# Analysis of Excitation and Dead Vibration Modes of Quartz Resonators

Authors: Zi-Gui Huang; Zheng-Yu Chen
Journal: Advances in Acoustics and Vibration
 (2014)

---

## Abstract

This study uses the finite element method (FEM) to analyze the excitation and dead vibration modes of two-dimensional quartz plates. We first simplify three-dimensional quartz plates with plane strain simplification and then compare the modes of the simplified three-dimensional plates to those of two-dimensional plates. We then analyze quartz vibrating elements of AT-cut plates and SC-cut plates. To understand the regularity of the resonance frequency of plates that are excitable by voltage loading, we compare the natural vibrations of quartz plates with the excitation frequency generated after the plates are excited by voltage loading.


---

## Body

## 1. Introduction

Quartz resonators are one of the passive components widely used in the computer, communication, and consumer-electronics industries; they are easily found in computers, electronic instruments, quartz watches, and mobile communication components. Quartz is a type of anisotropic piezoelectric material, and the piezoelectricity was discovered by the brothers Pierre Curie and Jacques Curie in 1880. In 1951, Mindlin expanded plate theory to include crystal plates and the discussion of the frequency of AT-cut quartz plates with consideration of the length-to-thickness ratio [1]. Bechmann then used resonance methods to obtain elastic and piezoelectric constants of different types of man-made quartz [2]. With the improvement in the calculating ability of computers and the use of finite element software, analyses of quartz plates can be found in many recent studies. Wang et al. [3, 4], Yong et al. [5], Patel et al. [6, 7], Patel and Yong [8], and Yang et al. [9] used the finite element method to analyze the piezoelectric vibrations of quartz plate and predict the Q value and equivalent electrical parameters of quartz resonators, in addition to the influence that the mesh impedances of plate grids had on transmitting sound waves.Since different cutting angles or temperature changes affect the forms of oscillation of quartz, different boundary conditions are applied in finite element analysis; the analysis results will then be discussed and compared. Generally, any structure could cause numerous types of natural vibration. One of the oscillation characteristics of quartz plates is the stable resonance frequency generated from the deformation of the quartz material caused by electrodes when applying voltage to the plates. This converse piezoelectric effect converts electrical energy into mechanical energy, and it is different from normal, natural vibrations. In this study, we evaluate the differences between the natural vibrations of quartz plates and the changes in vibration modes resulted from electric field polarization.


## 2. Finite Element Analysis on Two-Dimensional Quartz Plates

### 2.1. Setting the Size and Boundary Conditions of the Finite Element Model

A finite element analysis simulation software [10] was used in this study to analyze the vibrations of thin quartz plates. The size of the quartz resonators used in this study was 3.495 mm in length (2
a), 0.0638 mm in thickness (2
b), and 1.805 mm in width (2
c). The AT-cut and SC-cut of anisotropic piezoelectric quartz plates were considered in this paper. We set the boundary condition as the application of voltage differences to the upper and lower layers of quartz plates. Figure 1 shows the boundary condition setting of two-dimensional models.Figure 1
Boundary condition setting of two-dimensional quartz plate models.


### 2.2. Grid Layout and Frequency Convergence

Thickness shear modes are one of the vibration modes of quartz resonators. The frequencies of thickness shear modes are influenced by the thickness of quartz plates. Therefore, the thickness of grids must be sufficient to make the obtained frequency converge. In general, more grids result in a more precise value. However, to be efficient when analyzing, the number of grids should be just enough to make the frequency convergent. The models in this study come from the analysis results of the number of grids and frequency convergence in a study conducted by Huang and Chen [11].In their study, Huang and Chen found the appropriate number of grids in terms of grid convergence of the thickness of two-dimensional quartz plate models. When dividing the thickness of a quartz plate (0.0638 mm) into 10 grids, the error value (6.9342 ppm) they obtained was closer to convergence, compared to when the thickness was divided into 100 grids. Also, when dividing the length of the plate (3.495 mm) into at least 500 grids, the error value of resonance frequency they obtained dropped to under 30 ppm; the value was less compared to that obtained when dividing the length into 1000 grids. Considering the length/grid ratio, the size of each grid was obtained, and the equation was written as 3.495/500 = 6.99 × 10−3 (mm). Based on the grid size, an appropriate number of grids for the width of the plate were calculated to achieve the frequency convergence; the equation was written as 1.805/6.99 × 10−3 = 258 (grid). To attain the best frequency convergence result, we divided the length of each model into 500 grids, the width into 260 grids, and the thickness into 10 grids.


