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Modeling of a Bridge-Shaped Nonlinear Piezoelectric Energy Harvester

  • Giacomo Gafforelli , Ruize Xu , Alberto Corigliano EMAIL logo and Sang-Gook Kim
Published/Copyright: July 11, 2014
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Abstract

Piezoelectric microelectromechanical systems (MEMS) energy harvesting is an attractive technology for harvesting small energy from ambient vibrations. Increasing the operating frequency bandwidth of such devices is one of the major challenges to be solved for real-world applications. A MEMS-scale doubly clamped nonlinear beam resonator has demonstrated very wide bandwidth and high-power density among the energy harvesters reported. In this paper, a first complete theoretical discussion of nonlinear resonance-based piezoelectric energy harvesting is provided. The sectional behavior of the beam has been studied through the Classical Lamination Theory (CLT) specifically modified to introduce the piezoelectric coupling and nonlinear Green-Lagrange strain tensor. A lumped parameter model has been built through Rayleigh–Ritz method and the resulting nonlinear coupled equations have been solved in the frequency domain through the Harmonic Balance Method (HBM). Finally, the influence of external load resistance on the dynamic behavior has been studied. The theoretical model shows that nonlinear resonant harvesters have much wider power bandwidth than that of linear resonators but their maximum power is still bounded by the mechanical damping as is the case for linear resonating harvesters.

Introduction

Piezoelectric microelectromechanical systems (MEMS) have been proven to be an attractive technology for harvesting small amount of energy from ambient vibrations. This technology promises to eliminate the need for replacing chemical batteries or complex wiring in microsensors/microsystems, moving us closer toward battery-less autonomous sensor systems and networks. In the meantime, new developments in sensors and complementary metal oxide semiconductor (CMOS) circuitry technology have considerably reduced the power consumption of electronics which can now be powered by a few μW of continuous power from ambient vibrations (Kim, Priya, and Kanno 2012). For MEMS-scale energy harvesters, piezoelectric transduction is the most appropriate scenario since standard MEMS thin-film processes are available for many piezoelectric materials, assuring high efficiency, high energy density and scalability of the device design. Operating frequency, frequency bandwidth, excitation level, power density and size are the key design requirements.

At the present time, most of the devices reported in the literature do not meet the desired requirements mainly due to the very narrow bandwidth and not-low-enough resonant frequency. Cantilever laminated beams with thin films of lead zirconate titanate Pb(Zr,Ti)O3 (PZT) on Si or SiNx have been widely used to achieve high-power generation at large deflections near the resonant frequency (Jeon et al. 2005). However, the frequency bandwidth of the linear resonance system is extremely small, making the harvesters very impractical. Moreover, excessive strain at the exact resonance may shorten the life time of the harvester due to the accelerated piezoelectric fatigue over 0.2% strain on the piezoelectric thin film.

Exploiting nonlinear behaviors has been identified as a possible solution to solve the issues emerged by studying cantilever linear harvesters. The effect of nonlinear piezoelectric constitutive equations has been studied in cantilever beam harvesters showing that one- or two-mode approximations are not sufficient to accurately predict the performance of the cantilever harvester (Abdelkefi, Nayfeh, and Hajj 2012). Other authors proposed bistable harvesters that exploit instability induced by pre-stresses or additional external magnetic interactions (Harne and Wang 2013). These designs seem promising but still require an external intervention (as glued magnets or pre-stresses) which enhances fabrication-related issues.

A nonlinear resonance-based energy harvester was designed and developed for ultra wide-bandwidth (UWB) energy harvesting (Hajati and Kim 2011). It was demonstrated that both wide enough bandwidth resonance and high enough power density could be achieved by a doubly clamped beam nonlinear resonance energy harvester. A doubly clamped beam at large deflection requires stretching strain in addition to the bending strain to be geometrically compatible, which stiffens the beam as the beam deflects and transforms the dynamics to the nonlinear regime. Interdigitated electrodes were employed to convert the stretching strain into electrical charge through d33-mode piezoelectrics. This device exploits pure geometrical constraints to induce the nonlinear hardening behavior to the clamped beam, in this way it is not required an additional external intervention on the harvester (as for common bistable) and the fabrication complexity is considerably reduced. Moreover, bridge resonant harvesters, in which nonlinear effects are activated due to axial stretching, can easily achieve the full strain capability of the piezoelectric layer since higher longitudinal strains can be obtained at equal transversal displacement with respect to e.g. cantilever linear resonators. This significantly shrinks the size of the device.

