 Thin film piezoelectrics characterization In general, the properties of thin film materials can differ significantly from its bulk counterparts. Therefore, adequate characterization of piezoelectric thin film properties is essential. Thin film characterization methods are usually based on similar principles as for bulk. The prevailing methods use converse piezoelectric effect where electrically excited thin piezoelectric film results in mechanical displace- ment, which is typically in the order of a few angstroms /6/. Sometimes the direct piezoelectric effect is used. Thin film piezoelectric together with electrodes are deposited on a substrate wafer and fixed in a rigid frame above pneumatic pressure cavity /7/. Pressure in the cavity is varied thus applying different mechanical stress to the piezoelectric layer. The charge integrator is used to measure the induced charge which is used in combination with excitation pressure to determine piezoelectric coefficients dij. For determining Young's modulus of thin piezoelectric films, several approaches exist. One of the possibilities to characterize mechanical thin film properties is presented in /8/. The experiment consists of loading a membrane with a line load applied to the middle of the span using nanoin-denter. A Mireau microscope interferometer is used to observe fringes that are formed on the loaded sample. Using a CCD camera these fringes are recorded and strains determined. From known stresses and strains in the material, Young's modulus can be determined. 3.3 Cantilever method for characterization of thin piezoelectric films In this case, characterization method is focused on piezoelectric coefficient dsi using direct piezoelectric effect. In the proposed characterization method we introduce a cantilever with mounted piezoelectric samples on silicon substrate, with exact control of deflection. Mounting several samples simultaneously to the same cantilever provides us a comparison of piezoelectric responses of various piezoelectric materials to the same stimulus. This provides fast and accurate comparison of different piezoelectric materials appropriate for R&D work. When comparing responses of different materials, relative comparative method is usually sufficient and sometimes preferred to comparing absolute values due to its simplicity. However, determination of absolute values of piezoelectric coefficients is also possible, upgrading the proposed method with analysis of mechanical setup using appropriate numerical simulation as shown later. For this purpose, finite element analysis (FEA) software ANSYS was used. Mechanical properties of piezoelectric and silicon were taken from literature /9,10/. Permittivity was determined from capacitance measurements. 4. Experimental setup Experimental setup consisting of rectangular cross-section cantilever with mounted samples is shown in Fig. 1. Due to the simplicity of cantilever with rectangular cross-section, also analytical expressions for stress distribution exist, enabling comparison with numerical results. Proposed characterization method uses samples with thin film piezoelectric capacitor structure on silicon substrate, mounted on stainless steel cantilever. The selection of optimal samples placement is essential, usually selected for high sensitivity as the region of maximum stress distribution in the beam still having sufficient uniformity. Stress decreases in cantilever longitudinal direction towards the cantilever free end where it reaches zero. Therefore, the samples are mounted in the region of maximum stress being at the root of the cantilever. Following our simulation results, care must be taken not to induce an excessive error in the placement of samples. (a) (b) Fig. 1: Top view of the cantilever with mounted samples and side guards: (a) schematic, (b) photograph For adequate characterization of piezoelectric thin film samples, high repeatability of sample loading is essential. The testing cantilever setup, together with bonded samples represents such a test structure. Stainless steel was selected as the material for cantilever, providing possibility of high repeatable deflections. Furthermore, stainless steel cantilever is mechanically resistant and can be reused after replacing samples. During characterization, samples are often exposed to higher mechanical stresses as during the normal sensor or actuator operation. To achieve such a wide measurement range, cold rolled austenitic stainless