Mechanical Behaviors of Electrostatic Microbeams with Nonideal Supports

Chang, Yunxia; Zhang, Qichang; Wang, Wei; Han, Jianxin

doi:https://doi.org/10.1155/2020/4507280

Shock and Vibration

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Abstract Introduction Methods Results and Discussion Conclusions Appendix Data Availability Conflicts of Interest Acknowledgments References Copyright Related Articles

Research Article | Open Access

Volume 2020 | Article ID 4507280 | https://doi.org/10.1155/2020/4507280

Mechanical Behaviors of Electrostatic Microbeams with Nonideal Supports

Yunxia Chang,^1,2Qichang Zhang ,¹Wei Wang,¹and Jianxin Han³

Academic Editor: Ömer Cívalek

Received30 Nov 2019

Revised04 Apr 2020

Accepted08 May 2020

Published17 Aug 2020

Abstract

Deviation of the actual system from the ideal supporting conditions caused by micromachining errors and manufacturing defects or the requirement of innovative design and optimization of microelectromechanical systems (MEMS) make the nonideal boundary in the micro-/nanoresonator system receive wide attention. In this paper, we consider the neutral plane tension, fringing field, and nonideal boundary factors to establish a continuum model of electrostatically driven microbeam resonators. The convergent static solution with nine-order Galerkin decomposition is calculated. Then, based on the static solution, a 1-DOF dynamic equation of up to the fifth-order of the dynamic displacement using a Taylor expansion is derived. The method of multiple scales is used to study the effect of spring stiffness coefficients on the primary frequency response characteristics and hardening-softening conversion phenomena in four cases. The various law of the system’s static and dynamic performances with the spring stiffness coefficients is obtained. The conditions for judging the hardening-softening transition are derived. So, adjusting the support stiffness values can be a measure of optimizing the resonator performance.

1. Introduction

Electrostatic microbeam resonators have the advantages of small size and light weight and are widely used in many fields, for instance, MEMS resonant sensor [1] and actuator [2]. Their small size allows sensitive systems to consume minimal energy and have low fabrication costs. However, due to the nonlinearity of the electrostatic force and the neutral plane tension, MEMS resonators can exhibit typical nonlinear dynamic characteristics. So far, the effects of nonlinearities on the static and dynamic performances of MEMS devices have been discussed in many works of literature [3–19].

But the above-mentioned works of literature only considered the ideal boundary conditions. In fact, both macro- and microstructures have errors and manufacturing defects, such as structure with elastically restrained, structure with nonuniform [20, 21], overcutting near anchor points [22], and initial deformation [23–26] of microstructures caused by residual stress. These cause the boundary conditions of the actual system to deviate from the ideal support conditions such that the displacement and rotation angle of the two fixed ends are not equal to zero. Bambill et al. [27] drew the conclusion that the characterization of real boundary conditions was much more important for microscale beams than for macroscale beams. In addition, Muthukumaran et al. [28] proposed that the boundary condition became one of the techniques responsible for the structural tuning of particular note in order to obtain a desired harmonic relation among its natural frequencies. Hence, the nonideal boundary has become a way of innovative design and optimization of electrostatic resonators [29]. Therefore, the nonideal boundary in the micro-/nanoresonator system has received wide attention from relevant scholars.

Rinaldi et al. [30] studied the boundary features of microcantilever beams through experiments. Results showed that nonclassical support boundaries could reduce the pull-in voltage of the microstructure. Rezaei et al. [31] analyzed the principal resonance behavior of piezoelectric actuated microcantilever and clamped beam under nonideal boundary conditions by using a two-dimensional multiscale method, and obtained the influence of nonideal boundary on the amplitude and frequency. Zhong et al. [32, 33] calculated the equivalent stiffness of nonideal support with fixed microbeam and microcantilever beam, respectively, and obtained the influence of nonideal boundary on vibration mode and frequency. Alkharabsheh and Younis [24] studied the fixed microarches with nonideal boundaries and compared the numerical results with experiments. Results demonstrated that nonideal boundary conditions had a significant effect on the qualitative dynamical behavior of the MEMS arch such as lowering its natural frequencies and causing unpredictable snap through or dynamic pull-in. Ekici et al. [34] used a multiscale method to study the superharmonic and subharmonic vibration of nonideal boundary microbeams. The nonideal boundary was simulated by helical spring. The conclusion was drawn that nonideal boundary conditions could cause shifting to the left or right side or no shifting in the graphs, depending on the mode numbers, axial force, deflections, and moments on the boundaries. Zeng et al. [35] studied the simulation of the nonideal boundary of the inclined supported beam. The finite element method and Galerkin method were used to study the static characteristics of the microbeam, which was in good agreement with the experimental results.

