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ARTICLE
Year : 2012  |  Volume : 2  |  Issue : 1  |  Page : 7-12

Stability Analysis of Mode Coupling Vibration Systems with Coulomb Friction


School of Mechanical Engineering, Xi'an University of Technology, Xi'an, China

Date of Web Publication24-Mar-2012

Correspondence Address:
Lilan Liu
School of Mechanical Engineering, Xi'an University of Technology, Xi'an
China
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Source of Support: None, Conflict of Interest: None


DOI: 10.4103/0976-8580.93230

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   Abstract 

In the article, the stability analysis of mode coupling systems with Coulomb friction is performed. A two-degree-of-freedom (2-DOF) vibration system with Coulomb friction is constructed. Taking the friction coefficient as a bifurcation parameter, a Hopf bifurcation graph is obtained using the Routh criterion. It is illustrated that Coulomb friction can induce self-excited oscillation in the mode coupling system. The analytic expressions of the limit cycle amplitudes of the oscillation system are achieved based on the extended harmonic balance method. Moreover, the effects of some parameters on the size of limit cycles are investigated. All the research method and results presented can provide a valuable reference for the structure optimal design of mechanical systems and vibration reduction.

Keywords: Friction, limit cycle, mode coupling vibration, stability


How to cite this article:
Liu L, Wu Z. Stability Analysis of Mode Coupling Vibration Systems with Coulomb Friction. J Eng Technol 2012;2:7-12

How to cite this URL:
Liu L, Wu Z. Stability Analysis of Mode Coupling Vibration Systems with Coulomb Friction. J Eng Technol [serial online] 2012 [cited 2019 Jan 23];2:7-12. Available from: http://www.onlinejet.net/text.asp?2012/2/1/7/93230


   1. Introduction Top


The self-excited oscillation behavior induced by friction exists widely in mechanical systems, which has been a main cause of system instability, such as vibration and squeal noise. For the generation mechanism, many researchers intend to clarify it from different aspects [1],[2] . As a whole, there may be four types of mechanisms to describe friction-induced vibration in brake systems [3] . The important one of them is the mode coupling instability. In the case of mode coupling, the system concerned will be instable and limit cycle will appear even with Coulomb friction. This negative effect is unfavorable and should be avoided in brake systems. So, to reduce or eliminate the instability caused by mode coupling, a better solution is to fall back on the optimum design of the system structure and physical parameters. However, it depends on full prior understanding of the influence of these parameters on the system stability. Due to complexity of the problem, one common method for stability analysis is modeling a linear or linearized model of brake systems [4] . In Ref. [5] , the instability mechanism of the steady sliding state has been understood well. Although vibration induced by friction in mode coupling systems has received considerable attention in recent years, there still exist some important aspects such as the effects of different physical parameters on the system stability and the strong nonlinearity induced by Coulomb friction has not been fully studied and are worth further discussion.

The object of this article is to investigate the stability and limit cycle behavior of mode coupling systems with Coulomb friction. The next is organized as follows: In Section 2, the mode coupling system subjected to Coulomb friction to be studied is introduced and modeled. In Section 3, the stability analysis of the system is carried out by using the Routh criterion. And, an analytical calculation method for the limit cycle amplitude based on the extended Harmonic Balance technique is presented in Section 4. The influence of physical parameters on the limit cycles is investigated in Section 5. Conclusion is made at last.


   2. System Description and Modeling Top


The mode coupling model used in this work is a 2-DOF mass-conveyor belt system as shown in [Figure 1]. The conveyor belt moves with a constant velocity vo . The mass is held by two springs (k1 and k2 ) and two dampers (C1 and C2 ) at two directions (x1 and x2 ). Because of the external force F e , the mass is always contacts with the belt. And Coulomb friction force exists at the contact surfaces.
Figure 1: The 2-DOF mass conveyor belt system

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The origin form of this model is first presented by Hulten [6],[7] to study the problem of drum brake squeal, in which only the stiffness is included. The system may be instable because of mode coupling. After that, a damping part was added in the model by Sinou and Je'ze'quel [8] to understand the role of damping. In their work, however, to simplify the analysis, the direction of friction force is not considered in the course of vibration, as described by



where, F fi is the friction force, F ni is the normal force, and μ is the friction coefficient.