### 2.3. Simplifying Quartz Plate Models

The equations of motion for a piezoelectric plate can be obtained from the variational principle shown in(1)
∫
t
0
t
d
t
∫
V
[
(
T
i
j
,
i
-
ρ
u
¨
j
)
δ
u
j
+
D
j
,
j
δ
ϕ
]
d
V
=
0
,
where T
i
j is the stress tensor, t is the time variable, and ρ and u
j are the density and displacement vector, respectively. D
j is the electric displacement vector and ϕ is the electric potential. V is the volume of the piezoelectric plate.The piezoelectric constitutive relationships among stress, strain, electric field, and electric displacement field in a stress-charge form are expressed as(2)
T
i
j
=
c
i
j
k
l
S
k
l
-
e
k
i
j
E
k
,
S
i
j
=
1
2
(
u
i
,
j
+
u
j
,
i
)
,
D
i
=
e
i
j
k
S
j
k
+
ε
i
j
E
j
,
E
i
=
-
ϕ
,
i
,
where S
k
l is the strain tensor and E is the electric field. The tensors c
i
j
k
l, e
k
i
j, and ε
i
j are elastic constants, piezoelectric constants (coupling coefficients), and dielectric constants, respectively.The stress-strain analysis used to analyze three-dimensional models can be divided into two methods for simplification in terms of elasticity: plane stress and plane strain. For anisotropic material like quartz, 2D model based on plane strain assumption does not give accurate results [12]. In this paper, to obtain approximate accurate results for the thickness mode and flexural mode frequencies from the 2D model, the shear strain in the z direction when using the XY plane strain case and the shear strain in the x direction when using the ZY plane strain case are not taken into consideration.The plane stress is mainly used to analyze very thin quartz plates. The external force is evenly distributed through the thickness of the plates, and the stress components do not change with the direction of thickness. Therefore, there are only normal stressesσ
x and σ
z, and shear stress τ
x
z when XZ is considered as the plane in plane stress case. The values of σ
y, τ
y
x, and τ
y
z would be 0 so that the plane stress case cannot be used to discuss the thickness shear vibration modes.The plane strain is mainly applied to analyze longer pillars. The cross section of a pillar and the longitudinal force do not change with length. When thez-axis is the major axis, then the displacement along the z-axis would always be 0. Thus, there are only normal strains ε
x and ε
y and shear strain γ
x
y when XY is considered as the plane in the plane strain case. Here, strains ε
z, γ
y
z, and γ
x
z would not exist.Thickness shear modes are the main source of resonation in quartz resonators for specific cuts of quartz; they can be seen as horizontal shearing motions along thex or z direction when the normal of plane is y. Though thin plate resonators tend to apply the simplification method of plane stress, the stress and shear stress of the thickness direction are not included in a plane stress analysis. This does not meet the requirements of two-dimensional quartz plate analysis. Therefore, we used plane strain analysis to analyze the two-dimensional quartz plate and discuss the resonance characteristics of the plate’s XY plane. To simplify the plate, or to ignore the influence that z-axis had on the plane, we made the length of the z-axis much longer than those of the x- and y-axes. The XY plane of the simplified three-dimensional resonator is shown as Figure 2.Figure 2
Simplification of quartz plate model.


