Journal of Applied Mathematics

Journal of Applied Mathematics / 2012 / Article

Research Article | Open Access

Volume 2012 |Article ID 527878 |

Cai-Wan Chang-Jian, Shiuh Ming Chang, Hsieh-Chung Hsu, "Couple-Stress Fluid Improves Dynamic Response of Gear-Pair System Supported by Journal Bearings", Journal of Applied Mathematics, vol. 2012, Article ID 527878, 20 pages, 2012.

Couple-Stress Fluid Improves Dynamic Response of Gear-Pair System Supported by Journal Bearings

Academic Editor: Nazim I. Mahmudov
Received06 Jul 2011
Accepted18 Aug 2011
Published12 Dec 2011


A systematic analysis of the dynamic behavior of a gear-bearing system with nonlinear suspension, couple-stress fluid flow effect, nonlinear oil-film force, and nonlinear gear mesh force is performed in the present study. The dynamic orbits of the system are observed using bifurcation diagrams plotted using the dimensionless rotational speed ratio as a control parameter. The onset of chaotic motion is identified from the phase diagrams, power spectra, PoincarƩ maps, Lyapunov exponents and fractal dimension of the gear-bearing system. The numerical results reveal that the system exhibits a diverse range of periodic, subharmonic, quasiperiodic, and chaotic behaviors. The couple-stress fluid would be a useful lubricating fluid to suppress nonlinear dynamic responses and improve the steady of the systems. The results presented in this study provide some useful insights into the design and development of a gear-bearing system for rotating machinery that operates in highly rotational speed and highly nonlinear regimes.

1. Introduction

Lubricants with additives are often considered as non-Newtonian fluids and are found to be able to used to improve the properties of lubricants such as the viscosity of lubricants in many studies and also many applications. According to the results of experiments, it evidenced that the use of small amounts of suitable additives can improve lubricant properties. It can make the viscosity of the lubricant to be independent of the temperature. With the development of modern machine elements, the increasing use of complex fluids as lubricants has been emphasized. Oliver [1] had found that the presence of dissolved polymer in the lubricant could increase the load-carrying capacity and decrease the friction. Spikes [2] showed that the base oil blending with additives could reduce the friction and the surface damage in elastohydrodynamic contacts. Because of the behavior of the complex fluids violates the linear shear-stress-rate relationship, it fails to describe the rheological behaviour of the non-Newtonian fluid. Therefore, a different microcontinuum theory has been developed to better describe the rheological behaviour of the non-Newtonian fluid. Shehawey and Mekheimer [3] applied the couple-stress model to analyze the peristalsis problem for its relative mathematical simplicity. Das [4] proposed the analysis of elastohydrodynamic theory of line contacts. Das [5] studied the slider bearing lubricated with couple-stress fluids in magnetic field and observed that both the values of the maximum load capacity, and corresponding inlet-outlet film ratio depend on couple stress, magnetic parameters and the shape of bearings. Elsharkawy and Guedouar [6] proposed an efficient numerical scheme to solve the direct lubrication problem for journal bearings lubricated with couple stress fluids, which consists of the modified Reynolds equation, the film thickness equation, and the boundary conditions for the pressure field. Hsu et al. [7] studied the short journal bearings lubricated with the non-Newtonian fluid which is combined with the effects of couple-stresses and surface roughness. It was found that the combined effects of couple stress and surface roughness can improve the load-carrying capacity and decrease the attitude angle and friction parameters. Lahmar [8] also found that the lubricants with couple stress would increase the load-carrying capacity and stability and decrease the friction factor and the attitude angle. The above researches are all about the applications of the couple-stress fluids, and all the results of their studies emphasized that the couple-stress fluids are more superior and more stable than the traditional Newtonian fluids. Chang-Jian and Chen [9] found couple-stress fluid can be used to suppress nonperiodic or even chaotic dynamic response especially for higher rotating speeds in rotor-bearing systems.