But as we know, the Coulomb friction force has its own direction which depends on the relative sliding velocity between two contact surfaces. So such an assumption may be not sufficient for the real dynamic behavior of mechanical systems.

In this article, therefore, to make up the shortage of above assumption, a complete Coulomb model considering direction is adopted



where, denotes the absolute velocity of the mass, and sgn(•) is the sign function.

Therefore, the motion equation of the nonlinear system shown in [Figure 1] is



where, x1 and x2 present the absolute displacements of the mass in the directions of x1 and_x2 , respectively.

In such a case, the external force F e will cause a static displacement of the mass. So when there are the static equilibrium points of the system are:



Taking the static equilibrium points as a new origin of coordinate and inserting into Equation (3), the following can be obtained as



where, represent the displacements of the mass in the new coordinate, respectively. It can be seen in Equation (5) that the stiffness matrix is unsymmetrical because of the friction coefficient μ.

To generalize the system equation, the damping ratio ξi = ci / (2wim)(i =1,2), and the natural frequency ωi = √ki /m(i =1,2)are introduced into Equation (5) and the next relation can be obtained as



It should be pointed out that the aim of the next work is to find out an appropriate analysis method. So the values of parameters used are prior known. In the next computation, the values of the three constant parameters are m=1 kg, v o = ms -1 , and F e = 4.9_N, respectively.


   3. Stability Analysis Top


For a nonlinear system like Equation (6), there is an explicit parameter μ in the stiffness matrix, and so the eigenvalues not only relate to the damping and frequency of the system but also relate to the friction coefficient. Therefore, its stability about the system static solution can be estimated by the eigenvalues of the linearized equation by using the Routh criterion [9] .

The linearized equation of Equation (6) is



And the characteristic equation of Equation (7) can be obtained as



with λ the eigenvalues of the linearized system.

So the eigenvalues of the linear system can be computed by solving the following characteristic polynomial

For Equation (9), if the real parts of the eigenvalues λ are all negative, the static solution of the system is stable. Otherwise it is unstable even if only one root has a positive real part. But solving Equation (9) is very complex. Fortunately, according to the Routh criterion, we do not have to solve the characteristic polynomial actually, and only the Routh coefficients are needed. If all the Routh coefficients are positive, the static solution of the system is stable. Therefore, using the Routh criterion and taking friction coefficient μ as a bifurcation parameter, the Hopf bifurcation point μH can be expressed by the other parameters as



with e= ω 12 and r = ξ 12 .

Equation (10) indicates that the variation of the Hopf bifurcation point has a direct relation with the damping and frequency of the system, as shown in [Figure 2] with

ω1 = 1.1~2s -1, ω 2 = 1.508s -1, ξ1 = 0.001~0.04 and ξ2 = 0.0102.
Figure 2: Three dimension graph of Hopf bifurcation points

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   4. Amplitude Calculation of Limit Cycles Top


From Section 3, it is illustrated that in the case of mode coupling, the vibration system will be instable and limit cycle will appear even with Coulomb friction. The conventional Harmonic Balance technique is a classical method to determine the amplitudes of limit cycles for nonlinear vibration systems. The approach is usually suitable to analyze one-dimensional vibration problem, whereas the mode coupling phenomenon is involved in a 2-DOF problem. To overcome this shortcoming, Hoffmann et al. [10] present a modified approach called extended harmonic balance with a main advantage of yielding multi-DOF mode coupling system. So based on the procedure of the extended harmonic balance, the following calculation is put forward to calculate the limit cycle amplitudes of the oscillation system quantitatively.

The solutions of Equation (6) are supposed as



where denote the static displacements induced by the oscillation, represent the amplitudes of limit cycles, and ω is the harmonic oscillation frequency.