steel (1.4310) was selected for the cantilever realization. This material has an extended elastic range due to a special treatment during the fabrication. In this case, the cantilever returns to its initial position even after extremely large deflections. To achieve large measured range of stresses for samples under test, the mechanical part of testing system has to provide adaptability. Therefore, 10 cm long and 18 mm wide stainless steel strips (cantilevers) of thickness 0.5 mm were cut by milling and then pressed between two rigid stainless steel plates acting as a fixed support. In this approach, the cantilever length is adjustable, resulting in increased measured range with high repeatability and accuracy. To illustrate the characterization of piezoelectric samples with described experimental setup, various thin PZT layers were deposited by sol-gel method on silicon chips covered by Pt/Ti as reported elsewhere /11/. Gold electrodes were placed on top of PZT layer by sputtering and shaped by shadow mask method. Thin Ti and Pt layers with thicknesses of 10 and 100 nm respectively are not significant for the overall mechanical properties of the relatively thick samples and were thus neglected in numerical simulations. As an example of the proposed characterization procedure, three samples with two different thicknesses of PZT layer were introduced, marked as samples PZT1a, PZT1b and PZT2. Due to our numerical simulations, two dummy guard chips were added at cantilever sides to achieve better stress uniformity over the samples (Fig. 1). To assure a reliable transfer of induced mechanical stress from the cantilever to the PZT samples, a strong and stable bond between the cantilever and the samples has to be achieved. Therefore, an epoxy adhesive (UHU endfest 3000) with high bonding strength of 3000 N/cm2 was used for PZT samples bonding. The extended elastic range of the selected stainless steel, in the combination with the mentioned adhesive enable highly reliable loads on testing samples, up to the silicon tensile strength. In addition, samples fixed with the selected adhesive can be easily removed at relativly low temperatures what makes the testing cantilever reusable /11/. Fig. 2: Experimental setup: Tayior-Hobson traversing table and micromanipulator are used to achieve high deflection repeatability. To achieve highly repeatable stresses, testing cantilever with bonded samples is mounted on the fixed part of modified Taylor-Hobson 150mm Traversing Table, as shown in Fig. 2. The computer controlled worktable is motor driven in both directions, but can also be moved manually. Straight-ness accuracy of the worktable is within ±1 pm over the full 150mm range. In order to assure deflection repeatibil-ity, a micromanipulator with 8 mm tall pointed pin is mounted at the top of the worktable, as described in detail elsewhere /12/. Voltage response of PZT samples is measured by Semiconductor Parameter Analyzer HP4155A, including SMU and PMU Generator Expander HP41501A. For determination of piezoelectrics permittivity, capacitance on test capacitors is measured with HP4284A Precision LCR Meter at various frequencies, at excitation amplitude 1 V and DC bias 0 V. 5. Numerical modeling For the purpose of simulation, commercial FEM modeling and simulation software ANSYS was used. Simulator input for cantilever test structure with samples is built using ANSYS proprietary scripting language APDL. Meshing is done using built-in automatic mesh generator. The resulting hex-ahedral mesh of simulated test structure is shown in Fig. 3. Local improvement of the mesh was done manually to refine mesh in structure critical regions such as thin PZT layer and to avoid badly shaped elements. The test structure basically consists of several different layers - stainless steel (SS) cantilever, silicon (Si) substrate chip, metal and PZT layer. Electrodes and interface layers were neglected at mechanical simulation due to their small thicknesses. For modeling SS and Si materials, three-dimensional SOLID95 elements were used. PZT layer was modeled with SOLID226 elements with capability to couple mechanical and electrical quantities using piezoelectric effect. Fig. 3: Generated mesh of cantilever with 3 bonded samples and two side guards. When we take into account material symmetry, general form of stiffness matrix [c] for ceramics, permittivity matrix [n] and piezoelectric coefficients matrix [d] can be simplified /1/. [c]= ^11 '-12 0 0 0 Ci3 0 0 0 Cjj C33 0 0 0 0 0 0 C44 0 0 000 0 C44 0 00000 (3) [d] = "fil 00 " [n] = 0 fii 0 00 03 ■ 0 0 0 0 ^15 0 0 0 0 0 0 .