Gears have played important roles in power transmission, and therefore the study of gear dynamics is necessary. Many studies have focused on analyzing gear dynamics or relative researches. Vedmar and Andersson [10] presented a method to calculate dynamic gear tooth force and bearing forces and the bearing model was under elastic bearings assumption. The simulation results of elastic model were somewhat different comparing with stiff one. The gear mesh model used with constant was studied by a lot of people, such as Kahraman and Singh [11], Lin et al. [12], Yoon and Rao [13], and Ichimaru and Hirano [14]. Amabili and Fregolent [15] introduced a method based on the measurement of the gear torsional vibrations to identify natural frequency, damping parameters, and equivalent gear error of a spur-gear-pair model. ƖzgĆ¼ven and Houser [16, 17] performed dynamic analysis on gears with the effects of variable mesh stiffness, damping, gear errors profile modification, and backlash. Cai and Hayashi [18] calculated the optimum profile modification to obtain a zero vibration of the gear pair. Umezawa et al. [19] analyzed a single DOF numerical gear pair model and compared their numerical results with experimental dynamic transmission errors. McFadden and Toozhy [20] used the high-frequency technique combined with synchronous averaging to detect the failure in rolling element bearings. Litvin et al. [21] proposed a modified geometry of an asymmetric spur-gear drive designed as a favorable shape of transmission errors of reduced magnitude and also reduced contact and bending stresses for an asymmetric spur-gear drive. Guan et al. [22] performed finite-element method to simulate the geared rotor system constructed from beam and lumped mass/stiffness elements and compared the required actuation effort, control robustness, and implementation cost. Giagopulos et al. [23] presented an analysis on the nonlinear dynamics of a gear-pair system supported on rolling element bearings and used a suitable genetic algorithm to measure noise and model error. Theodossiades and Natsiavas [24] investigated dynamic responses and stability characteristics of rotordynamic systems interconnected with gear pairs, supported on oil journal bearings. They found many nonperiodic dynamic behaviors. They [25] also analyzed the motor-driven gear-pair systems with backlash and found periodic and chaotic dynamics in this system.

Although virtually all physical phenomena in the real world can be regarded as nonlinear, most of these phenomena can be simplified to a linear form given a sufficiently precise linearization technique. However, this simplification is inappropriate for high-power, high-rotational-speed gear system, and its application during the design and analysis stage may result in a flawed or potentially dangerous operation. As a result, nonlinear analysis methods are generally preferred within engineering and academic circles. The current study performs a nonlinear analysis of the dynamic behavior of a gear-pair system equipped with couple-stress fluid lubricated journal bearings under nonlinear suspension. The nondimensional equation of the gear-bearing system is then solved using the Runge-Kutta method. The nonperiodic behavior of this system is characterized by using phase diagrams, power spectra, PoincarƩ maps, bifurcation diagrams, Lyapunov exponents, and the fractal dimension of the system.

2. Mathematical Modeling

2.1. Nonlinear Dynamic Models

Some assumptions are presented to simplify dynamic models to be able to simulate the gear-bearing system, that is, nonlinear suspension (hard spring effect), short journal bearing, nonlinear gear meshing force, and nonlinear couple-stress fluid film force effect are established. Figure 1 shows the gear-baring model presented in this study. The equations of motion used to describe geometric centers of gear and pinion (š‘‚š‘”(š‘‹š‘”,š‘Œš‘”) and š‘‚š‘(š‘‹š‘,š‘Œš‘)) can be written asš‘šš‘Ģˆš‘‹š‘Ģ‡š‘‹+š¶š‘ī€·š‘‹+š¾š‘āˆ’š‘‹š‘—1ī€ø=š‘Šš‘š‘„,š‘šš‘Ģˆš‘Œš‘Ģ‡š‘Œ+š¶š‘ī€·š‘Œ+š¾š‘āˆ’š‘Œš‘—1ī€ø=šæš‘š‘¦āˆ’šŗš‘š‘¦āˆ’š‘Šš‘š‘¦āˆ’š‘šš‘š‘šš‘”,š‘”Ģˆš‘‹š‘”Ģ‡š‘‹+š¶š‘”ī€·š‘‹+š¾š‘”āˆ’š‘‹š‘—š‘”ī€ø=āˆ’š‘Šš‘š‘„,š‘šš‘”Ģˆš‘Œš‘”Ģ‡š‘Œ+š¶š‘”ī€·š‘Œ+š¾š‘”āˆ’š‘Œš‘—2ī€ø=šæš‘š‘¦āˆ’šŗš‘š‘¦+š‘Šš‘š‘¦āˆ’š‘šš‘”š‘”,(2.1) where šæš‘š‘¦ and šæš‘”š‘¦ are the centrifugal forces in the vertical gear mesh direction for pinion and gear, šŗš‘š‘¦ and šŗš‘”š‘¦ are the inertia forces in the vertical gear mesh direction for pinion and gear, š‘Šš‘š‘„ is the dynamic gear mesh force in the horizontal direction, and š‘Šš‘š‘¦ is the dynamic gear mesh force in the vertical direction.