First, substitute Equation (11) into the nonlinear terms located in the right side of Equation (6), and there is



It can be seen that a constant and a first harmonic components are contained in the right side of Equation (12). But there are six parameters which are unknown. To obtain these parameters, first, the Fourier coefficients of the terms f1 (t) and f2 (t) are calculated by integration over one oscillation period as follows:



Similarly, the Fourier coefficients of the terms g 1 (t) and g 2 (t) can also be obtained as



When the above Fourier coefficients are all obtained, the right side of Equation (6) can therefore be represented as



Then, substitute both Equation (11) and Equation (13) into Equation (6) directly and compare the coefficients of the sine, cosine and constant terms. Consequently, six equations can be obtained as follows:



At last, according to these six equations, the six unknown parameters can solved by using the Newton's method. And so, the amplitudes of the limit cycles of the vibration system can be achieved.


   5. Effects of Parameters on Limit Cycles Top


To further understand the effects of some physical parameters on the size of limit cycles, the oscillation amplitudes varying with different parameter values are calculated using the analytical method presented in Section 4.

First, the variation of the limit cycles with the friction coefficient μ is investigated. The values of the used parameters are e = 1.325 with ω 2 = 1.508s -1 , r = 0.98 with ξ 2 = 0.0102 and μ=0.3~0.4, respectively. Under this condition, the value of the Hopf bifurcation point is μH =0.283 according to Equation (10). So when μ>μH , the system will be unstable. What's more, with the increasing of the friction coefficient_μ, the system will be more unstable and the oscillation amplitude becomes bigger. Consequently, as demonstrated in [Figure 3], it is shown that with the increasing of μ, the amplitudes of the limit cycles get greater in both x1 and x2 directions. Comparably, the variation in x 1 direction is more obvious.
Figure 3: Effects of the varying μ on the amplitudes of limit cycles

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Next, the effect of the frequency ratio r = 0.98with ξ2 =0.0102, e=0.993~1.325 with ω2 = 1.508s -1 , and μ= 0.3, respectively. According to Equation (10), all the values of the Hopf bifurcation points with different frequency ratio e are listed in [Table 1]. It can be seen that the Hopf bifurcation point becomes higher with the increasing of the frequency ratio e. As we know, the higher value μH is beneficial for the system stability. So increasing e can diminish the oscillation amplitude. [Figure 4] gives the relationship between the oscillation amplitude and the frequency ratio e. It is shown that when the frequency ratio e increases, the amplitudes of the limit cycles decrease in both x1 and x2 directions.
Figure 4: Effects of the varying e on the amplitudes of limit cycles

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Table 1: Values of Hopf bifurcation points with different

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In addition, the effect of the damping ratio r on limit cycles is also analyzed. The values of used parameters are e = 1.325 with ω2 = 1.508s -1 , r=0.490~2.941 with ξ2 =0.0102, and μ-0.3, respectively. Similarly, the values of the Hopf bifurcation points with different damping ratio r are listed in [Table 2]. It can be seen that increasing the damping ratio r can increase or decrease the value of Hopf bifurcation point μH. So, increasing damping ratio may make a certain vibration mode of the system more unstable sometimes. The relationship between the oscillation amplitude and the frequency ratio r is illustrated in [Figure 5]. It is can be seen that when the damping ratio increases, the amplitudes of the limit cycles decrease in x1 direction while it increases in x2 direction. This means that adding more damping in the vibration system to reduce oscillation amplitudes is not feasible in some cases.
Figure 5: Effects of the varying r on the amplitudes of limit cycles

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Table 2: Values of Hopf bifurcation points with different r

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From the above figures and analysis, it can be known that in the considered region, the increasing of the friction coefficient and the frequency ratio can lead to regular variations of limit cycles. While for the damping ratio, because its effect pattern on the limit cycles is relatively complex, its variation tendency should be combined with detail stability analysis in prior.


