Nonlinear resonances of electrostatically actuated nanobeam
Canchang Liu^{1} , Shuchang Yue^{2} , Yingzi Xu^{3}
^{1, 2, 3}School of Transportation and Vehicle Engineering, Shandong University of Technology, Zibo, 255049, China
^{1}Corresponding author
Journal of Vibroengineering, Vol. 16, Issue 5, 2014, p. 24842493.
Received 23 October 2013; received in revised form 2 May 2014; accepted 7 June 2014; published 15 August 2014
JVE Conferences
Nonlinear response of electrostatically actuated nanobeam nearhalf natural frequency is studied by considering the nonlinearities of the large deformation, electrostatic force and Casimir effect. A firstorder fringe correction of the electrostatic force, large deformation, viscous damping, and Casimir effect are included in the dynamic model. The dynamics of the resonator are investigated by using the method of multiple scales in a direct approach to the problem. The sufficient conditions of guaranteeing the system stability and a saddlenode bifurcation are studied. The influences of large deformation, damping, actuation, and fringe effect on the resonator response are studied. The peak amplitude of the primary resonance is given in the paper. Numerical simulations are conducted for uniform nanobeam.
Keywords: nanobeam, nonlinear vibration, Casimir effect, electrostatic force.
1. Introduction
Microelectromechanical systems (MEMS) devices have been investigated thoroughly in the literature for their potential to build high sensitive sensors [1], probes [2], filters [3], and resonators [46]. MEMS devices have several advantages that are related to their fabrication technology allowing them to be compatible with the complementary metal oxide semiconductor (CMOS) processes [7, 8]. This advantages result into low power consumption, lower cost [9], increasing manufacturability and reliability, and enabling single chip solutions. Resonators made of simplysimply supported beam have been modeled and measured by various research groups [1011].
Nano beams have long been considered ideal building blocks for nanoelectromechanical systems’ (NMES) devices because of their superior electromechanical properties. Some of the NMES devices can be simply modeled as cantilevers or fixedfixed beams hanged over an infinite conductive substrate. These slender nano beams are excited via electrostatic or magnetomotive forces. As the excitation magnitude increases, nanotube resonators display distinctive nonlinear characteristics due to the relatively small dimensions of nanodevices. The effective resonance bandwidth of such devices can be altered due to the presence of nonlinearities [12]. Some nano beams can transform a planar motion into a motion of whirling [13]. These nonlinear behaviors may have detrimental effect on the nanodevices.
The stability of the nonlinear systems and the types of nonlinearities are highly sensitive to physical parameters, initial amplitude, and excitation frequency [5, 6, 14]. It is important to identify bifurcation points and bifurcation parameters in order to design and control systems under parametric excitation [14, 15]. A doublesided electro mechanically driven nanotube resonator taking into account the Van der Waals force has been investigated [16]. An energybased method has been used to create analytical relationships for the steadystate amplitude of the nanotube as a function of driving frequency and excitation voltage. The nonlinear response of electrostatically actuated cantilever beam microresonators nearhalf natural frequency was analyzed by considering the nonlinearities of the forces of electrostatic and Casimir [17]. Reduced order model analysis of frequency response of AC near half natural frequency electrostatically actuated MEMS cantilever was studied.
Optical experimental investigation of movable microsystem components was studied by using timeaveraged holography. A deeper insight into computational and experimental interpretation of timeaveraged MEMS hologram was provided by the analytical results between parameters of the chaotic oscillations and the formation of timeaveraged fringes [18].
Nonlinearities play a significant role in nano scale. The nonlinearities arise from a number of sources such as large deflections (geometric nonlinearities), electrostatic actuation, and Casimir effect. These slender nano beams are suspended over a trench and excited via electrostatic or magnetomotive forces. Nano beams resonators display distinctive nonlinear characteristics due to the relatively small dimensions of nano beams. Electrostatic actuation can create a variety of nonlinear parametric resonances depending on system parameters, excitation frequency, and excitation voltage.