In this paper, a first comprehensive theoretical discussion on nonlinear resonance-based piezoelectric energy harvesting is provided. First, the electrical damping is considered as a linear dashpot added to the classical mechanical damper and the influence of the additional damping has been studied. It has been shown that the maximum power generation of nonlinear resonant harvesters is theoretically bounded by the mechanical damping of the dynamic system, which is the same as the well-known result for linear piezoelectric harvesters (duToit, Wardle, and Kim 2005). Theoretical modeling of this damping boundedness is presented here for nonlinear harvesters (Section 2). In Section 3, this result is verified through a more accurate model which considers the influence of an external load resistance to the dynamic behavior of the nonlinear oscillator. The sectional behavior of the doubly clamped beam is studied through the Classical Lamination Theory specifically modified to introduce the piezoelectric coupling and nonlinear Green-Lagrange strain tensor. A lumped parameters model is built and solved through the Harmonic Balance Method (HBM). The theoretical model shows that nonlinear resonant harvesters have much wider power bandwidth than that of linear resonators, but their maximum power is still bounded by the mechanical damping as is the case for linear resonating harvesters.

Simple model with linear electrical damping

A general nonlinear piezoelectric resonant energy harvester is modeled in Figure 1 by a spring-mass system. kL and kN are the linear and nonlinear stiffness, cM and cE are the linear mechanical and electrical damping, mc is the concentrated mass and w is the displacement of the mass relative to the reference system, finally yext is the displacement of the reference frame to the ground. The system behaves as a Duffing oscillator and its dynamics is described by eq. [1]:

[1]mcw¨+cE+cMw˙+kLw+kNw3=y¨extmc

In the case of a doubly clamped beam, at large deflections the stretching strain increases the stiffness. The hardening behavior is obtained when kN>0. The solution of eq. [1] is achieved through the HBM in case of harmonic excitation (Worden and Tomlinson 2000). Harmonic balance mimics the spectrum analyzer by simply assuming that the response to a sinusoidal excitation is a sinusoid at the same frequency. A trial solution w = Wsin(ωt) is substituted in the equation, then the coefficients of the same harmonics are equated and the nonlinear Frequency Response Function (FRF) is computed as shown in eq. [2]:

[2]Y=ΩM2+1+34αY2+i2ζE+ζMΩM1

where α=kN/kLW02 is a measure of the nonlinearity of the system, W0 is the linear static displacement, Y=W/W0 is the dimensionless amplitude, ΩM = ω/ωn is the dimensionless excitation frequency, ζM= cM/2ωnmc and ζE= cE/2ωnmc are the electrical and mechanical damping ratios.

Figure 1 
					Nonlinear energy harvester with linear electric damping
Figure 1

Nonlinear energy harvester with linear electric damping

The equivalent stiffness and the natural frequency are amplitude dependent, which explains the hardening behavior of the oscillator as shown in eq. [3]):

[3]keq=kL(1+34αY2)ωn=(kLm(1+34αY2))1/2
Figure 2 shows the influence of damping on the amplitude response. The higher the damping the lower is the jump-down frequency and the displacement amplitude. The maximum amplitude and the jump-down frequency are given in eq. [4] (Brennan et al. 2008).
[4]Yd(23α((1+3α4(ζE+ζM)2)1/21))1/2Ωd121/2(1+(1+3α4(ζE+ζM)2)1/2)1/2
Figure 2 
					FRF of the Duffing oscillator for different values of electrical damping (α = 0.048, ζM = 0.0056, ωn = 0.0016)
Figure 2

FRF of the Duffing oscillator for different values of electrical damping (α = 0.048, ζM = 0.0056, ωn = 0.0016)

The linear electric dashpot represents the amount of damping injected in the system by the piezoelectric material, thus the power generation is given by the power dissipated by the dashpot.