### 2.4. Comparison between Three-Dimensional and Two-Dimensional Quartz Plate Modes

The simplification of three-dimensional models helps to improve the analysis efficiency of the finite element method. However, according to the grid convergence information in the study conducted by Huang and Chen, the size of each grid of the model dimensions must be smaller than7
×
1
0
-
3 mm to achieve frequency convergence [11]. This could be very difficult to realize when analyzing a three-dimensional model. Considering the directional effects of the length, the width, and the thickness of a three-dimensional model produces extremely complicated oscillating curves.To compare a three-dimensional model with theXY plane of a two-dimensional model, we set the grid layout of the three-dimensional model to 500 grids for the length, 1 grid for the width, and 10 grids for the thickness. We set the grid layout of the other three-dimensional model to 1 grid for the length, 260 grids for the width, and 10 grids for the thickness when comparing it with the ZY plane of the two-dimensional model. This type of grid layout reduced the complexity of the three-dimensional models and facilitated the comparison of the frequency curves of the three-dimensional models to those of the two-dimensional models. The sizes and grid layouts of the models in this study are shown in Table 1.Table 1
Sizes and grid layouts of the three- and two-dimensional models.
SC-cut
Model
Dimension
Mesh numbers
(
L
×
W
×
T
) (mm)
(
L
×
W
×
T
)
Case 1
2D (X
Y plane)
3.53
×
0.0638
(
L
×
T
)
500
×
10
(
L
×
T
)
3D
3.53
×
1.805
×
0.0638
500
×
1
×
10
Case 2
2D (Z
Y plane)
1.85
×
0.0638
(
W
×
T
)
260
×
10
(
W
×
T
)
3D
3.495
×
1.85
×
0.0638
1
×
260
×
10Figures3 and 4, respectively, show the frequency responses obtained from analyzing the models in Case 1 and Case 2. We selected three different modes from the curves to analyze; they were flexural modes (indicated by 1), thickness shear modes (indicated by 2), and coupled resonant modes (indicated by 3). From the mode shapes corresponding to the noticeable peak values in Figure 3 (m
1, m
2, m
3, p
1, p
2, and p
3), we found that we could still obtain similar modes from the two-dimensional model. The error values of Case 1 are shown in Table 2. Though the number of grids was set to 1 for the width of the three-dimensional model, there were still some oscillations caused by the width effect. In other words, the advantage of using a two-dimensional model for analysis is that the influence of the width direction of the plate can be eliminated. The oscillation modes of the XY plane can then be specifically discussed.Table 2
Comparison of the error values of three- and two-dimensional models’ mode frequency.
SC-cut
3D (MHz)
2D (MHz)
Error (%)
Case 1
p
1
28.0525
m
1
28.0725
0.069513
p
2
28.145
m
2
28.215
0.248712
p
3
28.25
m
3
28.33
0.283186
Case 2
a
1
30.65
b
1
30.67
0.065253
a
2
31.005
b
2
30.938
−0.21609
a
3
31.39
b
3
31.435
0.143358Comparison of the frequency response of the SC-cut three-dimensional plate and the SC-cut two-dimensional plate (XY plane).
(a)
(b)Comparison of the frequency response of the SC-cut three-dimensional plate and the SC-cut two-dimensional plate (ZY plane).
(a)
(b)The same result was discovered when using the models in Case 2 to analyze theZY plane; we obtained the result by comparing the mode shapes corresponding to the noticeable peak values in Figure 4 (a
1, a
2, a
3, b
1, b
2, and b
3). The difference was that the baseband of the ZY direction was located at a higher frequency (31.005 MHz) and the baseband of the XY direction was located at a lower frequency (28.145 MHz). Thus, the resonant mode of the ZY direction was easily affected by the coupled resonant mode of the XY direction; this caused the resonant mode of the ZY direction to separate and produce incomplete oscillations. This is shown as Mode a
3 in Figure 4.In this section, we used SC-cut three-dimensional models and two-dimensional models to compare the mode oscillations. When using three-dimensional models for analysis, we found it difficult to examine the oscillation characteristics of the plates due to the complicated oscillating modes resulting from the natural vibrations of the three directions. Therefore, we set the number of grids to 1 for each single direction (either the length or the width) to decrease the degree of interference. Through analysis of the two-dimensional models, we found that the mode shapes after simplification corresponded to those of the three-dimensional models. The average error value fell within the range of ±0.02 to 0.3%. In other words, we could replace the three-dimensional vibration analysis with a two-dimensional plane strain analysis whenonly examining the oscillation characteristics of the thickness direction. This not only effectively reduced the interference from the third direction but also significantly improved the efficiency of analysis. Thus, we used the two-dimensional models for the following analyses.


## 2.1. Setting the Size and Boundary Conditions of the Finite Element Model

A finite element analysis simulation software [10] was used in this study to analyze the vibrations of thin quartz plates. The size of the quartz resonators used in this study was 3.495 mm in length (2
a), 0.0638 mm in thickness (2
b), and 1.805 mm in width (2
c). The AT-cut and SC-cut of anisotropic piezoelectric quartz plates were considered in this paper. We set the boundary condition as the application of voltage differences to the upper and lower layers of quartz plates. Figure 1 shows the boundary condition setting of two-dimensional models.Figure 1
Boundary condition setting of two-dimensional quartz plate models.


## 2.2. Grid Layout and Frequency Convergence

Thickness shear modes are one of the vibration modes of quartz resonators. The frequencies of thickness shear modes are influenced by the thickness of quartz plates. Therefore, the thickness of grids must be sufficient to make the obtained frequency converge. In general, more grids result in a more precise value. However, to be efficient when analyzing, the number of grids should be just enough to make the frequency convergent. The models in this study come from the analysis results of the number of grids and frequency convergence in a study conducted by Huang and Chen [11].In their study, Huang and Chen found the appropriate number of grids in terms of grid convergence of the thickness of two-dimensional quartz plate models. When dividing the thickness of a quartz plate (0.0638 mm) into 10 grids, the error value (6.9342 ppm) they obtained was closer to convergence, compared to when the thickness was divided into 100 grids. Also, when dividing the length of the plate (3.495 mm) into at least 500 grids, the error value of resonance frequency they obtained dropped to under 30 ppm; the value was less compared to that obtained when dividing the length into 1000 grids. Considering the length/grid ratio, the size of each grid was obtained, and the equation was written as 3.495/500 = 6.99 × 10−3 (mm). Based on the grid size, an appropriate number of grids for the width of the plate were calculated to achieve the frequency convergence; the equation was written as 1.805/6.99 × 10−3 = 258 (grid). To attain the best frequency convergence result, we divided the length of each model into 500 grids, the width into 260 grids, and the thickness into 10 grids.


