Free Vibration Analysis of Elastic Bodies for Six-Axis Force Sensor ()

Dezhang Xu, Zhihong Wang

School of Mechanical and Automotive Engineering, Anhui Polytechnic University, Wuhu, China.

**DOI: **10.4236/jst.2013.31003
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School of Mechanical and Automotive Engineering, Anhui Polytechnic University, Wuhu, China.

Now the six-axis force sensor (6-AFS) is used widely, and as the core components, mechanical properties of its elastic bodies are significant. With the increase of dynamic loads, studies on dynamic characteristics of the 6-AFS become more and more important. In this paper, the study focuses on the free vibration problem of a novel 6-AFS. The research approach is to decompose the sensor into several separate elastic bodies (four lamellas and upper and lower membranes) and research these elastic bodies respectively. The free vibration of the lamella is studied based on Rayleigh-Ritz method and the separation of variables. The analytical solutions of free vibration of the membranes are deduced according to the nature of Bessel functions. Both the analytical results are simulated with MATLAB. Compared the simulated diagrams with actual situations, they are very close. The mode shapes obtained play a major role in solving the forced vibration of the sensor.

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D. Xu and Z. Wang, "Free Vibration Analysis of Elastic Bodies for Six-Axis Force Sensor," *Journal of Sensor Technology*, Vol. 3 No. 1, 2013, pp. 13-20. doi: 10.4236/jst.2013.31003.

1. Introduction

Scientists commit themselves to improving the level of intelligent robots because they want to obtain an equipment that can work as human beings. In order to have the similar functions as human’s hand, the six-axis wrist force sensor is developed which can measure force components and moment components [1,2].

Over the years, static characteristics of multi-axis force sensors have been further studied by domestic and foreign scholars and many achievements have been obtained. In 1990, Tsuneo Yoshikawa, a professor at Kyoto University in Japan, deduced the relationship of stress-strain and static-coupling of a cross-shape force sensor under static load using Material Mechanics in detail [3]. In 2010, K. Q. Liang et al. used Material Mechanics and finite element method to analyze the relationship of stress-strain of a novel 6-AFS at the State Key Laboratory of Sensor Technology, and determined the cross-coupling through static calibration [4]. A. G. Song, a professor at Southeast University, designed a four-axis force sensor with low coupling and analyzed the cross-coupling by using Material Mechanics and finite element method [5]. To improve the accuracy of these force sensors, researchers all over the world have made unremitting efforts. Y. Haddab et al. at French FEMTO-ST Institute used Kalman filtering technique to reduce the output noise [6]. The author of this paper used matrix perturbation theory to discuss the relation between the value of elements in cross-coupling matrixand the sensor’s measuring accuracy. In this paper, an important conclusion was drawn that when the increments of the forces at six directions are the same, the measuring accuracy is ideal, and this conclusion received high attention from researchers at Institute of Intelligent Machines, Chinese Academy of Sciences (CAS) and was seen as one of the bases for the design of multi-axis force sensor (MAFS) [7]. Synthesizing the present research achievements, researches about the static characteristics of MAFS are indepth and sufficient. However, less attention is paid to dynamic characteristics of these sensors. AMTI Inc. is the main manufacturer of MAFS internationally and only the upper limit frequency is given in its instruction. Along with the increase of situations that intelligent robots work under dynamic loads, studies about vibration problem of the MAFS become more and more important. So in this paper, the dynamic problem is researched.

For the mechanical property of a 6-AFS, the focus should be drawn to its sensing elements which are the core components of the sensor. The lightweight thin plate structures have been widely used as elastic bodies to detect the force information, e.g., the four-dimensional fingertip force sensor and the 6-AFS based on double layer E-type membrane developed by Institute of Intelligent Machines, CAS, they all use thin plate as the elastomer to detect the outside force information. Thus, the knowledge of its free vibration is significant to the structural designers [8]. The free vibration characteristic of a elastic thin plate is the basis and has great significance for the follow-up studies of the forced vibration. Since the introduction of the small deflection theory of plate bending, people are interested in vibration problems of the elastic thin plate. The free vibration analysis of rectangular and circular plates is important for the design of plate-type structures. Consequently, a great many of research reports have been conducted on the dynamic behavior of such structures. Leissa offered comprehensive sets of research data for the free vibration of elastic thin plates based on Kirchhoff’s thin plate theory [9]. As closed form solutions for plate vibration problems are known only for certain special cases in which at least a pair of opposite sides is simply supported. One has to use approximate method. As a result, a large number of useful methods have been developed to get solutions for some practical problems. The Rayleigh-Ritz method is one of the most popular methods to obtain the approximate solutions for the natural frequencies of rectangular and annular plates [10-12]. Rayleigh-Ritz method uses a linear combination of some assumed basic functions to express the mode shape. Finite element methods often divide the elastic body into a number of smaller elements and approximate the solution by using local piecewise continuous shape functions [13,14]. And there are some other approximate methods including the differential quadrature (DQ) method [15], the least squares techniques [16], the Meshless methods [17], and the spline finite strip method by G. Akhras and W. Li [18].

