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CALCULATION OF CYLINDRICAL MULTILAYER ELECTROMECHANICAL TRANSDUCER AT DIFFERENT POLARIZATION TYPES IN NON-STATIONARY MODES.

UDC 539.3

Introduction. Piezoceramic electromechanical multilayer cylindrical transducers are often used in acoustoelectric devices for receiving and emitting an acoustic signal including non-stationary one. In this regard it is necessary to study the transmission of electroelastic disturbances in multilayer piezoceramic bodies of cylindrical shape under various manufacturing parameters and operating conditions.

In this work oscillations of a multilayer piezoceramic hollow cylinder with electrode surfaces of separation of layers are explored. Oscillations are caused by sudden potential difference, alternating sign for the adjacent layers. An important issue in designing such bodies is the choice of polarization direction of layers, which affects the emissive ability of the element. Therefore the study of electromechanical state of the piezoelectric element in different polarization types and the choice of optimal variant is accepted as the purpose of the work.

Analysis of recent research and publications. Research of oscillations of piezoceramic elements of constructions with non-stationary electrical and mechanical loads is an important aspect for the mechanics of conjugated fields. The fundamental issues of electroelasticity problems formulation, including in a cylindrical coordinate system [1, etc.], are considered. Analytical solutions of a number of important problems of hydroacoustics in non-stationary formulation [2] are proposed. The classical approaches to the formulation and solving of axisymmetric oscillations of multilayer massive bodies and shells of cylindrical and spherical form are described [3, 4, etc.]. Oscillations of homogeneous radially polarized cylinders with non-stationary loads [5, 6] were reflected. The stationary and nonstationary oscillations of piezoceramic bodies with curved surfaces were investigated [7, 8]. Harmonic oscillations of heterogeneous magneto-electroelastic cylinders were studied [9]. Axisymmetric oscillations in cylinders with piezoceramic radially polarized layers were studied [10].

The publications analysis shows that the study of the disturbance transmission in electroelastic multilayer cylinders (and other rotation bodies that are planned for research in subsequent works) depending on the number of layers and their polarization direction as well as the conditions of securing and loading is indeed an urgent and important task in the design process of devices that operate based on piezoelectric effect.

Problem statement. The radial oscillations of a multilayer hollow cylinder consisting of n piezoceramic polarized through-thickness layers with separating surfaces [R.sub.0] <... < [R.sub.k] < ... < [R.sub.n], where [R.sub.n]--external, [R.sub.0]--internal radius of a cylinder are studied. Oscillations of a k layer are described by the motion equation and the electric induction equation in a cylindrical coordinate system

[mathematical expression not reproducible], (1)

[mathematical expression not reproducible], (2)

under material ratio in layers with radial polarization direction (i = 1 ... n)

[mathematical expression not reproducible],

In the case of an alternating polarization direction we have

[mathematical expression not reproducible]. (3)

Here [u.sup.k] (r, t) and [[sigma].sup.k.sub.ik]--mechanical displacement and stress, [D.sup.k.sub.r] (r, t) --component of radial direction vector of electrical induction; [[phi].sup.k] (r, t)--electrical potential; [[rho].sup.k]--material density; [c.sub.ij.sup.k] elasticity module at a constant electric field; [[epsilon].sup.k.sub.33]--dielectric capacity at constant deformation; [e.sup.k.sub.ij] piezoelectric module of a k layer.

Initial conditions are imposed on displacement and its speed

[mathematical expression not reproducible]. (4)

Stress or displacement is set on the outer surfaces

u([R.sub.a], t) = [U.sub.a](t) [conjunction] [[sigma].sub.r] ([R.sub.a], t) = [p.sub.a](t), a = 0, n. (5)

The conditions of full contact are met between the layers k = 1, ..., n - 1

[u.sup.k]([R.sub.k]) = [u.sup.k+1]([R.sub.k]), [[sigma].sup.k.sub.rr]([R.sub.k]) = [[sigma].sup.k+1.sub.x]([R.sub.k]), [[phi].sup.k+1]([R.sub.k]). (6)

The electrodes in layers separating surfaces and outer surfaces indicate the potential difference

[phi]([R.sub.k]) = [(-1).sup.k+1] V(t), k = 0, ..., n . (7)

In [10] on the layers separating surfaces of the piezoceramic sphere, in addition to the condition of electric potential equality, the electrical induction continuity conditions are given by analogy with (6). In our case this condition is not necessary because the electrical induction continuity condition is placed if internal electrodes are absent or not connected to electric field.