The equations of motion of the center of bearing 1 (š‘‹1,š‘Œ1) and the center of bearing 2 (š‘‹2,š‘Œ2) under the assumption of nonlinear suspension can be written asš‘š1Ģˆš‘‹1+š‘1Ģ‡š‘‹1+š‘˜11š‘‹1+š‘˜12š‘‹31=š¹š‘„1,š‘š1Ģˆš‘Œ1+š‘1Ģˆš‘Œ1+š‘˜11š‘Œ1+š‘˜12š‘Œ31=āˆ’š‘š1š‘”+š¹š‘¦1,š‘š2Ģˆš‘‹2+š‘2Ģ‡š‘‹2+š‘˜21š‘‹2+š‘˜22š‘‹32=š¹š‘„2,š‘š2Ģˆš‘Œ2+š‘2Ģˆš‘Œ2+š‘˜21š‘Œ2+š‘˜22š‘Œ32=āˆ’š‘š2š‘”+š¹š‘¦2.(2.2) According to the principles of force equilibrium, the forces acting at the center of journal 1, that is, š‘‚š‘—1(š‘‹š‘—1,š‘Œš‘—1) and center of journal 2, that is, š‘‚š‘—2(š‘‹š‘—2,š‘Œš‘—2) are given byš¹š‘„1=š‘“š‘’1cosšœ‘1+š‘“šœ‘1sinšœ‘1=š¾š‘1ī€·š‘‹š‘āˆ’š‘‹š‘—1ī€ø2,š¹š‘¦1=š‘“š‘’1sinšœ‘1āˆ’š‘“šœ‘1cosšœ‘1=š¾š‘1ī€·š‘Œš‘āˆ’š‘Œš‘—1ī€ø2,š¹š‘„2=š‘“š‘’2cosšœ‘2+š‘“šœ‘2sinšœ‘2=š¾š‘2ī€·š‘‹š‘”āˆ’š‘‹š‘—2ī€ø2,š¹š‘¦2=š‘“š‘’2sinšœ‘2āˆ’š‘“šœ‘2cosšœ‘2=š¾š‘2ī€·š‘Œš‘”āˆ’š‘Œš‘—2ī€ø2,(2.3) in which š‘“š‘’1 and š‘“šœ‘1 are the viscous damping forces in the radial and tangential directions for the center of journal 1, respectively, and š‘“š‘’2 and š‘“šœ‘2 are the viscous damping forces in the radial and tangential directions for the center of journal 2, respectively.