## 2.3. Simplifying Quartz Plate Models

The equations of motion for a piezoelectric plate can be obtained from the variational principle shown in(1)
∫
t
0
t
d
t
∫
V
[
(
T
i
j
,
i
-
ρ
u
¨
j
)
δ
u
j
+
D
j
,
j
δ
ϕ
]
d
V
=
0
,
where T
i
j is the stress tensor, t is the time variable, and ρ and u
j are the density and displacement vector, respectively. D
j is the electric displacement vector and ϕ is the electric potential. V is the volume of the piezoelectric plate.The piezoelectric constitutive relationships among stress, strain, electric field, and electric displacement field in a stress-charge form are expressed as(2)
T
i
j
=
c
i
j
k
l
S
k
l
-
e
k
i
j
E
k
,
S
i
j
=
1
2
(
u
i
,
j
+
u
j
,
i
)
,
D
i
=
e
i
j
k
S
j
k
+
ε
i
j
E
j
,
E
i
=
-
ϕ
,
i
,
where S
k
l is the strain tensor and E is the electric field. The tensors c
i
j
k
l, e
k
i
j, and ε
i
j are elastic constants, piezoelectric constants (coupling coefficients), and dielectric constants, respectively.The stress-strain analysis used to analyze three-dimensional models can be divided into two methods for simplification in terms of elasticity: plane stress and plane strain. For anisotropic material like quartz, 2D model based on plane strain assumption does not give accurate results [12]. In this paper, to obtain approximate accurate results for the thickness mode and flexural mode frequencies from the 2D model, the shear strain in the z direction when using the XY plane strain case and the shear strain in the x direction when using the ZY plane strain case are not taken into consideration.The plane stress is mainly used to analyze very thin quartz plates. The external force is evenly distributed through the thickness of the plates, and the stress components do not change with the direction of thickness. Therefore, there are only normal stressesσ
x and σ
z, and shear stress τ
x
z when XZ is considered as the plane in plane stress case. The values of σ
y, τ
y
x, and τ
y
z would be 0 so that the plane stress case cannot be used to discuss the thickness shear vibration modes.The plane strain is mainly applied to analyze longer pillars. The cross section of a pillar and the longitudinal force do not change with length. When thez-axis is the major axis, then the displacement along the z-axis would always be 0. Thus, there are only normal strains ε
x and ε
y and shear strain γ
x
y when XY is considered as the plane in the plane strain case. Here, strains ε
z, γ
y
z, and γ
x
z would not exist.Thickness shear modes are the main source of resonation in quartz resonators for specific cuts of quartz; they can be seen as horizontal shearing motions along thex or z direction when the normal of plane is y. Though thin plate resonators tend to apply the simplification method of plane stress, the stress and shear stress of the thickness direction are not included in a plane stress analysis. This does not meet the requirements of two-dimensional quartz plate analysis. Therefore, we used plane strain analysis to analyze the two-dimensional quartz plate and discuss the resonance characteristics of the plate’s XY plane. To simplify the plate, or to ignore the influence that z-axis had on the plane, we made the length of the z-axis much longer than those of the x- and y-axes. The XY plane of the simplified three-dimensional resonator is shown as Figure 2.Figure 2
Simplification of quartz plate model.