In the present paper, Rayleigh-Ritz method and the separation of variables are used to obtain the natural frequencies and the corresponding mode shapes of the Kirchhoff rectangular plate. And according to the nature of Bessel equations and Bessel functions, the analytical expressions of natural frequencies and associated mode shapes of the Kirchhoff circular plate are derived. At last, the simulation diagrams of analytical results are obtained by the software of MATLAB. The natural frequencies and mode shapes deduced will be used to solve the dynamic response of thin plates under harmonic force in follow-up studies.

2. Differential Equation of Thin Plate

2.1. Governing Equations of Rectangular Plate

A vast literature exists about the free vibration of rectangular plates. Consider a thin rectangular plate of length, width and uniform thickness, oriented so that its middle surface contains and axes of a Cartesian coordinate system (), as shown in Figure 1. Based on Kirchhoff’s thin plate theory, the free vibration differential equation of thin plates is:

, (1)

where is the transverse deflection; is the differential operator in Cartesian coordinates (i.e.,，

), is the bending rigidity; is Young’s modulus; is Poisson’s ratio; is mass density per unit volume; is the time. It is well-known that the free vibration of an elastic linear system is harmonic, therefore, the deflection of free vibration of the thin plate can be assumed to be:

, (2)

where is the natural frequency, is the associated mode shape, depend on initial conditions. Considering one solution with the general form:

, (3)

then it is possible to obtain the following equation in terms of spatial variables only:

. (4)

This equation is a two-dimensional partial differential equation, and the exact solution is limited to vibration problems with simple shape, load and boundary conditions. There are no exact solutions for natural frequencies and associated mode shapes of the transverse vibrations except plates with four edges or one opposite edges simply supported. For the case of complex shape, load or boundary conditions, approximate method must be used, such as lumped mass method, finite element method and assumed mode method. In this paper, Rayleigh-Ritz method is adopted [19].

Figure 1. The rectangular plate.

2.2. Rayleigh-Ritz Method Rayleigh-Ritz method is a semi-analytical method and widely used in solving free vibration problems of the thin plate. For this method, the vibration mode shape is expressed in terms of the plate characteristic functions as:

. (5)

where and are polynomial functions depending upon the boundary conditions of the plate, is the unknown parameter that need to be found.

The procedure of free vibration doesn’t involve any outside force, and the expressions for the maximum strain and kinetic energy respectively are:

,(6)

(7)

The principle of minimum potential energy is that for the constraint of boundary conditions, the potential energy corresponding to the exact solution is less than any other possible potential energy. Then the variation of potential energy functional should be zero, namely,

.

Minimization of the difference between and with respect to each of the coefficient leads to:

, (8)

where and.

From Equation (8), the simultaneous linear homogeneous equations with the unknown coefficients are obtained. These linear equations can be solved as an eigenproblem. Hence, it is possible to estimate the natural frequencies and mode shapes of thin plate.

2.3. Governing Equations of Circular Thin Plate

The vibration of an isotropic circular plate with constant thickness is well documented. The motion equation of a circular thin plate is similar to that of rectangular thin plate. The only difference is the conversion from Cartesian coordinates to polar coordinates. In polar coordinates, the differential equation of free vibration of a thin plate is:

, (9)

where is the differential operator in polar coordinates,

.