2.2. Nonlinear Couple-Stress Fluid Film Force

The non-Newtonian Reynolds-type equation can be performed asšœ•ī‚µšœ•š‘„š‘”(ā„Ž,š‘™)šœ•š‘ī‚¶+šœ•šœ•š‘„ī‚µšœ•š‘§š‘”(ā„Ž,š‘™)šœ•š‘ī‚¶šœ•š‘§=6šœ‡š‘ˆšœ•ā„Žšœ•š‘„+12šœ‡šœ•ā„Žšœ•š‘”,(2.4) where š‘”(ā„Ž,š‘™)=ā„Ž3āˆ’12š‘™2ā„Ž+24š‘™3tanā„Ž(ā„Ž/2š‘™), šœ•ā„Ž/šœ•x=āˆ’(š‘šœ€/š‘…)sinšœƒ, šœ•ā„Ž/šœ•š‘”=š‘Ģ‡šœ€cosšœƒ+š‘šœ€Ģ‡šœ‘sinšœƒ, š‘„=š‘…šœƒ, š‘ˆ=š‘…šœ”, šœ€=š‘’/š‘, and ā„Ž=š‘(1+šœ€cos(š›¾āˆ’šœ‘(š‘”)))=š‘(1+šœ€cosšœƒ). Thus š‘”(ā„Ž,š‘™) can also be performed as š‘”(ā„Ž,š‘™)=š‘3(1+šœ€cosšœƒ)3āˆ’12š‘™2š‘(1+šœ€cosšœƒ)+24š‘™3tanā„Ž(š‘(1+šœ€cosšœƒ)/2š‘™), where š‘™=(šœ‚/šœ‡)1/2, in which šœ‡ is the classical viscosity parameter and šœ‚ is a new material constant peculiar to fluids with couple stresses and Reynolds equation that can be rewritten asšœ•ī‚µš‘…šœ•šœƒš‘”(ā„Ž,š‘™)šœ•š‘ī‚¶+šœ•š‘…šœ•šœƒī‚µšœ•š‘§š‘”(ā„Ž,š‘™)šœ•š‘ī‚¶šœ•š‘§=āˆ’6šœ‡šœ”š‘šœ€sinšœƒ+12šœ‡(š‘Ģ‡šœ€cosšœƒ+š‘šœ€Ģ‡šœ‘sinšœƒ).(2.5) Using the ā€œshort bearing approximationā€ (šæ/š·<0.25, šœ•š‘/šœ•šœƒā‰Ŗšœ•š‘/šœ•š‘§), then we can set šœ•š‘/šœ•šœƒ=0. The following equation can be introduced:šœ•2š‘šœ•š‘§2=āˆ’6šœ‡šœ”š‘šœ€sinšœƒ+12šœ‡(š‘Ģ‡šœ€cosšœƒ+š‘šœ€Ģ‡šœ‘sinšœƒ)š‘”(ā„Ž,š‘™).(2.6)

The resulting damping forces about the journal center in the radial and tangential directions are determined by integrating pressure distribution over the area of the journal sleeve:š‘“š‘’ī€œ=š¹cosšœ‘=šæ0š‘Ÿī€œ02šœ‹š‘“š‘(šœƒ)cosšœƒš‘‘šœƒš‘‘š‘§,(2.7)šœ‘ī€œ=š¹sinšœ‘=šæ0š‘Ÿī€œ02šœ‹š‘(šœƒ)sinšœƒš‘‘šœƒš‘‘š‘§.(2.8) Substituting (2.7) and (2.8) into (2.2)ā€“(2.3) enables the values of š¹š‘„1, š¹š‘„2, š¹š‘¦1, and š¹š‘¦2 to be obtained.

2.3. Nonlinear Gear Meshing Force

Figure 2 presents a schematic illustration of the dynamic model considered between gear and pinion. šæš‘š‘¦ and šæš‘”š‘¦ are the centrifugal forces in the vertical gear mesh direction for pinion and gear, šŗš‘š‘¦ and šŗš‘”š‘¦ are the inertia forces in the vertical gear mesh direction for pinion and gear, š‘Šš‘š‘„ is the dynamic gear mesh force in the horizontal direction, and š‘Šš‘š‘¦ is the dynamic gear mesh force in the vertical direction. Thus, šæš‘š‘¦, šæš‘”š‘¦, šŗš‘š‘¦, šŗš‘”š‘¦, š‘Šš‘š‘„, and š‘Šš‘š‘¦ can be performed asšæš‘š‘¦=š‘šš‘š‘’š‘šœ”2š‘sinšœƒ1,šæš‘”š‘¦=š‘šš‘”š‘’š‘”šœ”2š‘”sinšœƒ2,šŗš‘š‘¦=š‘šš‘š‘’š‘Ģˆšœƒ1cosšœƒ1,šŗš‘”š‘¦=š‘šš‘”š‘’š‘”Ģˆšœƒ2cosšœƒ2,š‘Šš‘š‘„=š¶š‘šī€·Ģ‡š‘‹š‘āˆ’Ģ‡š‘‹š‘”āˆ’š‘’š‘ī€øĪ©sin(Ī©š‘”)+š¾š‘šī€·š‘‹š‘āˆ’š‘‹š‘”āˆ’š‘’š‘ī€ø,š‘Šcos(Ī©š‘”)š‘š‘¦=š¶š‘šī€·Ģ‡š‘Œš‘āˆ’Ģ‡š‘Œš‘”āˆ’š‘’š‘ī€øĪ©cos(Ī©š‘”)+š¾š‘šī€·š‘Œš‘āˆ’š‘Œš‘”āˆ’š‘’š‘ī€ø.sin(Ī©š‘”)(2.9) Substituting (2.9) into (2.1) enables the values of šæš‘š‘¦, šæš‘”š‘¦, šŗš‘š‘¦, šŗš‘”š‘¦, š‘Šš‘š‘„, and š‘Šš‘š‘¦ to be obtained.