The nonlinearities of the large deformation, electrostatic force and Casimir effect are taken into account in the analysis of the nonlinear response of electrostatically actuated nanobeam nearhalf natural frequency. The firstorder fringe correction of the electrostatic force, large deformation, viscous damping, and Casimir effect are included in the model. The method of multiple scales is used directly in the analysis of the partialdifferential equation of motion and boundary conditions of the resonator. The sufficient conditions for the stability of the system and a saddlenode bifurcation are given. The influences of large deformation, damping, actuation, and fringe effect on the resonator response are discussed. Numerical simulations are conducted for uniform nanobeam.
2. Partialdifferential equation of motion
A flexible nanobeam suspended over a grounded substrate is considered (Fig. 1). The beam is electrostatically actuated by applying an alternating voltage between the beam and the underlying plate. This paper investigates the case in which there is no DC polarizing voltage and with only the AC voltage present. The AC voltage will still contribute to the static voltage component. In addition to the electrostatic force, viscous damping and Casimir effect are considered. The length of the beam is relatively large compared to the width and thickness. Therefore, EulerBernoulli hypothesis holds. Considering the nonlinear vibration of the system, the partialdifferential equation of motion and boundary conditions can be written as [17, 19]:
$+\frac{{\epsilon}_{0}W}{2}\frac{V{\left({t}^{\text{'}}\right)}^{2}}{{\left(gw\right)}^{2}}\left(1+0.65\frac{gw}{W}\right),$
where $w(x,t\text{'})$ is the transverse displacement of the beam. $x$ and $l$ are longitudinal coordinate and beam's length, respectively. $E$, $A$, $I$, and $\rho $ are Young’s modulus, crosssectional area, cross sectional moment of inertia, and material density, respectively. ${b}^{*}$ is the coefficient of viscous damping per unit length. $W$ is the beam width, g is the initial gap between the beam and ground electrode, and $V$ is the applied voltage. $\hslash =\text{1.055\xd7}{\text{10}}^{\text{34}}\mathrm{}\text{Js}$ is Planck’s constant. $c=\text{2.998\xd7}{\text{10}}^{\text{8}}$ ms^{}^{1} is the speed of light.
Fig. 1. Schematic of an electrically actuated nanobeam
Dimensionless variables are now introduced:
where $u$, $z$, and $t$ are the dimensionless displacement of beam, dimensionless longitudinal coordinate, and dimensionless time, respectively. The dimensionless equation of the motion and boundary conditions are written as:
For a simplysimply supported (SS) nanobeam:
For a clampedclamped supported (CC) nanobeam:
where:
Considering $\alpha $, $\delta $, $\beta $, $f$ and $b$ to be small parameters, the influences of the Casimir effect, excitation force, fringe correction, and damping are taken as weak terms. Expanding around $u=$ 0 of the righthand side of Eq. (3), retaining the terms up to the third power of $u$, and setting all these terms to a slow scale by multiplying them by $\epsilon $ a small dimensionless bookkeeping parameter, one obtains:
$+\epsilon \delta \left[\left(1+f\right)+\left(2+f\right)u+\left(3+f\right){u}^{2}+\left(4+f\right){u}^{3}\right]{V}^{2}\left(t\right).$
A firstorder expansion of the dimensionless displacement $u$ can be written as:
where ${T}_{0}=t$ is a fast time scale and ${T}_{1}=\epsilon t$ is a slow time scale. Substituting Eq. (7) and the time derivatives into Eq. (6) and equating coefficients of like powers of $\epsilon \text{,}$ the following approximation equations and boundary conditions are written as:
For the simplysimply supported nanobeam:
For the clampedclamped supported nanobeam:
$+\delta \left[\left(1+f\right)+\left(2+f\right){u}_{0}+\left(3+f\right){u}_{0}^{2}+\left(4+f\right){u}_{0}^{3}\right]{V}^{2}\left({T}_{0}\right).$
For the simplysimply supported nanobeam:
For the clampedclamped supported nanobeam:
where ${D}_{n}=\partial /\partial {T}_{n}$, $n=$0, 1, 2,…. The first order approximate solution of Eq. (8) can be written as:
The dimensionless voltage is considered as [17]:
where ${\mathrm{\Omega}}_{}^{*}$ is the dimensionless frequency of excitation given by:
The resonance when excitation frequency is near half the natural frequency is investigated. The excitation frequency can be written as:
where $\sigma $ is a detuning parameter. The square of the voltage $V$ is given by [17]:
Substituting Eqs. (14) and (18) into Eq. (11), the secular terms are collected and set equal to zero. One can notice that there are additional secular terms for the excitation frequencies nearhalf natural frequency. By using the solvability condition and stating that the righthand side to be orthogonal to every solution of the homogenous problem Eq. (11), one obtains:
$+3\beta {g}_{4kk}{A}_{k}^{2}{\stackrel{}{A}}_{k}+\frac{1}{2}{C}_{1}{g}_{0kk}{e}^{i\sigma {T}_{1}}+{C}_{3}{g}_{2kk}{A}_{k}{{A}^{\text{'}}}_{k}{e}^{i\sigma {T}_{1}}+\frac{1}{2}{C}_{3}{g}_{2kk}{A}_{k}^{2}{e}^{i\sigma {T}_{1}}=0,$
where:
${g}_{4kk}={\int}_{0}^{1}{{\varphi}^{\u2033}}_{k}{\varphi}_{k}dz{\int}_{0}^{1}{{\varphi}^{\text{'}}}_{k}^{2}dz.$
Expressing ${A}_{k}$ in polar form:
Separating the real and imaginary parts of the equation of the secular terms, the amplitude ${a}_{k}$ and phase ${\gamma}_{k}$ of the response is governed by the following polar form of modulation equations:
where:
${v}_{k}=\frac{3(20\alpha +{C}_{4}){g}_{3kk}+3\beta {g}_{4kk}}{8{\omega}_{k}{g}_{1kk}},{\sigma}_{k}=\frac{(2{\omega}_{k}\sigma +4\alpha +{C}_{2})}{2{\omega}_{k}}.$
Steady state solutions of Eq. (1) for the primary resonance response correspond to the fixed points of Eqs. (21) and (22), which can be obtained by setting ${D}_{1}{a}_{k}={D}_{1}{\gamma}_{k}=\text{0}$. That is:
From Eqs. (23) and (24), the frequencyresponse equation is obtained:
The amplitude of the response is functions of the external detuning and the amplitude of the excitation.
Let ${E}_{k}={a}_{k}^{2}$, Eq. (25) can be written as:
The derivative of Eq. (25) with respect to $\sigma $ yields [20]:
Along the resonance curve, we consider the peak of the resonance. At this point, with the drive held fixed:
This implies that at the peak of the resonance:
Substituting this equation into Eq. (24), one can finds that $\mathrm{c}\mathrm{o}\mathrm{s}\left({\gamma}_{k}\right)=$0. Assumed that ${\varsigma}_{k}{a}_{k}^{2}+{F}_{k}\ne \text{0}$, one yields:
Then, the peak amplitude of the primary resonance ${a}_{k\mathrm{m}\mathrm{a}\mathrm{x}}$ can be written as:
The peak amplitude of the primary resonance is functions of the damping, the external detuning and the amplitude of the excitation.
The stability of the solutions is determined by the eigenvalues of the corresponding Jacobian matrix of Eq. (6). The corresponding eigenvalues are the roots of:
where:
${n}_{k}=\frac{{F}_{k}{\varsigma}_{k}{a}_{k}^{2}}{{\varsigma}_{k}{a}_{k}^{2}+{F}_{k}}{\mu}_{k}^{2}+\frac{{\sigma}_{k}+{v}_{k}{a}_{k}^{2}}{{\varsigma}_{k}{a}_{k}^{2}+{F}_{k}}\left({v}_{k}{\varsigma}_{k}{a}_{k}^{4}+{F}_{k}{\sigma}_{k}+3{v}_{k}{a}_{k}^{2}{F}_{k}{\sigma}_{k}{\varsigma}_{k}{a}_{k}^{2}\right).$
The sum of the two eigenvalues is –${m}_{k}$. If ${m}_{k}<$0, it means at least one of the eigenvalues will always have a positive real part. The system will be unstable. If ${m}_{k}=$0, it means a pair of purely imaginary eigenvalues and hence a Hopf bifurcation may occur. If ${m}_{k}>$0, the sum of two eigenvalues is always negative, and accordingly, at least one of the two eigenvalues will always have a negative real part. Based on the analyses mentioned above, the sufficient conditions of guaranteeing the system stability are [14]:
Unstable periodic solutions corresponding to a saddle is:
The value of $f\left({\sigma}_{k}\right)$ is positive value when there is no solution of equation $f\left({\sigma}_{k}\right)=0$:
where a saddlenode bifurcation occurs.
3. Case study
The behavior of an electrostatically actuated simplysimply and clampedclamped supported nanobeam is investigated. The nanobeam is modeled as an EulerBernoulli. Table 1 gives the common boundary conditions for the transverse vibration of beams.
The nonlinearities arise from the large deformation of structure is considered. The electrostatic and Casimir forces acting on the resonator induce nonlinear resonances. Parametric coefficients are found in both linear and nonlinear terms within the governing equation. The model also includes firstorder fringe correction of the electrostatic field. The case of uniform beams is considered. Table 2 gives values of the physical characteristics of a typical nanobeam.
Nonlinearities play a significant role in nano scale. In the work, the nonlinearities arise from a number of sources such as large deflections, electrostatic actuation, and Casimir effect. As the excitation magnitude increases, nanobeam resonators display distinctive nonlinear characteristics due to the relatively small dimensions of nanobeam. Electrostatic actuation can create a variety of nonlinear parametric resonances depending on system parameters, excitation frequency, and excitation voltage. When the separation of surfaces is larger than 20 Nm and less than 1000 Nm, Casimir effects occur [21]. In this work, such gap distances are considered. The influence of the large deflections, electrostatic actuation, and Casimir effect to the nonlinear terms is relative to the distance between the nanobeam and the substrate. Tables 3 and 4 shows comparison of the value of the nonlinear terms among the Casimir effect, electrostatic actuation, and large defections of the SS and CC beam. There are small changes for the values of nonlinear terms of the Casimir effect and electrostatic actuation when the gap between the nanobeam and the substrate becomes large. However, the nonlinear term induced by the large deformation changes on the contrary.
Table 1. Common boundary conditions for the transverse vibration of beams
End conditions of beam