As shown in Figure 3, the power generation increases until the system jumps down, before which the power reaches the maximum. Moreover, the amount of power that can be extracted depends on the electrical damping injected in the system. When the electrical damping is zero, no power can be harvested, while when the damping is too high, the oscillator does not move and no power is then produced. An optimal electrical damping which maximizes the power generation lies in between. Providing the power spectrums for varying electrical damping, the envelope of all peaks is obtained (black line in Figure 3).

By comparing Figure 3 to the well-known power response of a linear harvester (Du Toit 2005), it is proved that nonlinear harvesters have a much larger bandwidth than linear harvesters which are useful only when operating near the resonance frequency of the system. Computing the power at the jump-down using eq. [4], a closed expression of the maximum power is provided:

[5]Pd=12CEw˙2=ζEmy¨ext24ω0(ζM+ζE)2

Eq. [5] is the same to the result that was obtained for linear harvesters (Roundy 2003), and the peak power occurs when ζE = ζM, as it can be shown in Figure 3 or by providing the derivative. The previous expression can be considered as a theoretical upper bound to the power generation for all kind of resonant energy harvesters. However, this does not mean that ζE= ζM is always the optimal condition for the oscillator. However, this is true only at Ω = Ωd (as in linear system it is true only at resonance) while for other excitation frequencies, the optimal electrical damping is higher (when Ω < Ωd) or lower (when Ω>Ωd) than the mechanical damping. In conclusion, each excitation frequency requires a specific electrical damping for the harvester to work in the optimal condition.

Figure 3 
					Power response of the Classical Duffing Oscillator for different values of electrical damping
Figure 3

Power response of the Classical Duffing Oscillator for different values of electrical damping

The simple model suggests that the electrical damping needs to match the mechanical damping at the maximum power; thereby eq. [5] provides an upper limit for both linear and nonlinear resonant harvesters. However, the model relies on a strong hypothesis on the piezoelectric coupling, which should take into account the nonlinear behavior. This issue is considered in the following section with more accurate modeling of the piezoelectric coupling.

Accurate model

A more accurate model needs to be developed since the model presented in Section 2 is not suitable to describe the completely coupled piezoelectric behavior. Indeed, a linear dashpot is not sufficient enough to describe the coupling as it was extensively demonstrated (Roundy 2003; Du Toit 2005). For instance, the previous simple model is not able to explain the increase of stiffness due to the piezoelectric coupling. A coupled nonlinear model of a doubly clamped piezo-laminated beam is developed in this paper. The sectional behavior of the beam is studied by means of Classical Lamination Theory (CLT) specifically modified to introduce the piezoelectric coupling and nonlinear strain. By appropriate hypothesizing on the deflection and electric field, a lumped system is obtained and then solved through HBM. The influence of the external load resistance is then studied and the results obtained in Section 2 are confirmed.

Figure 4 
					Doubly clamped bridge-shaped piezolaminated beam with tip mass
Figure 4

Doubly clamped bridge-shaped piezolaminated beam with tip mass

Geometry

The doubly clamped beam resonator is presented in Figure 4. L and h are the half length and the total thickness of the piezolaminated beam, respectively. A concentrated mass (mc) is placed in the middle of the beam. The x1-coordinate originates in the neutral axis and is directed downward while x3-coordinate lies along the beam axis. A PZT layer is placed on top of the beam substrate and is activated in d33-mode when the beam deflects. To implement d33-mode, interdigitated (IDT) electrodes span one surface of PZT thin film, which has been polarized along x3-axis, wraps from one electrode to the next in alternating directions. In such way, when the PZT layer is stretched an electric field arises parallel to the x3-axis, the generated charge can be collected by the IDT electrodes. The IDT electrodes are alternatively connected, resulting in a couple of electrodes. One of them is grounded while the other is attached to an external load resistor (R), which represents an ideal external circuit employed for managing the power generated by PZT.