For the universality of the solution we introduce dimensionless variables

[mathematical expression not reproducible], (8)

where [l.sub.0], [[rho].sub.00], [c.sub.00], [[epsilon].sub.00], [t.sub.l] = [l.sub.0][square root of ([[rho].sub.00]/[c.sub.00])]--standardized values. With such nondimensionalization the output equations will not change.

In the transition in (1) (2) towards displacements and electric potential being the solving functions (3) for k-layer we receive

[mathematical expression not reproducible], (9)

[mathematical expression not reproducible]. (10)

Hereinafter in order to take into account the polarization direction in layers we consider [e.sup.k.sub.33] = [e.sub.33] in the case of polarization of all layers in the radial direction, and [e.sup.k.sub.33] = [(-1).sup.k-1] [e.sub.33] if the first layer is polarized radially, the further ones are polarized alternating-sign next but one.

Thus we obtain the initial-boundary value problem, which is described by the equation (9) with initial and boundary conditions (4) (5). The electric potential of each time layer is determined by displacement from (10) under the conditions (7).

Numerical solution. In order to solve the initial-boundary value problem we construct a numerical scheme based on difference approximations. Within the integration interval [R.sub.0] < ... < [R.sub.k] < ... < [R.sub.n] we introduce the partition:

[OMEGA] = {[r.sub.m(k-1)+i], = [R.sub.k-1] + (i - 1)[[DELTA].sub.k], [[DELTA].sub.k] = ([R.sub.k] - [R.sub.k-1])/m, k = 1, ..., n, i = 1, ..., m + 1} .

Let us proceed from the continuum functions to the desired discrete values of functions at the partition points: u([u.sub.m(k-1)+i]) = [u.sub.m](k-1)+i-1], [[phi]([r.sub.m(k - 1)+i]) = [[phi].sub.m(k - 1) + i - 1].

The difference form of the equations (9), (10) that is formulated for internal partition points takes the following form:

[mathematical expression not reproducible], (11)

[mathematical expression not reproducible]. (12)

Electric potential on the outer surfaces and separating surfaces equals (7)

[[phi].sub.m(k - 1) + 1] = [(-1).sup.k] V(t), k = 1, ..., n + 1. (13)

Displacement on the outer surfaces is found from the difference form of material ratios, written with one-sided difference expressions with second-order accuracy

[mathematical expression not reproducible]. (14)

Matching condition (6) converts to

[mathematical expression not reproducible].

The displacement on separating surfaces is determined by displacement and electric potential at inner points:

[mathematical expression not reproducible]. (15)

In matrix form the system of equations (11) (12), taking into account (13) - (15) at the inner partition points, turns into

[rho][[d.sup.2]U/d[t.sup.2]] = AU + B[PHI] + [F.sub.1], D[PHI] = CU + [F.sub.2], (16)

where U = {[u.sub.m(k - 1) + i - 1]}, [PHI] = {[[phi].sub.m(k = 1) + i - 1]}, k = 1, ..., n, i = 2, ..., m .

The system (16) time integration is done by introducing partition at of the time interval t [member of] [0, T] with the step [DELTA]t. The solution is searched by means of the explicit difference scheme

[[??].sup.p+1] = [[u.sup.p+1] - 2[u.sup.p] - [u.sup.p-1]]/[DELTA][t.sup.2],

in which the inner points displacement in the p +1 time layer is determinated from (11) because of the known displacement and electric potential of the p-time-layer, and the electric potential is found from (12) through inner displacements on the same layer. On the boundaries and surfaces of conjugation the displacement is determined from (14) (15).