In recent years, the static and dynamic characteristics of microbeam were studied by considering nonideal support along with edge field, or other factors. In Pallay and Towfighian’s literature [29], a MEMS-parametric resonator was introduced, which used nonideal supports and electrostatic edge fields to achieve an innovative design of energy-efficient resonators. Bashma et al. [36] used the finite element method based on wavelet transform to obtain the influence of nonideal support and edge effect on static attraction voltage and first-order natural frequency of the microcantilever beam. Chuang et al. [37] obtained an approximate analytical solution to the pull-in voltage of a microcurled cantilever beam considering the nonideal boundary and edge effect. Yayli [38] investigated the lateral free vibration of microbeams under various boundary conditions on the basis of the gradient theory of elasticity. Lishchynska et al. [39]established a model for predicting the static behavior of an electrostatic microcantilever beam considering the residual stress gradient and nonideal anchors. The analytical results were in good agreement with the experimental results. Tadi Beni et al. [40] introduced the modified couple stress theory, in conjunction with the MAD solving method, to investigate the effect of the Casimir attraction, Elastic boundary conditions, and size dependency on nonlinear pull-in behavior of the supported beam. Shojaeian et al. [41] studied the electromechanical instabilities of micro-/nanobeams with an initial curved shape and subjected to the electrostatic field and Casimir intermolecular force using a modified couple stress theory. However, they seldom analyze their effects on dynamic response.

The purpose of this article is to explore the influence law of nonideal boundaries on the dynamics of resonators and to provide theoretical support for the optimal design of MEMS. In this paper, a continuum model of electrostatic microbeam resonators is established. The convergent static solution with nine-order Galerkin decomposition [42] is calculated. It is used to investigate the influences of nonideal boundaries on the system’s static characteristics. Based on the static solution, a 1-DOF dynamic equation of up to five orders of the dynamic displacement using Taylor expansion is derived. This quintic equation is a powerful complement to the cubic equation. Then, the method of multiple scales [43] is used to study the effects of nonideal boundaries on the primary frequency response characteristics and hardening-softening conversion phenomena in four cases. The various law of the system’s static and dynamic performances with the spring stiffness coefficients is obtained. The details are going to be discussed in the following sections.

The paper is organized as follows: an introduction including the literature review and motivation of the research, equation of motion and methods, results and discussion, and lastly, conclusions.

2. Equation of Motion and Methods

Due to micromachining errors and manufacturing defects or the requirement of innovative design, the displacements and rotation angles of the two fixed ends of the microbeam are not equal to zero. To simulate and quantify these small rotation angles and deflections, artificial rotational and translational springs are introduced [24, 30–33, 44]. In this paper, only symmetrical springs are considered. That is, the stiffness coefficients of left and right springs, and , are the same. The schematic diagram is shown in Figure 1. With the application of DC and AC voltage across the beam and electrode backplate, a distributed electrostatic force between the beam and electrode is generated to deform and vibrate the microbeam.

The first-order fringing field correction of electrostatic force per unit length, namely, Palmer model [45, 46], is expressed as follows:

Hence, the governing equation per unit length along the microbeam [24, 32, 42, 47] can be given by the following equation:where is the position along the microbeam length, represents transverse deflection, is the moment of inertia of the cross section (, where and represent, respectively, the microbeam’s width and thickness), and are, respectively, the microbeam’s length and the initial gap, and represent, respectively, the viscous damping per unit length and the material density, is the dielectric constant of the gap medium, is time, represents the effective Young’s modulus with for a wide microbeam and for a narrow microbeam , in which represents Young’s modulus while represents the Poisson’s ratio.

The system’s nonideal boundary conditions are given by the following equation:where and represent the rotational and translational stiffness.

For convenience, introduce the following nondimensional variables:where . Thus, the governing equation of motion and the system’s boundary conditions become as follows:where , , , , , , , .

Galerkin method is a powerful method, which is capable of handling static and dynamic problems of nonlinear systems. It is limited by solving the mode shapes. See Appendix A for the expression of the mode shapes.

In a microbeam resonator, the DC voltage causes the microbeam to form a new static equilibrium position, and the AC voltage excites the microbeam to vibrate around the equilibrium position. Thus, microbeam deflection can be given by the following equation:where the static deflection due to the DC voltage is denoted by , and the dynamic deflection due to the AC voltage is denoted by .