Sectional behavior: Modified Classical Lamination Theory (MCLT)

The beam’s final stack is not homogeneous since different layers are deposited. The mechanical response of the layered beam can be obtained by means of a number of theories (Ballhause et al. 2005). A very thin beam must be designed to activate nonlinear stretching. Thus, CLT is adopted here in order to introduce the piezoelectric coupling in PZT layer and the Green-Lagrange nonlinear strain tensor. The bending (S33–L) and stretching (S33–N) strains along the beam axis are computed from Euler–Bernoulli kinematics assumptions and the Green-Lagrange strain–displacement relationship:

[6]S33L=x12w1x32S33N=12(w1x3)2

where w1 and w3 are the vertical and horizontal displacement of the beam neutral axis.

The electric potential (ϕ) is constant across the piezoelectric layer. Piezoelectric constitutive laws are adopted to describe strain–stress relation, the fully coupled law for d33-mode reads as follows:

[7]T33=C33S33e33E3+T33rD3=e33S33+ε33SE3

where T33 is the stress component parallel to x3-axis, T33r is the residual stress component, S33 is the strain tensor component, D3 the electric displacement component, E3 the electric field component (E3 = −∇ϕ) and C33, e33 and ε33S are the elastic, piezoelectric and dielectric constant, respectively. Eq. [7] is known as the e-form of piezoelectric constitutive relations.

By considering a layered section and by integrating on the thickness, one obtains the generalized stiffness usually defined for the theory of laminates. In such a case, the new constitutive law contains, in the integrated constitutive equations, the generalized stiffness due to residual stresses and the generalized piezoelectric coefficient. Moreover, the same procedure is adopted on the electrical part of the constitutive law obtaining the internal capacity. The same method is applied to compute the equivalent translational and rotational mass of the beam which are summed to the concentrated mass (Ardito et al. 2013).

Lumped model: Rayleigh–Ritz method

Rayleigh–Ritz method is adopted to describe beam deflection and electric potential along the beam. The vertical displacement is modeled as a cubic polynomial while the electric potential can be considered as linear because the strain is constant between two electrodes (Figure 5). The coordinate x3 starts in the middle of each electrode and is directed opposite to the polarization vector P3 which wraps from one electrode to the next in alternating directions.

[8]w1(x3;t)=w(t)ψw(x3)=w(t)(3(x3/L)22(x3/L)3)ϕ(x3;t)=v(t)ψv(x3)=v(t)(x3*a/2)/l
Figure 5 
						Polarization and electric potential between IDT electrodes
Figure 5

Polarization and electric potential between IDT electrodes

Motion equation

Euler–Lagrange equations are used to compute the motion equation:

[9]ddtLq˙iLqi+Dq˙i=0

where the Lagrangian is a combination of kinetic energy (K), internal energy (E) and external work (W):

[10]L=KEW

The involved quantities are computed as follows:

[11]E=12VT33S33D3E3dV=1220LA(T33S33D3E3)dAdx3
[12]K=12mtip(w˙+y˙ext)2+12Vρ(w˙1+y˙ext)2dV=12mtip(w˙+y˙ext)2+1220LAρ(w˙1+y˙ext)2dAdx3
[13]W=qv
[14]D=12cMw˙2

where V and A are the volume of the beam and the area of the beam cross section.

By employing assumptions of eqs [6]–[8], and solving eq. [9] for qi=w,v the motion equations of the coupled system connected to an external load resistance read:

[15]mww¨+cMw˙+(kl+kr)w+kNw3Θχvv+Θηvwv=myy¨extkEv+Θχvw1/2Θηvw2=qq˙=R1v

where mw is the total mass, my is the mass activated by the external acceleration; kl, kr and kN are the linear elastic, the residual stress and the nonlinear stiffness; kE is the internal capacitance of PZT, Θχv and Θηv are the linear and nonlinear coupling coefficients, cM is the mechanical damping coefficient, and R is the external load resistance. The coefficients are computed by integrating the shape functions and the generalized constitutive coefficients on the volume of the beam.