^31 ^31 ^33 000 (4) (5) Due to the lack of exact information in the literature, mechanical properties of thin PZT layer were approximated by bulk values. Therefore, values cn = 13,9x101° Pa, 10 C33 = 11,5x1010 Pa, C44 = 2,56x1010 Pa, C13 = 7,43x10 Pa, C12 = 7,78x1010 Pa, were taken from literature /10/. Due to the small thickness of PZT compared to the cantilever and Si substrate, the error introduced is negligible. SS material is usually considered isotropic. The Young's modulus of SS material was measured using nanoindenta-tion method /13/. The measured value of SS Young's modulus is Y = 167.56 GPa. Silicon is very well known material. Due to Si crystal symmetry, it is described by 3 stiffness coefficients C11, C12 and C44. In our case Si was modeled using anisotropic symmetric matrix with coefficients C11 = 0,1657x106 Pa, C12 = 0,0639x106 Pa, C44 = 0,0796x106 Pa/14/. Due to the longitudinal stress dominating in our case as confirmed by our numerical simulation, only piezoelectric coefficient d3i was taken into account. Boundary conditions for cantilever at FEM simulation were fixed support on the cantilever left side (deflection and its derivative equal to 0) and free deflection on the right side. To allow simple load variation, the deflection was described in the program as a parameter. Electrical ground boundary condition was set on the bottom electrode. Standard sparse direct linear solver was used for solving the model having 85000 elements with 4 basic variables (degrees of freedom) of the problem: electric potential and displacements in x, y, z direction. Sparse direct solver is a robust and fast solver for linear and nonlinear analysis, appropriate when poorly shaped elements are present in the model, such as the high aspect ratio (thickness vs. width) elements in the model of PZT layer. The sparse direct solver is based on a direct solution of equations by elimination, as opposed to iterative solvers where the solution is obtained through an iterative process that successively refines an initial guess to the final solution that is within a prescribed tolerance of the final solution. Direct elimination requires the factorization of an initial very sparse linear system of equations into a lower triangular matrix followed by forward and backward substitution. Drawback of this solver is that it requires a significant amount of memory, thus it is not suitable for larger scale models with more than a half million variables. Because sparse direct solver is based on direct elimination, poorly conditioned matrices do not pose difficulty in producing the solution /15/. Direct solver was chosen for our simulated approach since it does not exceed the recommended number of equations and there was enough computer memory available to perform computation. Simulations were performed on Intel Core Duo 6600 64bit processor architecture with 4GB RAM memory, running at 2.4GHz. A single simulation run with chosen solver required typically 6 minutes. 6. Procedure for determination of piezoelectric coefficient dsi analyzer as described previously. Numerical simulator was configured as discussed in the previous section, to translate the test structure into numerical model. The characterization of piezoelectric effect and related d3i parameter was performed by fitting the measured voltage response with simulated response: d31 parameter value was varied in the simulator until a good match between measured and calculated voltage response was found. The value of d3i that provided best fit throughout all deflections between calculated and measured voltage response was selected as the final result for the piezoelectric coefficient d3i. 7. Results and Discussion The PZT samples capacitance was measured using LCR meter at frequencies ranging from 20 Hz to 10 kHz, at excitation voltage of 10 mV. A relatively small dependence of capacitance vs. frequency was detected (Fig. 4). Measured capacitance value at 1 kHz was taken, as stated in /1/. Top electrode area was measured under the microscope. PZT layer thickness was measured after the fabrication of the layer. From data given in Table 1 the relative permittivity hr for samples was calculated. Samples PZT1a and PZT1b are built on the same PZT layer differing only in their electrode position, regarding to the cantilever support (Fig. 1). Electrode