Mode shape

Value of $\xi $

Simplysimply supported

$\mathrm{s}\mathrm{i}\mathrm{n}\left(\frac{\xi}{l}x\right)$

$\pi $

Clampedclamped supported

$\left[\mathrm{c}\mathrm{o}\mathrm{s}\mathrm{h}\left(\frac{\xi}{l}x\right)\mathrm{c}\mathrm{o}\mathrm{s}\left(\frac{\xi}{l}x\right)\right]\upsilon \left[\mathrm{c}\mathrm{o}\mathrm{s}\mathrm{h}\left(\frac{\xi}{l}x\right)\mathrm{c}\mathrm{o}\mathrm{s}\left(\frac{\xi}{l}x\right)\right]$

4.730

where $\upsilon =\frac{\mathrm{c}\mathrm{o}\mathrm{s}\mathrm{h}\xi \mathrm{c}\mathrm{o}\mathrm{s}\xi}{\mathrm{s}\mathrm{i}\mathrm{n}\mathrm{h}\xi \mathrm{s}\mathrm{i}\mathrm{n}\xi}.$

Table 2. Physical characteristics of a nanobeam
Parameter

Symbol

Value

Beam width

$W$

500 Nm

Beam length

$l$

30 μm

Beam thickness

$h$

300 Nm

Initial gap distance

$g$

200 Nm

Material density

$\rho $

2330 kg/m^{3}

Young’s modulus

$E$

169 GPa

Peak AC voltage

$V$

2.0 V

Table 3. Comparison of the value of nonlinear terms among the Casimir effect, electrostatic actuation and large deformation of the first mode of SS beam
$g$, Nm

Casimir effect

Electrostatic actuation

Large deformation

50.0000

10.1063

17.4783

–0.6169

70.0000

1.8791

6.4104

–1.2090

90.0000

0.5348

3.0353

–1.9986

110.0000

0.1961

1.6730

–2.9856

130.0000

0.0851

1.0199

–4.1699

150.0000

0.0416

0.6680

–5.5517

170.0000

0.0222

0.4618

–7.1308

190.0000

0.0128

0.3328

–8.9073

210.0000

0.0077

0.2480

–10.8813

Fig. 2 shows the primary resonance curves of the first mode of simplysimply supported nanobeam for three different sets of the excitation voltages. There is no jump and hysteresis phenomenon when ${V}_{0}=$1.5 V. The saddle node bifurcation and jump phenomenon can be eliminated by choosing certain numerical values of the excitation voltages. Three solutions exist in the cases of ${V}_{0}=$2.0 V and ${V}_{0}=$2.1 V. The jump phenomenon presents. The peak amplitude of the primary resonance response at ${V}_{0}=$1.5 V is the smallest one among the three cases.
Fig. 3 shows the primary resonance curves of the first mode of simplysimply supported nanobeam for considering the effect of the nonlinear term or not. There is no jump and hysteresis phenomenon when the effect of the nonlinear term is $\beta =$0. Three solutions exist in the cases of considering the effect of the nonlinear term $\beta =$2.6667. The jump phenomenon presents. There is a different vibration behavior for the nonlinear vibration of the nonlinear system. So, the effect of the nonlinear term to the vibration behavior should be taken into account in the analysis of the large deformation of the nanobeam.
Table 4. Comparison of the value of nonlinear terms among the Casimir effect, electrostatic actuation, and large deformation of the first mode of CC beam
$g$, Nm