When applying an implicit difference scheme (Newmark algorithm)

[mathematical expression not reproducible],

where [xi]--scheme parameter, system (14) forms a single matrix, from which all unknowns at inner points are determined at the same time. An important issue of explicit scheme application is partition step size selection in spatial and temporal coordinates, since the explicit scheme stability condition must be satisfied. Practice shows that it's usually enough to accept [[DELTA].sub.x] [greater than or equal to] 10[DELTA]t. For an implicit scheme steps of one order are chosen.

Numerical results. Let us consider the non-stationary oscillations of the ceramic ball PZT-4 [6] under zero initial conditions. Disturbance is given in the form of V(t) = [V.sub.0]H(t), where H(t)--Heaviside function. Such load is the most convenient for studying dependencies of transmission and reflection of disturbance waves. Oscillations research of n-layer cylinders with parallel and reverse polarization directions of layers is conducted. Geometric parameters are [R.sub.0] / [R.sub.n] = 0.5, where n--the number of layers. The results are presented in dimensionless form.

Fig. 1 shows that in radially polarized cylinders with a pair and odd number of layers oscillations arise with the amplitude of one order, respectively. Oscillations represent a superposition of radial and thickness oscillations. The frequency of radial oscillations depends on the geometric dimensions of the cylinder [5] and is the same for all cases considered. As the number of cylinder layers grows the frequency of the thickness oscillations increases, which is associated with a decrease in the characteristic oscillatory size, in this case the layer thickness h. Maximum displacements arise in cylinders with an odd number of layers, which is explained by the summation of displacements with different signs occurring in adjacent layers. Polarization of such elements is carried out by applying positive potential difference to outer electrodes, the inner ones are not connected to the electric circuit. Maximum displacements in all cases arise on the inner surface, on the outer surface in the case of an odd number of layers we have [u.sub.max]([R.sub.n]) [approximately equal to] 2.5 and [u.sub.max]([R.sub.n]) [approximately equal to] 0.8 for a pair number of layers.

Fig. 2 illustrates the oscillations of the outer surface of the cylinder with the oncoming polarization of the layers. We see that the displacement is practically proportional to the number of layers, since the deformation of each layer is the same and is summed up with each other. The period of radial oscillations is the same as in the previous case (Fig. 1). The maximum displacement values are proportional to the maximum displacements of the odd number of layers under radial polarization: [u.sub.max]([R.sub.n]) [approximately equal to] 2.5n.

The analysis of the results shows that the circumferential stress is also proportional to the number of layers. For radial stresses the dependence is not so linear, but stress also increases as the number of layers grows.

Fig. 3 depicts curves of radial stresses on the median surface and circumferential stresses on the outer surfaces. It can be seen that the maximum values for radial and circumferential stresses are approximately the same, but they occur at different points of the cylinder. The frequency of change in radial stresses corresponds to the thickness oscillations of the cylinder [5] and the circumferential stresses change with the frequency corresponding to the radial oscillations.

An interesting research issue is the pattern of disturbance transmission in a cylinder. Let us consider the distribution of stresses at different moments of time (n = 5, oncoming polarization) using the results shown in Fig. 4.

Fig. 4 clearly shows that since the electric load application the stress inside the body attained certain values that are practically identical at all points of the layers (in this case [R.sub.k] = 0.6, 0.7, 0.8, 0.9), but from the outer free surfaces there is wave transmission displacement with the speed [a.sub.k] = [square root of (c.sup.k.sub.33]/[[rho].sup.k])] and, according to the graph, when t > 0.2 waves overlay.

Finally let us analyze the dependence of oscillations on the geometrical proportions in cylinders with the same number of layers. Fig. 5 shows the displacements that arise in five-layer cylinders with different inner openings. As the inner opening grows the displacement and oscillations frequency increase significantly. Displacements of the sphere with an opening [R.sub.0] = 0.3[R.sub.n] are more than five times less than displacements of the sphere [R.sub.0] = 0.7[R.sub.n].