## 2.4. Comparison between Three-Dimensional and Two-Dimensional Quartz Plate Modes

The simplification of three-dimensional models helps to improve the analysis efficiency of the finite element method. However, according to the grid convergence information in the study conducted by Huang and Chen, the size of each grid of the model dimensions must be smaller than7
×
1
0
-
3 mm to achieve frequency convergence [11]. This could be very difficult to realize when analyzing a three-dimensional model. Considering the directional effects of the length, the width, and the thickness of a three-dimensional model produces extremely complicated oscillating curves.To compare a three-dimensional model with theXY plane of a two-dimensional model, we set the grid layout of the three-dimensional model to 500 grids for the length, 1 grid for the width, and 10 grids for the thickness. We set the grid layout of the other three-dimensional model to 1 grid for the length, 260 grids for the width, and 10 grids for the thickness when comparing it with the ZY plane of the two-dimensional model. This type of grid layout reduced the complexity of the three-dimensional models and facilitated the comparison of the frequency curves of the three-dimensional models to those of the two-dimensional models. The sizes and grid layouts of the models in this study are shown in Table 1.Table 1
Sizes and grid layouts of the three- and two-dimensional models.
SC-cut
Model
Dimension
Mesh numbers
(
L
×
W
×
T
) (mm)
(
L
×
W
×
T
)
Case 1
2D (X
Y plane)
3.53
×
0.0638
(
L
×
T
)
500
×
10
(
L
×
T
)
3D
3.53
×
1.805
×
0.0638
500
×
1
×
10
Case 2
2D (Z
Y plane)
1.85
×
0.0638
(
W
×
T
)
260
×
10
(
W
×
T
)
3D
3.495
×
1.85
×
0.0638
1
×
260
×
10Figures3 and 4, respectively, show the frequency responses obtained from analyzing the models in Case 1 and Case 2. We selected three different modes from the curves to analyze; they were flexural modes (indicated by 1), thickness shear modes (indicated by 2), and coupled resonant modes (indicated by 3). From the mode shapes corresponding to the noticeable peak values in Figure 3 (m
1, m
2, m
3, p
1, p
2, and p
3), we found that we could still obtain similar modes from the two-dimensional model. The error values of Case 1 are shown in Table 2. Though the number of grids was set to 1 for the width of the three-dimensional model, there were still some oscillations caused by the width effect. In other words, the advantage of using a two-dimensional model for analysis is that the influence of the width direction of the plate can be eliminated. The oscillation modes of the XY plane can then be specifically discussed.Table 2
Comparison of the error values of three- and two-dimensional models’ mode frequency.
SC-cut
3D (MHz)
2D (MHz)
Error (%)
Case 1
p
1
28.0525
m
1
28.0725
0.069513
p
2
28.145
m
2
28.215
0.248712
p
3
28.25
m
3
28.33
0.283186
Case 2
a
1
30.65
b
1
30.67
0.065253
a
2
31.005
b
2
30.938
−0.21609
a
3
31.39
b
3
31.435
0.143358Comparison of the frequency response of the SC-cut three-dimensional plate and the SC-cut two-dimensional plate (XY plane).
(a)
(b)Comparison of the frequency response of the SC-cut three-dimensional plate and the SC-cut two-dimensional plate (ZY plane).
(a)
(b)The same result was discovered when using the models in Case 2 to analyze theZY plane; we obtained the result by comparing the mode shapes corresponding to the noticeable peak values in Figure 4 (a
1, a
2, a
3, b
1, b
2, and b
3). The difference was that the baseband of the ZY direction was located at a higher frequency (31.005 MHz) and the baseband of the XY direction was located at a lower frequency (28.145 MHz). Thus, the resonant mode of the ZY direction was easily affected by the coupled resonant mode of the XY direction; this caused the resonant mode of the ZY direction to separate and produce incomplete oscillations. This is shown as Mode a
3 in Figure 4.In this section, we used SC-cut three-dimensional models and two-dimensional models to compare the mode oscillations. When using three-dimensional models for analysis, we found it difficult to examine the oscillation characteristics of the plates due to the complicated oscillating modes resulting from the natural vibrations of the three directions. Therefore, we set the number of grids to 1 for each single direction (either the length or the width) to decrease the degree of interference. Through analysis of the two-dimensional models, we found that the mode shapes after simplification corresponded to those of the three-dimensional models. The average error value fell within the range of ±0.02 to 0.3%. In other words, we could replace the three-dimensional vibration analysis with a two-dimensional plane strain analysis whenonly examining the oscillation characteristics of the thickness direction. This not only effectively reduced the interference from the third direction but also significantly improved the efficiency of analysis. Thus, we used the two-dimensional models for the following analyses.


## 3. Excitation and Dead Vibration Modes of Quartz Resonators

Through the analysis of finite element software, we found that quartz plates produced numerous types of oscillation modes when excited by an electric field. The patterns of these oscillation modes were exactly the same as those generated from natural oscillations. But the resonances at certain frequencies became minimal after being excited by the voltage loading. Thus, we considered the resonances which had a frequency width of less than 2500 Hz as failure resonant frequencies. We further discussed whether the mode characteristics of AT-cut and SC-cut plates could be excited by the electric field and the regularity of the frequencies.