To calculate the static deflection, set the time-varying terms in (5) equal to zero and obtain the following:

Here the static deflection is expressed as , where is the ith generalized coordinate (here is a constant), is the ith mode shape, and i is the order of Galerkin discreteness. Substituting the expression into (9) and applying the Galerkin method yield the system of nonlinear algebraic equations.

Substituting the above (8) and (9) into (5), setting , omitting the parameter exciting terms, and keeping the fifth power terms about , yield the following:

Omitting the dynamic forcing term, neglecting damping term, and keeping only linear terms about in (10) yield the following:

Let , where is mode shape and is the frequency of the system. Then, one can obtain the frequency of the system for various conditions.

3. Results and Discussion

Next, this paper analyzes the static and dynamic characteristics of the systems.

3.1. Static Analysis

In this section, the influences of the support spring coefficients on the static deflection and the natural frequency of the system are discussed by the numerical solution.

3.1.1. Convergence Analysis

Because the microbeam maintains symmetric shapes during motion, only symmetric modes (namely the modes when i equals even number) are considered to verify the convergence using the data in literature [4].

Setting regardless of fringing field effect, the outcome obtained by the first five symmetric modes (namely, i = 9) is shown in Figure 2. Compared with Nayfeh et al. [4], the convergence effect is good, and the research in this paper is feasible.

3.1.2. Static Deflection

Next, calculate the static deflection of a microbeam with the parameters listed in Table 1 and the various spring stiffness coefficients and .

The effects of rotational stiffness on the system’s static features are discussed by changing the value of rotational stiffness, as shown in Figure 3. The red dot dash line is the corresponding stable value when the rotational stiffness is infinite. The deflection-DC voltage curve is divided into the upper branch and lower one. The solid line of the lower branch represents the steady state, and the black dotted line of the upper branch represents the unstable state. Only the stable values make sense. With the increase of before pull-in phenomenon occurs, the static deflection corresponding to the same voltage decreases, the static pull-in voltage increases and eventually reaches the stable value.

(a)

(b)

Figure 4 shows the effect of the translational stiffness on the static characteristics of the system. The red dot dash line is the corresponding stable value when the translational stiffness is infinite. As the goes up before pull-in phenomenon occurs, the static deflection corresponding to the same voltage goes down, the static pull-in voltage goes up, and eventually reaches the stable value.

(a)

(b)

In a word, with the growth of support stiffness (refers to rotational stiffness and translational stiffness) before pull-in phenomenon occurs, the static deflection corresponding to the same voltage goes down, the static pull-in voltage goes up, and eventually reaches a stable value.

3.1.3. Natural Frequency

The influence of the rotational coefficient on the first-order frequency is shown in Figure 5. The red dot dash line is the corresponding stable value when the rotational stiffness is infinite. In the case of the same DC voltage, the greater the rotational stiffness is, the higher the first-order frequency is until it finally tends to the stable value.

(a)

(b)

Figure 6 shows the effect of translational stiffness on first-order frequency by applying the numerical method. The red dot dash line is the corresponding value when the translational stiffness is infinite. In the case of the same DC voltage, the greater the translational stiffness is, the higher the first-order frequency is until it eventually tends to the stable value.

(a)

(b)

In short, as the support stiffness (refers to rotational stiffness and translational stiffness) goes up, the first-order natural frequency increases, until it eventually tends to the stable value.

3.2. Dynamic Analysis

Introducing and applying the Galerkin method, obtain the following dynamic equation via equation (10):where , represents the corresponding Jth derivative of the function , is the corresponding Jth derivative of the mode shape .

See Appendix B for the detailed solving process by the method of multiple scales.

Hence, frequency response equation is obtained as follows:where

The peak amplitude is as follows:

It is found through analysis that is the function of DC voltage and AC voltage as independent variables for a given microbeam resonator.

The backbone curve is as follows:

When , the nonlinearity has a hardening effect that tends to bend the frequency response curves to higher frequencies. When , the nonlinearity has a softening effect, which tends to bend the frequency response curves to lower frequencies.

When , a real threshold can be obtained as follows:

If the real threshold exists and satisfies the following condition, the system has a hardening-softening effect transition phenomenon.

3.2.1. Convergence Verification

Assuming that the maximum microbeam deflection is given by , where is the approximate solution of the static deflection obtained by the nine-order Galerkin discretization. Given the voltage value, calculate the system’s response, as shown in Figure 7.