Conclusions. The developed approach enables effective research of dynamic electromechanical state of piezoceramic multilayer cylinders at electrical and mechanical loads. It is established that radially polarized cylinders with a pair number of layers emit high-frequency oscillations of low amplitude. The oscillations of radially polarized cylinders with an odd number of layers are close to the solid cylinder oscillations in amplitude and period.

The frequency of radial vibrations of multilayer cylinders coincides with the frequency of solid cylinders. The amplitude values of displacements of cylinders with oncoming polarized layers are proportional to the number of layers. With inner opening growth the outer surface oscillations and their frequency increase significantly.

Thus when designing electromechanical transducers operating in non-stationary modes it is necessary to take into account the abovementioned regularities and carry out a detailed calculation of specific elements of structures. The proposed numerical scheme makes it possible to extend the scope of the method by changing the securing and loading conditions, materials of layers, including elastic ones.

References

[1.] Babayev A.E. (1990). Unsteady waves in continuous media with a system of reflective surfaces. Kyiv: Naukova Dumka.

[2.] Busch-Vishniac I.J. (1999). Electromechanical Sensors and Actuators. New York: Springer.

[3.] Guz A.N., Kubenko V.D. & Babayev A.E. (1984). Hydroelasticity of shell systems. Kiev: High School.

[4.] Kubenko V.D. (1979). Nonstationary interaction of structural elements with the environment. Kiev: Naukova Dumka.

[5.] Shul'ga N.A. & Grigor'eva L.O. (2009). Radial electroelastic nonstationary vibration of a hollow piezoceramic cylinder subject to electric excitation. International Applied Mechanics, 45, 2, 134-138.

[6.] Ding H.J., Wang H.M. & Hou P.F. (2003). The transient responses of piezoelectric hollow cylinders for axisymmetric plain strain problems. Int. J. of Solids and structures, 40, 105-123.

[7.] Shulga M.O. & Grigoryeva L.O. (2010). Electromechanical unstationary thickness vibrations of piezoceramic transformers at electric excitation. Mechanical Vibrations: Types, Testing and Analysis, 179-204.

[8.] Shul'ga N.A. & Grigor'eva L.O. (2011). Comparative Analysis of the Electroelastic Thickness Vibrations of Layers with Curved Boundaries. International Applied Mechanics, 47, 2, 177-185.

[9.] Yu J., Ma Q., & Su Sh. (2008). Wave propagation in non-homogeneous magneto-electro-elastic hollow cylinders. Ultrasonics, 48, 8, 664-677.

[10.] Grigorenko A. Ya. & Loza I.A. (2011). Axisymmetric waves in layered hollow cylinders with piezoceramic radially polarized layers. Problems of Computational Mathematics and Strength of Construction, 17, 87-95.

[phrase omitted]; Grigoryeva Ludmila, ORCID: https://orcid.org/0000-0001-7013-0327

Received May 08, 2017

Accepted December 09, 2017

L. Grigoryeva, PhD, Assoc. Prof.

Kyiv National University of Construction and Architecture, 31 Povitroflotskiy Ave., Kiev, Ukraine 03680; e-mail: l_grigoryeva@ukr.net

DOI: 10.15276/opu.1.54.2018.01

Caption: Fig. 1. Displacement of inner surface r = [R.sub.0] of n-layer cylinders with radial polarization of layers

Caption: Fig. 2. Displacement of outer surface r = [R.sub.n] of n-layer cylinders with oncoming polarization of layers

Caption: Fig. 3. Circumferential and radial stress of five-layer cylinders with oncoming polarization of layers

Caption: Fig. 4. Distribution of radial stress of five-layer cylinders radially

Caption: Fig. 5. Outer surface oscillations of five-layer cylinders of various radii

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Title Annotation:MACHINE BUILDING. PROCESS METALLURGY. MATERIALS SCIENCE
Author:Grigoryeva, L.
Publication:Odes'kyi Politechnichnyi Universytet. Pratsi
Article Type:Report
Date:Mar 1, 2018
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