### 3.1. Analysis Results and Discussion (AT-Cut)

The analysis of quartz plates can be divided into two parts; one is the analysis of natural vibration frequencies, and the other is the analysis of excited vibration frequencies caused by voltage loading. When the sizes of quartz resonators differ, their resonance modes change in different ways. Figure5 shows the dispersion curves of the resonance modes when AT-cut plates of different sizes vibrate naturally and when they are excited by electrodes.Figure 5
Dispersion curves of the resonance modes of different sized plates vibrating naturally and being excited by electrodes (AT-cut,XY-plane).In Figure5, the horizontal axis represents the length-to-thickness ratio (a/b), and the longitudinal axis represents the frequency value. The range of frequency is between 25 MHz and 27 MHz. The curves composed of solid dots denote the natural resonant modes of quartz plates, and the curves composed of empty dots denote the resonant modes of plates excited by voltage loading. By slightly modifying the size of the plates, it is easy to find differences between the plates that were excited by the resonant nodes and those plates that were not. The longitudinal line in Figure 5 represents the location of the original size of the quartz resonator, and the original size was further analyzed. Figure 6 shows the comparison of the natural vibrations and the excited vibrations of the original plate size.Figure 6
Comparison of the plate’s natural and excited vibrations.The goal is to compute the susceptance (the imaginary part of the admittance) for a frequency range around the eigenfrequencies of the structure. In Figure6, the horizontal axis represents the frequency, and the longitudinal axis represents the susceptance. The line denotes the frequency response curve generated from the vibrations after the plate is excited by the voltage loading, and the solid dots are the resonance frequencies of the plate’s natural vibrations. According to Figure 6, the plate produces 16 natural resonant modes when the frequency ranges between 25 MHz and 27 MHz. However, there are only 7 modes of excited vibrations generated in this range when exciting the plate with voltage loading. Therefore, when applying voltage to the piezoelectric plate, some modes generate resonance frequencies of low impedance when being excited by voltage loading. Yet, some natural frequencies of the plate are unexcitable by voltage loading and subsequently cause resonant vibration failure. In brief, only some resonant modes can be excited among the plate resonances generated from the converse piezoelectric effect.To determine the regularity among the resonant modes generated from both the plate’s natural vibrations and the excited vibrations, we had a discussion on the resonant modes in Figure6. By observing the 15 modes within the frequency range, we found several characteristics of vibrations which could be excited by voltage loading.Among the vibration modes of two-dimensional quartz plates, there are four basic modes. They are the flexural mode, the thickness shear mode, the coupled mode of the flexural and thickness shear modes, and the extension mode. These four modes can be further divided into symmetric and antisymmetric resonant modes in terms of their shape (as shown in Figures7 and 8). After categorizing the resonance characteristics of the modes, preparations are complete for determining whether the resonant modes can be excited.Figure 7
Antisymmetric resonant mode.Figure 8
Symmetric resonant mode.First, we evaluated the symmetry of each mode by looking at the mode shapes in Figure6. The mode shapes of P1 to P10 in Figure 6 were then taken out to develop Figure 9. Among the ten modes, P3, P5, P7, and P9 were symmetric resonant modes; P1, P4, P6, P8, and P10 were categorized as antisymmetric resonant modes. By evaluating the resonant modes of different symmetric characteristics, we found some consistent phenomena. When the mode shapes were considered antisymmetric, they could be excited; however the symmetric resonant modes could not be excited. P2 and P7 appeared neither symmetric nor antisymmetric, but according to the analysis, neither could be excited. This was further examined in the following portion of the study.Mode shapes (P1 to P10).
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)


### 3.2. Analysis Results and Discussion (SC-Cut)

The vibrations of piezoelectric plates represent the coupling effects of the force field and the electric field. Therefore, the material elasticity matrix of the force field, the dielectric constant matrix of the electric field, and the piezoelectric constant matrix of the electromechanical coupling must be provided in the analysis. Through the simplification of quartz plates, we ran the plane strain analysis on theXY plane and the ZY plane of two-dimensional models. However, when running the analysis on the ZY plane of AT-cut quartz plates, the piezoelectric constants of the ZY direction, e
222, e
233, e
223, e
322, e
333, and e
323, were always 0; we could not analyze the piezoelectric plate oscillations of the ZY plane. Thus, we additionally analyzed the resonant modes of the XY and ZY planes of SC-cut plates. We then compared the locations of the two thickness shear modes and the regularities of their excited vibration frequencies and frequencies of failure.The material parameters of SC-cut plates stand for the application of a different kind of quartz plates, and these plates have better adaptability to temperature changes. When the temperature changes, the error value of the thickness-shear frequency is lower compared to that of AT-cut plates. The size of the SC-cut quartz plates used in this study is 3.53 mm in length (2
a), 0.0638 mm in thickness (2
b), and 1.85 mm in width (2
c). According to the analyses, the thickness shear mode of XY plane was 28.21586 MHz and that of ZY plane was 30.93937 MHz. We set frequency ranges of 3 MHz above and below the two basebands for the XY and ZY planes to develop frequency curves of different sized plates (as shown in Figures 10 and 11).Figure 10
Dispersion curves of the resonant modes of different sized plates vibrating naturally and being excited by electrodes (SC-cut,XY-plane).Figure 11
Dispersion curves of the resonant modes of different sized plates vibrating naturally and being excited by electrodes (SC-cut,ZY-plane).The purpose of analyzing the vibrations of SC-cut plates was to compensate for the incapability of analyzing theZY plane of AT-cut plates. Besides, we used the analysis results of SC-cut plates to decide whether the method used to determine the excited vibration frequencies and dead vibration frequencies in previous section was appropriate. We found that when the resonant modes were antisymmetric, they could also be excited and the modes that were considered symmetric could not be. This proved the suitability of the method used previously. However, something different occurred when analyzing only the XY plane of AT-cut plates. In this case, we could not be certain about the requirements for exciting the extensional vibration modes, since the five curves of extensional vibration modes in Figure 5 were neither symmetric nor antisymmetric. Moreover, none of them could be excited. Therefore, we needed more data to find out the requirements for exciting extensional vibration modes.We selected 4 extensional vibration mode shapes (m
1 to m
4) from the analyses of the XY and ZY planes of SC-cut plates to develop Figure 12. The mode shapes of m
1 and m
3 were symmetric, and the mode shapes of m
2 and m
4 were antisymmetric. After analysis, the results of exciting these modes with voltage corresponded to those mentioned in Section 3.1. Thus, we believe that the requirements for exciting extensional vibration modes are the same as those mentioned in Section 3.1, where the mode shapes can be excited when they are antisymmetric.Extensional vibration modes (in SC-cut).
(a)
(b)
(c)
(d)