Casimir effect

Electrostatic actuation

Large deformation

50.0000

9.8517

17.0380

–0.7568

70.0000

1.8318

6.2489

–1.4832

90.0000

0.5214

2.9588

–2.4519

110.0000

0.1912

1.6308

–3.6627

130.0000

0.0829

0.9942

–5.1157

150.0000

0.0405

0.6512

–6.8108

170.0000

0.0217

0.4501

–8.7481

190.0000

0.0124

0.3244

–10.9276

210.0000

0.0075

0.2417

–13.3492

Fig. 2. Amplitudefrequency of primary resonance curves of the first mode of simplysimply supported nanobeam for three different sets of the excitation voltages
Fig. 3. Amplitudefrequency curves of primary resonance of the first mode of simplysimply supported nanobeam for considering the nonlinear term of large deformation or not
Fig. 4. Critical curve of saddle burfurcation of the simplysimply supported nanobeam
Fig. 5. Jump curves of the simplysimply supported nanobeam
Fig. 6. Peak amplitude of the primary resonance curves of the first mode of simplysimply supported nanobeam for three different sets of the initial gap between the beam and ground electrode
The sum of the two eigenvalues is always negative when ${m}_{k}>$0, and accordingly, one of the two eigenvalues must have at least a negative real part. When $f\left({\sigma}_{k}\right)=\text{0}$, the other eigenvalue is zero where a saddlenode bifurcation occurs. We utilize Eq. (35) to study variation of the response amplitude with the excitation voltage. The critical curve of saddle burfurcation of the simplysimply supported nanobeam is illustrated in Fig. 4. When ${n}_{k}>$0, the vibration system may be stable. However, When ${n}_{k}<$0, the vibration system is unstable. Stable and unstable regions are shown in the figure.
The variation of the response amplitude with the frequency detuning parameter $\sigma $ and the excitation amplitude is studied by utilizing Eq. (25). Fig. 5 illustrates the frequencyresponse curve of the simplysimply supported nanobeam when ${\sigma}_{A}<{\sigma}_{B}$, which only a stable trivial solution exists. As $\sigma $ is increased, the trivial solution loses stability at point C and gives rise to a branch of stable periodic solutions. The amplitude of these stable solutions increases as $\sigma $ is increased further towards point C. At point C, the periodic solution loses stability through a saddlenode bifurcation, and the response amplitude jumps down to point D where only trivial solutions exist. Increasing beyond point D leads only to the stable trivial solutions.
Fig. 6 shows the peak amplitude of the primary resonance curves of the first mode of simplysimply supported nanobeam for three different sets of the initial gap between the beam and ground electrode. It is easily noted that ${a}_{max}$ decreases significantly as the initial gap between the beam and ground electrode increases. A larger initial gap can relatively lead to a smaller peak amplitude ${a}_{max}$. For fixed initial gap, the increase of the excited voltage can lead to the increase of the peak amplitude.
4. Conclusions
The nonlinear response of electrostatically actuated nanobeam nearhalf natural frequency is studied by considering the nonlinearities of the large deformation, electrostatic force and Casimir effect. The gap between the nanobeam and the substrate decides the values of the nonlinear terms of the Casimir effect, electrostatic actuation and large deformation. The gap distances have the different influence on the value of large deflections, electrostatic actuation, and Casimir effect. The peak amplitude decreases with the increasing of the gap distances and increases with the largening of the excited voltage. Some references are given for the analysis and control of the nano and micro nonlinear system.
The sufficient conditions guaranteeing the system stability is given. The saddlenode bifurcation is studied. The nonlinearities of large deformation, damping, actuation, and fringe effect have influences on the resonator response. The peak amplitude of the primary resonance has a relationship to the damping, the external detuning and the amplitude of the excitation.
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