of PZT1a was located 2.7 mm from the support, while the electrode of PZT1b was located 5.4 mm from the cantilever support. Sample PZT2 was prepared with modified processing for double thickness of PZT1, resulting in changed value of PZT permittivity. The electrode location for PZT2 was the same as for PZT1a, 2.7 mm from the support. Simulated stress profile in PZT layer is shown in Fig. 5 (simulation path is shown in the inset). From Fig. 5 can be concluded that electrode exact position is important when performing characterization of multiple samples. Following our numerical simulations results, to minimize the difference of stress profile in neighbor samples, two longer guard chips are added at the sides, as shown in Fig. 1. Calculated stress distribution in the cantilever and samples is shown in Fig. 6a. (T EL 4 w U PZTIaand PZTIb PZT2 1—- I I [ I I 1 I I [ I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I -t -M-l I I I I I I I I I I I I I I i I I ' I I . I I 1 The described experimental setup was used to deflect cantilever. Corresponding voltage response of the mechanically loaded PZT samples was measured with parametric Frequency [Hz] Fig. 4: Measured samples CapaCitanCe vs. frequenCy. Table 1: Measured sample parameters and calculatedrelatlve permittivity of PZT layers Sample PZT Thickness [mn] Electrodes rmm^l Capacitance [nF] Rel. permittivity fir PZTla 740 0.87 7.67 737 PZTlb 740 0.87 7.67 737 PZT2 1554 0.87 2.40 484 Fig. 5: Simulated longitudinal stress profile in PZT layer vs. position on Si chip. The effect of guard chips is quantified in Fig. 6 and Table 2. As shown, the absolute stress in samples is decreased when guard chips are present. However, stress uniformity over the samples improves significantly. The relative difference in stress in both cases, without and with guard chips, was calculated between central and side samples. Guard chips thus provide more homogenous stress conditions on all samples. According to the piezoelectric effect, voltage response is proportional to the stress, what is described by piezoelectric coefficients. Calculated voltage response of PZT samples due to calculated stress is given in Fig. 6b. Measured time dependent voltage response of PZT samples during testing is shown in Fig. 7. Here, the cantilever was deflected to predefined values using the micromanipulator as previously described. At start, the cantilever was first manually deflected over the desired deflection value, and then after this it was released to rest in final position determined by micromanipulator. Similar procedure was applied also during the end of testing. Consequently, voltage spikes always occurred at the start and at the end of loading. As also seen in Fig. 7, the response for constantly deflected cantilever slowly decreases with time, probably due to piezoelectric internal effects such as leakage and recom- (a) (b) Fig. 6: Simulated longitudinal stress distribution in stainless steel cantilever and silicon chips (a) and corresponding voltage on top of PZT layer due to accumulated charge (b). Positions on the chips A, B and C show where stresses were compared. binations, and due to external effects such as input impedance of HP4155A connected to the sample. Therefore, measurement of the response was done after the spike settled down, typically after 10 seconds. Table 2: Improvement of the stress uniformity over samples when guard chips are used. Stress in samples without guard chips [MPa] Stress in samples with guard chips [MPa] Position B Positions A, C Rel. difference Position B Positions A, C Rel. difference 13.19 14.74 10.5 % 10.04 10.08 3.7 % Table 3: Measured voltage response and simulated values for different deflections of cantilever with best fit value for d31 parameter. PZTla PZTlb PZT2 Deflection MeasfmVl Sim [mVl MeasfmVl Sim [mVl MeasfmVl Sim [mVl 3.175 mm 35.5 35.24 24.9 27.80 41 37.38 5.715 mm 60.0 63.40 50.8 50.10 63.7 67.30 8.255 mm 95.4 91.62 76.9 72.43 92.5 97.19 10.795 mm 121 119.8 93.9 94.70 125 127.1 13.335 mm 144 148.0 114 117.0 158 157.1 15.875 mm 173 176.2 141 139.1 187 186.9 Fig. 7: Measured voltage response vs. time during testing Measured voltage response results are graphically displayed in Fig. 8. The response amplitude is dependent on electrode distance from the cantilever support and is in correlation with simulated stress profile in PZT layer shown in Fig. 5. The voltage on PZT1a is thus considerably higher than voltage on PZT1b. PZT2 that differs