## 3.1. Analysis Results and Discussion (AT-Cut)

The analysis of quartz plates can be divided into two parts; one is the analysis of natural vibration frequencies, and the other is the analysis of excited vibration frequencies caused by voltage loading. When the sizes of quartz resonators differ, their resonance modes change in different ways. Figure5 shows the dispersion curves of the resonance modes when AT-cut plates of different sizes vibrate naturally and when they are excited by electrodes.Figure 5
Dispersion curves of the resonance modes of different sized plates vibrating naturally and being excited by electrodes (AT-cut,XY-plane).In Figure5, the horizontal axis represents the length-to-thickness ratio (a/b), and the longitudinal axis represents the frequency value. The range of frequency is between 25 MHz and 27 MHz. The curves composed of solid dots denote the natural resonant modes of quartz plates, and the curves composed of empty dots denote the resonant modes of plates excited by voltage loading. By slightly modifying the size of the plates, it is easy to find differences between the plates that were excited by the resonant nodes and those plates that were not. The longitudinal line in Figure 5 represents the location of the original size of the quartz resonator, and the original size was further analyzed. Figure 6 shows the comparison of the natural vibrations and the excited vibrations of the original plate size.Figure 6
Comparison of the plate’s natural and excited vibrations.The goal is to compute the susceptance (the imaginary part of the admittance) for a frequency range around the eigenfrequencies of the structure. In Figure6, the horizontal axis represents the frequency, and the longitudinal axis represents the susceptance. The line denotes the frequency response curve generated from the vibrations after the plate is excited by the voltage loading, and the solid dots are the resonance frequencies of the plate’s natural vibrations. According to Figure 6, the plate produces 16 natural resonant modes when the frequency ranges between 25 MHz and 27 MHz. However, there are only 7 modes of excited vibrations generated in this range when exciting the plate with voltage loading. Therefore, when applying voltage to the piezoelectric plate, some modes generate resonance frequencies of low impedance when being excited by voltage loading. Yet, some natural frequencies of the plate are unexcitable by voltage loading and subsequently cause resonant vibration failure. In brief, only some resonant modes can be excited among the plate resonances generated from the converse piezoelectric effect.To determine the regularity among the resonant modes generated from both the plate’s natural vibrations and the excited vibrations, we had a discussion on the resonant modes in Figure6. By observing the 15 modes within the frequency range, we found several characteristics of vibrations which could be excited by voltage loading.Among the vibration modes of two-dimensional quartz plates, there are four basic modes. They are the flexural mode, the thickness shear mode, the coupled mode of the flexural and thickness shear modes, and the extension mode. These four modes can be further divided into symmetric and antisymmetric resonant modes in terms of their shape (as shown in Figures7 and 8). After categorizing the resonance characteristics of the modes, preparations are complete for determining whether the resonant modes can be excited.Figure 7
Antisymmetric resonant mode.Figure 8
Symmetric resonant mode.First, we evaluated the symmetry of each mode by looking at the mode shapes in Figure6. The mode shapes of P1 to P10 in Figure 6 were then taken out to develop Figure 9. Among the ten modes, P3, P5, P7, and P9 were symmetric resonant modes; P1, P4, P6, P8, and P10 were categorized as antisymmetric resonant modes. By evaluating the resonant modes of different symmetric characteristics, we found some consistent phenomena. When the mode shapes were considered antisymmetric, they could be excited; however the symmetric resonant modes could not be excited. P2 and P7 appeared neither symmetric nor antisymmetric, but according to the analysis, neither could be excited. This was further examined in the following portion of the study.Mode shapes (P1 to P10).
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)