It can be seen from Figure 7 that the regularity trend of the frequency response curve is consistent and the convergence is good. Therefore, the above-mentioned approximate solution of maximum microbeam deflection can be used to determine the vibration characteristics of the system.

3.2.2. Softening and Hardening Effects

Nonlinear hardening and softening characters have been reported in many works of literature. The system’s nonlinear softening and hardening characteristics are determined by parameter , which is determined by the DC voltage , static deflection , and natural frequency . Furtherly, since the static displacement and natural frequency depend on and the boundary support stiffness values, the parameter is ultimately affected by the DC voltage and the boundary support stiffness values. So, the boundary support stiffness values do affect the softening and hardening characteristics of the system.

To investigate how the nonideal support stiffness to affect the system's frequency response curve in this section, there are four cases to discuss as seen in Table 2.

(1) Comparison of Case 1 and Case 2. The stiffness values in Case 1 are used to simulate the ideal fixed boundary system, and the data in Case 2 simulate a nonideal boundary system. Other physical parameters refer to Table 1.

For a given electrostatic microbeam resonator in Cases 1 and 2, the parameter is the function of the DC voltage. Hence, Figure 8(a) shows the relationship between the parameter p₃ and DC voltage under different boundary conditions. As the DC voltage increases, the parameter decreases. The dotted line is the boundary of the hardening and softening features. As shown in Figure 8(a), when , hardening characteristics that ideal boundary system demonstrates are predicted. According to Figure 7, this prediction is true. Meanwhile, the nonideal boundary system at the same DC voltage also shows hardening characteristics.

(a)

(b)

It can be seen clearly from Figure 8(b) that the nonideal boundary has an influence on the softening and hardening features. The abscissa value corresponding to the intersection point is smaller than the value of . Approximate maximum deflection at the time of the transition can be obtained according to the formula , as shown in Figure 9. Obviously, the nonideal boundary reduces the critical deflection of the transition. Therefore, under the same DC voltage, the transition occurs first.

For the sake of illustration, select the three groups V_D corresponding to the dotted line in the above Figure 8(b) to analyze the amplitude-frequency response. Assume that the dimensionless damping coefficient is .

When , the real threshold of the ideal boundary system exists, and the system is in hardening effect region. Nevertheless, whether there is a hardening-softening effect, conversion needs to be furtherly analyzed and judged by the second condition of equation (19). When is given, the system’s excitation amplitude f₁ depends on the AC voltage , so the parameter in equation (19) is actually determined by the parameter . Therefore, given a suitable to meet with the condition of equation (19), there is a hardening-softening effect conversion in the ideal boundary system, as shown in Figure 10(b). In this case, the nonideal boundary system has a hardening-softening conversion phenomenon, but the maximum deflection of the transition is less than that of the ideal boundary system, as shown in Figure 10(a).

(a)

(b)

When , the two boundary systems behave differently. The real threshold of the ideal boundary system exists, and there is a hardening-softening conversion if a suitable to meet with the condition of equation (19) is selected, as shown in Figure 11(b). While the real threshold of the nonideal boundary system does not exist, the system shows a softening effect and there is not a hardening-softening conversion, as shown in Figure 11(a).

(a)

(b)

When , the real threshold of both boundary systems do not exist. So there are no hardening-softening conversion phenomena in both boundary systems. Both boundary systems show a softening effect, as shown in Figure 12.

(a)

(b)

In summary, the laws of the dynamic performance of the system with the spring stiffness coefficients are obtained.(i)Under the same DC voltage, as the spring stiffness goes down, the vibration frequency of the system becomes smaller and the amplitude becomes larger.(ii)If the real threshold does not exist, there will be no hardening-softening transition. If the real threshold exists and is satisfied, the system will have a hardening-softening transition phenomenon.(iii)If there is hardening-softening transition, the nonideal boundary reduces the critical deflection of the transition. So, under the same DC and AC voltage, the transition occurs first.

(2) Case 3. In order to study the influence of translational spring on the system’s softening and hardening characteristics, the spring stiffness coefficient values are taken as follows:, . Similarly, select the three groups V_D to analyze the amplitude-frequency response. They are 1.5 V, 2.8 V, and 3.4 V, respectively.

When , , the real threshold exists, but does not meet with (19), and the system is in the hardening effect region. So, the system shows hardening characteristic, as shown in Figure 13(a). Likewise, the system with also shows hardening characteristics, as shown in Figure 13(b).