[16a]ENN=12V(C33S33N)(S33N)dV=12VC33(12ψw2w2)2dV=14kNw4
[16b]EEL=12V2(e3E3)(S33L)dV=12V2(e3ψvv)(x1ψww)dV=Θηvvw
[16c]EEN=12V2(e3E3)(S33N)dV=12V2(e3ψvv)(x1ψww)dV=12Θηvvw
[16d]EEE=12V2(ε3E3)(E3)dV=12V2(ε3ψvv)(ψww)dV=12kEv2

The other coefficients are computed in the same way but they are not reported since they are customary in CLT (Ardito et al. 2013).

Eq, [15] describes the dynamic behavior of the nonlinear harvester. Additional coupling terms arise with respect to a linear harvester. When substituting the aforementioned assumptions in the internal energy expression (eq. [11]), the nonlinear strain (∝w2) multiplies the piezoelectric strain (∝ v) and an additional “nonlinear coupled term” (eq. [16c]) is obtained. Accordingly to eq. [9], by differentiating with respect to w and v, new nonlinear coupling terms proportional to w appear in eq. [15]. These additional coupling terms are negligible at low w, physically the bending strain prevails on the stretching strain and the beam does not activate the nonlinear regime. In this case, eq. [15] reduces to the classical equations of linear harvesters (Du Toit 2005).

Solution: HBM

The oscillator frequency response to harmonic excitations is studied through HBM. Nonlinear systems do not respond to a monoharmonic signal with a monoharmonic at the same frequency but all harmonics are involved in the response (Worden and Tomlinson 2000). The solution provided by HBM is always an approximation, since to appropriately apply the method the trial solution must be an infinite sum of all harmonics. However, according to physic considerations, one or few of harmonics are enough to correctly describe the dynamics. In this case, the amplitude is well described by a single harmonic, while two harmonics are required to get the correct voltage response since stretching mode has twice the frequency of bending one. Moreover, at large amplitudes, the linear response (described by the first harmonic) can be neglected and only the second harmonic survives. Neglecting the linear coupling terms and substituting the trial solutions w = W sin(ωt) and v = V sin(2ωt+ Φv) in eq. [15], the FRF is computed:

[17]Y={[ΩM2+1+(34α+κηv2ΩM22(4ΩM2+ΩE2))Y2]+i[(2ζM+κηv2ΩE4(4ΩM2+ΩE2)Y2)ΩM]}1

where ΩM= ω/ωn is the dimensionless excitation frequency, ΩE= 1/RkEωn is the dimensionless cut-off frequency of the circuit (RkE is the time constant of the RC circuit) and κηv = W0 Θηv/(kEkL)1/2 is the effective piezoelectric nonlinear coupling coefficient. κηv is a global measure of the degree of coupling which takes into account d33-mode piezoelectric coupling coefficient κ33 = e33/(C33εS33)1/2, geometrical and nonlinear aspects. In case of a pure linear piezoelectric system, κηv would exactly coincide with κ33.

The equivalent stiffness and damping coefficients depend on the amplitude because of the nonlinear behavior of the system:

[18]keq=kL(1+(34α+κηv2ΩM22(4ΩM2+ΩE2))Y2)ζeq=ζM+ζE=ζM+(κηv2ΩE8(4ΩM2+ΩE2))Y2

For small amplitudes, the nonlinear behavior is not activated, and no damping is injected into the system by the coupling activated by the stretching strain. In this case, the bending strain dominates and the FRF in eq. [17] would reduce to one of a linear harvester where equivalent stiffness and damping do not depend on amplitude (duToit 2005).