## 3.2. Analysis Results and Discussion (SC-Cut)

The vibrations of piezoelectric plates represent the coupling effects of the force field and the electric field. Therefore, the material elasticity matrix of the force field, the dielectric constant matrix of the electric field, and the piezoelectric constant matrix of the electromechanical coupling must be provided in the analysis. Through the simplification of quartz plates, we ran the plane strain analysis on theXY plane and the ZY plane of two-dimensional models. However, when running the analysis on the ZY plane of AT-cut quartz plates, the piezoelectric constants of the ZY direction, e
222, e
233, e
223, e
322, e
333, and e
323, were always 0; we could not analyze the piezoelectric plate oscillations of the ZY plane. Thus, we additionally analyzed the resonant modes of the XY and ZY planes of SC-cut plates. We then compared the locations of the two thickness shear modes and the regularities of their excited vibration frequencies and frequencies of failure.The material parameters of SC-cut plates stand for the application of a different kind of quartz plates, and these plates have better adaptability to temperature changes. When the temperature changes, the error value of the thickness-shear frequency is lower compared to that of AT-cut plates. The size of the SC-cut quartz plates used in this study is 3.53 mm in length (2
a), 0.0638 mm in thickness (2
b), and 1.85 mm in width (2
c). According to the analyses, the thickness shear mode of XY plane was 28.21586 MHz and that of ZY plane was 30.93937 MHz. We set frequency ranges of 3 MHz above and below the two basebands for the XY and ZY planes to develop frequency curves of different sized plates (as shown in Figures 10 and 11).Figure 10
Dispersion curves of the resonant modes of different sized plates vibrating naturally and being excited by electrodes (SC-cut,XY-plane).Figure 11
Dispersion curves of the resonant modes of different sized plates vibrating naturally and being excited by electrodes (SC-cut,ZY-plane).The purpose of analyzing the vibrations of SC-cut plates was to compensate for the incapability of analyzing theZY plane of AT-cut plates. Besides, we used the analysis results of SC-cut plates to decide whether the method used to determine the excited vibration frequencies and dead vibration frequencies in previous section was appropriate. We found that when the resonant modes were antisymmetric, they could also be excited and the modes that were considered symmetric could not be. This proved the suitability of the method used previously. However, something different occurred when analyzing only the XY plane of AT-cut plates. In this case, we could not be certain about the requirements for exciting the extensional vibration modes, since the five curves of extensional vibration modes in Figure 5 were neither symmetric nor antisymmetric. Moreover, none of them could be excited. Therefore, we needed more data to find out the requirements for exciting extensional vibration modes.We selected 4 extensional vibration mode shapes (m
1 to m
4) from the analyses of the XY and ZY planes of SC-cut plates to develop Figure 12. The mode shapes of m
1 and m
3 were symmetric, and the mode shapes of m
2 and m
4 were antisymmetric. After analysis, the results of exciting these modes with voltage corresponded to those mentioned in Section 3.1. Thus, we believe that the requirements for exciting extensional vibration modes are the same as those mentioned in Section 3.1, where the mode shapes can be excited when they are antisymmetric.Extensional vibration modes (in SC-cut).
(a)
(b)
(c)
(d)


## 4. Conclusion

In this study, we discuss the resonances of quartz plates. We first simplify our models with plane strain analysis and then analyze the resonances ofXY and ZY planes of our two-dimensional models. Quartz resonators are considered as frequency components; therefore, the number of grids becomes especially important when conducting the finite element analyses. Based on an earlier study [10], we set the grid layout of the models as 500 grids for the length, 260 grids for the width, and 10 grids for the thickness to achieve the best frequency convergence. We additionally analyze the XY and ZY planes of SC-cut material parameters, since the ZY plane of AT-cut plates cannot be simplified.The continuous stable oscillations of quartz resonators come from the converse piezoelectric effects when applying voltage to piezoelectric plates. However, when analyzing the oscillations of quartz plates, we notice that the excited quartz plates can only produce certain resonant modes; other resonant modes are considered as having failed, since they are not excitable by voltage loading. We use the finite element software to analyze the free oscillations and excited vibrations of quartz plates. By comparing the characteristics of resonant modes, we conclude that the resonant modes of quartz plates can be excited when the mode shapes are antisymmetric; when the mode shapes of the plates are symmetric, they cannot be excited. The difference in the surface charge density for symmetric modes obtained from free vibration approximated zero and hence cannot be excited by the voltage loading under the electrode configuration studied in this paper. This is in accordance with the experimental study of resonators and of the general result of Lewis’ paper [13].



---

*Source: 746847-2014-02-10.xml*