(a)

(b)

When , , the real threshold does not exist and the system is in softening effect region. So the system shows softening characteristic, as shown in Figure 14(a). However, the real threshold of the system with exists and the system is in hardening effect region. So there is hardening-softening conversion if a suitable to meet with the condition of (19) is selected, as shown in Figure 14(b).

(a)

(b)

When , , the real threshold does not exist and the system is in the softening effect region. So the system shows softening characteristic, as shown in Figure 15(a). Likewise, the system with also shows softening characteristics, as shown in Figure 15(b).

(a)

(b)

In a word, the laws of the dynamic performance of the system with the translational spring stiffness coefficient are the same as that of the comparison of Case 1 and Case 2.

(3) Case 4. In order to study the influence of rotational spring on the system’s softening and hardening characteristics, the spring stiffness coefficient values are taken as follows: . Similarly, select the three groups V_D to analyze the amplitude-frequency response. They are 2 V, 2.6 V, and 2.75 V, respectively.

When the real threshold exists and the system is in the hardening effect region. So there is hardening-softening conversion if a suitable to meet with the condition of (19) is selected, as shown in Figure 16(a). Likewise, the system with shows hardening-softening conversion if a suitable to meet with the condition of (19) is selected, for example . However, because selected in Figure 16(b) is too small, the system with only shows the hardening characteristic.

(a)

(b)

When , , the real threshold does not exist and the system is in the softening effect region. So the system shows softening characteristics, as shown in Figure 17(a). However, the real threshold of the system with exists and the system is in the hardening effect region. So there is hardening-softening conversion if a suitable V_A to meet with the condition of (19) is selected, as shown in Figure 17(b).

(a)

(b)

When , , the real threshold does not exist and the system is in the softening effect region. So the system shows softening characteristic, as shown in Figure 18(a). Likewise, the system with also shows softening characteristics, as shown in Figure 18(b).

(a)

(b)

In a word, the laws of the dynamic performance of the system with the rotational spring stiffness coefficient are the same as that of the comparison of Case 1 and Case 2, too.

4. Conclusions

In this paper, the Galerkin method and the method of multiple scales are used to theoretically investigate the mechanical behavior of electrostatic microbeam resonator with nonideal supports under forced excitation and study the feasibility of increasing vibration amplitude and reducing excitation voltage. The following main conclusions can be drawn.(i)The laws of the system’s static performances with the spring stiffness coefficients are obtained; with the growth of support stiffness before pull-in phenomenon occurs, the static deflection corresponding to the same voltage goes down, the static pull-in voltage increases, and eventually reaches a stable value.(ii)The laws of the system’s dynamic performances with the spring stiffness coefficients are obtained. Under the same DC voltage, as the support stiffness decreases, the vibration frequency of the system becomes smaller and the amplitude becomes larger.(iii)The conditions for judging the hardening-softening transition are derived. If the real threshold does not exist, there will be no hardening-softening transition. If the real threshold exists and is satisfied, the system will have a hardening-softening transition phenomenon.(iv)If there is hardening-softening transition, the nonideal boundary reduces the critical deflection of the transition. So, under the same DC and AC voltage, the transition occurs first.

The analysis provides a theoretical basis for implementing energy-saving resonators by adjusting the support stiffness values. The dynamic design of specific parameters can be further carried out to achieve frequency, amplitude regulation, and vibration form regulation.

So far, many studies have focused on the effect of Casimir gravity and size effect on the mechanical behavior of the system. The results show that both of them have a significant influence on the static and dynamic performance of the system. Then, the size effect on the system with nonideal boundary and Casimir force can be our next concern.

Appendix

A. Mode Shapes of Microbeams with Nonideal Supports

The mode shape of the linear undamped straight beam is expressed by the following equation:where

Eventually, each mode shape needs to be normalized by multiplying it by the constant ,where makes the maximum value of the corresponding mode shape equal to 1.

B. Solving by the Method of Multiple Scales

Considering the terms , , scale the damping and the dynamic forcing terms as follows:

Seek an approximate solution to this equation by lettingwhere .

Introducing the following operator:where

Introducing a tuning parameter and letting , obtain the following governing equation:

Eventually, the average equation can be given by the following equation:where a represents amplitude, and β represents phase.

The approximate dynamic solution can be given by the following:where

Data Availability

The data used to support the findings of this study are included within the article, see Table 1 for details.

Conflicts of Interest

The authors declare that there are no conflicts of interest regarding the publication of this paper.

Acknowledgments

The authors are grateful for the support from the National Natural Science Foundation of China (Grant nos. 11872044, 11702192, and 11772218).

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Copyright © 2020 Yunxia Chang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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