The displacement response Y is obtained by solving a cubic equation in ΩM resulting from the module of eq. [17], and the shape of the response is similar to the Duffing oscillator response. As eq. [18] shows, the external load resistor modifies the stiffness and the damping. According to the value of R, the curve is more (or less) distorted, and the value of jump-down frequency is modified too. In short circuit condition (S.C.), R→0 (ΩE → ∞), the stiffness reduces to the equivalent stiffness of the classical Duffing oscillator (eq. [3]), while the electrical damping goes to zero and no energy can be harvested. In open circuit condition (O.C.) R→∞ (ΩE → 0), the equivalent stiffness is increased while, as expected, the electrical damping still goes to zero and no energy can be harvested. All intermediate conditions depend on the value of R. Starting from O.C. condition, the damping introduced in the system increases as ΩE increases, until the maximum damping is reached. After this point, increasing ΩE reduces the electrical damping injected in the system until the S.C. condition is reached. As a result, the jump-down frequency, which depends on the total damping ratio value, decreases as ΩE increases, until to a minimum value (blue line in Figure 6), and then grows to reach the S.C. condition.

Figure 6 
						Amplitude response for different values of cut-off frequency
Figure 6

Amplitude response for different values of cut-off frequency

Electrical damping and power generation

The power generation is computed and plotted in Figure 7 by employing the relation shown in eq. [19]:

[19]P=v2R=mωn3ΩM2κηv2ΩE84ΩM2+ΩE2W4

The electrical damping injected to the system has a maximum when the displacement amplitude and the jump-down frequency are the lowest. This maximum depends on the value of the effective coupling coefficient κηv. Two situations must be considered: the peak electrical damping (i) cannot reach or (ii) can overcome the mechanical damping. In the first case, the electrical damping must be pushed to the maximum value in order to maximize the power. However, in this case, the harvester does not work efficiently since the power will always be lower than the maximum allowable for the system. In this second case (Figures 8 and 7), the system results bounded by the mechanical damping, and the power generation has two peaks when cE= cM. If the electrical damping is pushed to overcome the mechanical, the total damping injected in the system will excessively reduce the amplitude and lower the power generation.

Figure 7 
						Normalized power generation vs. dimensionless frequency (ΩM) and cut-off frequency (ΩE)
Figure 7

Normalized power generation vs. dimensionless frequency (ΩM) and cut-off frequency (ΩE)

Figure 8 
						Normalized electrical damping (cE/cM upper) and normalized power generation (P/PMax bottom) vs. dimensionless excitation frequency (ΩM) and dimensionless cut-off frequency (ΩE). The peak power generation is obtained when cE/cM = 1
Figure 8

Normalized electrical damping (cE/cM upper) and normalized power generation (P/PMax bottom) vs. dimensionless excitation frequency (ΩM) and dimensionless cut-off frequency (ΩE). The peak power generation is obtained when cE/cM = 1

Conclusion

In this paper, a first theoretical study of a nonlinear piezoelectric harvester is provided. A simple model is developed in which piezoelectric coupling is treated as a linear dashpot added to a nonlinear Duffing oscillator. The main result supports that the power generation is bounded by the mechanical damping for both linear and nonlinear harvesters. However, in the nonlinear case the power generation is spread out over a wider bandwidth.

A more accurate model is made to study the behavior of a bridge-shaped nonlinear harvester working in d33-mode. The direct influence of an external load resistor is included to consider a more accurate nonlinear coupling effect instead of the linear electrical damping employed in the first model. The sectional behavior of the beam is studied by means of Classical Lamination Theory specifically modified to introduce the piezoelectric coupling and nonlinear Green-Lagrange strain tensor. A lumped model is built through Rayleigh–Ritz method and is solved in the nonlinear regime by means of HBM. By solving the nonlinear FRF, the nonlinear equivalent stiffness and damping can be identified. This second model is suitable for predicting the response of a generic piezoelectric nonlinear harvester with arbitrary excitation frequency and external load.

Acknowledgments

Giacomo Gafforelli thanks Prof. Sang-Gook Kim and the Micro & Nano Systems Laboratory for the opportunity to collaborate and for being hosted as visiting Student at MIT.

Giacomo Gafforelli and Alberto Corigliano thanks Eniac joint undertaking, project Lab4MEMS, grant n°325622, for partial funding this research.

References

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Published Online: 2014-07-11
Published in Print: 2014-12-01

©2014 by De Gruyter

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