Defining a solution as Equation (3) and, and inserting them into Equation (9), the equation becomes:

. (10)

The solution of Equation (10) can be written as the sum of two distinct solutions, , where,

. (11)

Use the separation of variables and assume the mode shape as followings:

. (12)

Inserting Equation (12) into Equation (11) respectively, one obtains:

, (13)

. (14)

These two are special equations which are summed up in the study of some physical problems. The general solution of Equation (13) exists in terms of Bessel’s functions with constants and:

, (15)

here and are, respectively, the first and second category n-order Bessel functions. And the general solution of Equation (14) can be expressed with the linear combination of and with constants and:

, (16)

here and are the first and second category n-order Bessel functions of imaginary argument. Above all, the complete solution for displacement on the surface of the circular plate is described as following [20]:

. (17)

3. Free Vibration of 6-AFS’s Elastic Body

The 6-AFS studied in this paper is shown in Figure 2. The sensor consists of the base frame 1, lower E-type membrane 2, central solid cylinder 3, upper E-type membrane 4, middle force-transmitting loop 5, four lamellas 6 and upper force-transmitting loop 7. The base frame serving as a rigid support connects with the lower adapter by bolts. The lower and upper E-type membranes are connected by the cylinder. The middle force-transmitting loop links the upper E-type membrane and four lamellas. The upper force-transmitting loop connects with the upper adapter. For this sensor, components 2, 4 and 6 are elastic elements, and components 1, 3, 5, 7 seen as rigid bodies. The upper E-type membrane is used to detect tangential moments (), and the lower E-type membrane is used to sense the normal force () and both tangential forces (). The four lamellas are responsive to the normal moment (). For the structure and material parameters of the sensor, please refer to Table 1 and Table 2.

During the analysis, the boundary of the rectangular thin plate is seen as one opposite edges clamped and the others free, as shown in Figure 3. The boundary of the upper and lower membranes are both viewed as the inner and outside edges clamped, as shown in Figure 4.

Figure 2. Structure of the six-axis force sensor.

Table 1. Structure parameters of the sensor [m].

Table 2. Parameters of LY12.

Figure 3. Schematic diagram of the lamella.

Figure 4. Schematic diagram of the membrane.

3.1. Free Vibration of Rectangular Plate

Assume that the basic function for mode shape is expressed as the following form:

, (18)

where:;

;;

, , in which:

;

,.

In this paper, let and to calculate the natural frequencies and corresponding mode shapes of the plate. The forms of these basic functions are list in Table 3. Then the mode shape of the thin plate can be expressed as a linear combination of these 12 basic functions as follow:

. (19)

Insertion of Equation (19) into Equations (6) and (7) leads to and. According to Equation (8), a set of 12 simultaneous linear homogeneous equations with as the unknown parameters are obtained. Because the mode shape is existent, the determinant of the obtained equations must be zero and then get the natural frequency equation. Due to the huge computation, the software MATLAB is adopted to help calculate natural frequencies and mode shapes. In the present paper, the lowest six frequencies and mode shapes are obtained as shown in Table 4. The simulation diagrams of mode shapes are shown in Figure 5.

3.2. Free Vibration of Membranes

The boundary conditions of the membranes as shown in Figure 4 are given as follow:

. (20)

Substituting Equation (9) and Equation (17) into Equation (20) leads to the following linear equations:

(21)

In order to make this homogenous equations have a nonzero solution, its coefficient determinant must be zero, namely:

(22)

Table 3. The form of Φm(x)Φn(y).

Table 4. Natural frequencies and mode shapes.

Figure 5. Simulation diagrams of the mode shapes.

Figure 6. Simulation diagrams of the mode shapes.

Table 5. Values of λ_{nm}_{.}

Table 6. Natural frequencies and mode shapes.

Equation (22) is the natural frequency equation of the annular thin plate. According to the nature of Bessel functions, for any nonnegative integer, it has infinitely many solutions. One defines as the m^{th} root of Equation (22) when the circumferential mode number is. Table 5 shows the first four roots when is set to 1,2,3,4 respectively. Then the natural frequency is given by:

(23)

Substituting into Equation (21) leads to the values of and then obtains the mode shapes. Table 6 and Figure 6 respectively show the natural frequencies and mode shapes, and simulation diagrams by software MATLAB with.

4. Conclusion

In this paper, Rayleigh-Ritz method and the separation of variables method are introduced to analyze the free vibrations of the elastic bodies (the lamellas and the membranes) of the 6-AFS based on double layer E-type membrane. Through derivation, the analytical expressions of the natural frequencies and corresponding mode shapes are obtained and simulated by MATLAB. And the theoretical results are in good agreement with the actual situation. The analytical results of free vibrations have great significance to the follow-up studies about the dynamic response of the force vibration of thin plates. And it is also available to verify the correctness of the numerical methods.

5. Acknowledgements

This work is supported by the National Natural Science Foundation of China under Grant No. 51175001 and Anhui Provincial Natural Science Foundation under Grant No. 11040606M144.

Conflicts of Interest

The authors declare no conflicts of interest.

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