   6. Conclusion Top


In this case study, a 2-DOF mass conveyor belt system is built to investigate the problem of mode coupling vibration. The stability analysis of the system with Coulomb friction is carried out using the Routh criterion. The mathematical expression of the Hopf bifurcation point is given out using the Routh criterion. It is illustrated that both the frequency and the damping of the coupling modes have important effects on system stability and should be taken into account to avoid bad structure design. Moreover, the extended harmonic balance method is advanced, through which the analytic solutions of the limit cycle amplitudes of the nonlinear system are achieved. Furthermore, the effects of physical parameters on the size of limit cycles are discussed based on the analytic calculation. Among them, the values of the damping ratios should be considered carefully. All the work provides a better understanding of mode coupling mechanical system with Coulomb friction. And the methodology presented can be applied for mechanical structure design and parameter optimization.

 
   References Top

1.G. P. Ostermeyer, "Dynamic friction laws and their impacton friction induced vibrations", Proceedings of the 28th SAEB rake Colloquium and Exhibition, Phoenix, 2010.  Back to cited text no. 1
    
2.M. Graf, and G. P. Ostermeyer, "Instabilities in the sliding of continua with surface inertias: An initiation mechanism for brake noise", Journal of Sound and Vibration, Vol. 330, pp. 5269-5279, 2011.  Back to cited text no. 2
    
3.N. Hoffmann, M. Fischer, R. Allgaier, and L. Gaul, "A minimal modal for studying properties of the mode-coupling type instability in friction induced oscillations", Mechanics Research Communications, Vol. 29, pp.197-205, 2002.   Back to cited text no. 3
    
4.J. Kang, C. M. Krousgrill, and F. Sadeghi, "Comprehensive stability analysis of disc brake vibrations including gyroscopic, negative friction slope and mode-coupling mechanisms", Journal of Sound and Vibration, Vol. 324, pp. 387-407, 2009.  Back to cited text no. 4
    
5.J. Behrendt, C. Weiss, and N. P. Hoffmann, "A numerical study on stick-slip motion of a brake pad in steady sliding", Journal of Soundand Vibration, Vol. 330, pp. 636-651, 2011.   Back to cited text no. 5
    
6.J. Hultén, "Drum brake squeal--a self-exciting mechanism with constant friction", SAE Truck and Bus Conference, Detroit, pp. 695-706, 1993.   Back to cited text no. 6
    
7.J. Hultén, "Friction phenomena related to drum brake squeal instabilities", ASME Design Engineering Technical Conferences, Sacramento, pp. 588-596, 1997.  Back to cited text no. 7
    
8.J. J. Sinou, and L. Jézéquel, "Mode coupling instability in friction-induced vibrations and its dependency on system parameters including damping", European Journal of Mechanics A/Solids, Vol. 26, pp. 106-122, 2007.  Back to cited text no. 8
    
9.X. Y. Wu, and S. X. Zhang, "Automatic Control Theory", Xi'an, China: Xidian University Publications; 2008.  Back to cited text no. 9
    
10.N. Hoffmann, S. Bieser, and L. Gaul, "Harmonic balance and averaging techniques for stick-slip limit-cycle determination in mode-coupling friction self-excited systems", Technische Mechanik, Vol. 24, pp. 185-197, 2004.  Back to cited text no. 10
    

 
   Authors Top


Lilan Liu is teaching in Mechanical Engineering Department of Xi'an University of Technology, China. she graduated in 2002; post graduated in 2005 and got PhD in 2010 in area of Mechanical Engineering. Her areas of interest include mechanical system friction identification and compensation.



Ziying Wu is an Associate Professor in Mechanical Engineering Department at Xi'an University of Technology, China. He graduated in 1998; post graduated in 2002 and got PhD in 2007 in area of Mechanical Engineering. His areas of interest include mechanical system identification and control.


    Figures

  [Figure 1], [Figure 2], [Figure 3], [Figure 4], [Figure 5]
 
 
    Tables

  [Table 1], [Table 2]


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