in thickness and material properties produces response that is slightly higher than with PZT1a. Determination of piezoelectric coefficient d31 was done by using numerical simulation as described previously. Successive simulations were performed for various values of coefficient d31 until close agreement between simulated and measured voltage response was obtained. Measured and simulated responses at various deflections for best values of piezoelectric coefficient d31 are given in Table 3. The summary of measured values for relative permittivity nr and piezoelectric coefficient d31 for PZT materials under test is given in Table 4. Results obtained are in reasonable agreement with available values from the literature /7/. Table 4: Measured properties of PZT layer. Sample Relative permittivity -ör Piezoelectric coef. - dji [pC/N] PZTla 737 -66.1 PZTlb 737 -66.1 PZT2 484 -20.7 Fig. 8: Measured voltage response of PZT samples vs. deflection. Graphical representation of measured and simulated voltage responses vs. deflection for all three PZT samples are shown in Fig. 9. In the range of measured deflections, the simulated response displays linearity while it is slightly distorted for measured values, probably due to measurement error. 8. Conclusion Using the proposed cantilever method, piezoelectric coefficients d31 for various thin film piezoelectrics were determined. Cantilever based characterization method provides a fast comparison of different piezoelectric material samples, since multiple samples can be mounted simultaneously on the testing structure. Furthermore, when combining experimental data with numerical simulation, piezoelectric coefficient d31 can be determined by matching simulated results with voltage response measurements. Exact knowledge of geometry and material properties of cantilever and samples proved to be important in order to measure piezoelectric coefficients with sufficient accuracy. Stainless steel cantilever was adequately characterized by measuring its Young's modulus. Silicon properties are adequately determined by published data in the literature. Mechanical properties of PZT layers are on the other hand more difficult to acquire, since they are rather dependent on the actual PZT preparation procedure and composition. Nevertheless, we expect that error here introduced (b) Fig. 9: Graphical representation of measured and simulated voltage response of PZTsamples vs. deflection. is small due to very thin PZT layer compared to stainless steel cantilever and silicon substrate. To improve the presented method, based on numerical simulation results guard chips were mounted at the side of the cantilever to reduce stress variation over the samples. Determined values of piezoelectric coefficients dsi for PZT layers under test were in reasonable agreement with results available in the literature. Acknowledgment Authors would like to acknowledge Electronic Ceramics Department - K5, Jožef Stefan Institute, Slovenia for PZT samples preparation. This work was supported by Ministry of Higher Education, Science and Technology and Slovenian Research Agency. References /1/ T.L. Jordan, Z. Ounaies, "Piezoelectric Ceramics Characterization". NASA/ CR-2001-211225 ICASE report to NASA Langley Research Center. Report No. 2001-28, September 2001. /2/ Ansys Inc. "Ansys Inc. Theory reference". Ansys Inc., 2005. /3/ S. Penič, U. Aljančič, D. Vrtačnik, D. Resnik, M. Možek and S. 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Proc. 43rd International Conference on Microelectronics, Devices and Materials and the Workshop on Electronic Testing, Bled, Slovenia, September 2007, pp. 115-120. /13/ S. Penič, U. Aljančič, D. Vrtačnik, D. Resnik, M. Možek, M. Ma-kovec, R. Bošnjak and S. Amon "FEM modeling of piezoresis-tive force sensor for medical retractor and design verification". Proc. 6'h EUROSIM Congress on Modelling and Simulation, Ljubljana, Slovenia, September 2007, p. 158. /14/ A. M. Fitzgerald "Practical Issues in Finite Element Analysis of MEMS". Ansys Workshop, March 2006. /15/ Ansys Inc. "Ansys Inc. Basic Analysis Guide". Ansys Inc., 2005. Samo Penič, univ. dipl. inž. el. mag. Uroš Aljančič doc.dr. Drago Resnik doc.dr. Danilo Vrtačnik mag. Matej Možek prof.dr. Slavko Amon University of Ljubljana, Faculty of Electrical Engineering, Laboratory of Microsensor Structures and Electronics Trzaska 25, Ljubljana i000, SLOVENIA e-mail: matej.mozek@fe.uni-lj.si Telefon: 0i 4768 sos, Telefax: 0i 4264 6s0