2.4. Dimensionless of Nonlinear Dynamic Models

Couple-stress fluid film force and gear meshing force would be introduced in Equations (2.1)ā€“(2.3) and can be nondimensionalized to yield the following equations: šœ€ī…ž1=š›½1š‘š¾š‘š‘¦ī€ŗī€·š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€øcosšœ‘1āˆ’ī€·š‘„š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øsinšœ‘1ī€»4š›¼1ī€·š›¾1š›æ1āˆ’š›½12ī€øšœ”āˆ’š›æ1š‘š¾š‘š‘„ī€ŗī€·š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øcosšœ‘1+ī€·š‘¦š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€øsinšœ‘1ī€»4š›¼1ī€·š›¾1š›æ1āˆ’š›½12ī€øšœ”,šœ‘ī…ž1=12āˆ’š‘š¾š‘š‘¦ī€ŗī€·š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€øcosšœ‘1āˆ’ī€·š‘„š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øsinšœ‘1ī€»4š›¼1š›æ1šœ€1šœ”āˆ’īƒ©š›½12š‘š¾š‘š‘¦ī€ŗī€·š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€øcosšœ‘1āˆ’ī€·š‘„š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øsinšœ‘1ī€»4š›¼1šœ€1š›æ1ī€·š›¾1š›æ1āˆ’š›½12ī€øšœ”āˆ’š›½1š›æ1š‘š¾š‘š‘„ī€ŗī€·š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øcosšœ‘1+ī€·š‘¦š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€øsinšœ‘1ī€»4š›¼1šœ€1š›æ1ī€·š›¾1š›æ1āˆ’š›½12ī€øšœ”īƒŖ,šœ€ī…ž2=š›½2š‘š¾š‘š‘¦ī€ŗī€·š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€øcosšœ‘2āˆ’ī€·š‘„š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€øsinšœ‘2ī€»4š›¼2ī€·š›¾2š›æ2āˆ’š›½22ī€øšœ”āˆ’š›æ2š‘š¾š‘š‘„ī€ŗī€·š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€øcosšœ‘2+ī€·š‘¦š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€øsinšœ‘2ī€»4š›¼2ī€·š›¾2š›æ2āˆ’š›½22ī€øšœ”,šœ‘ī…ž2=12āˆ’š‘š¾š‘š‘¦ī€ŗī€·š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€øcosšœ‘2āˆ’ī€·š‘„š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€øsinšœ‘2ī€»4š›¼2š›æ2šœ€2šœ”āˆ’īƒ©š›½22š‘š¾š‘š‘¦ī€ŗī€·š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€øcosšœ‘2āˆ’ī€·š‘„š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€øsinšœ‘2ī€»4š›¼2šœ€2š›æ2ī€·š›¾2š›æ2āˆ’š›½22ī€øšœ”āˆ’š›½2š›æ2š‘š¾š‘š‘„ī€ŗī€·š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€øcosšœ‘2+ī€·š‘¦š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€øsinšœ‘2ī€»4š›¼2šœ€2š›æ2ī€·š›¾2š›æ2āˆ’š›½22ī€øšœ”īƒŖ,š‘„š‘ī…žī…ž=āˆ’2šœ‰2š‘ š‘„ī…žš‘āˆ’1š‘ 2ī€·š‘„š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øī‚µšœ™+š›½cos4ī‚¶āˆ’2šœ‰3š‘ ī€·š‘„ī…žš‘āˆ’š‘„ī…žš‘”āˆ’šøš‘ī€øāˆ’Ī›sinšœ™š‘ 2ī€·š‘„š‘āˆ’š‘„š‘”āˆ’šøš‘ī€ø,š‘¦cosšœ™š‘ī…žī…ž=āˆ’2šœ‰2š‘ š‘¦ī…žš‘āˆ’1š‘ 2ī€·š‘¦š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€øī‚µšœ™+š›½sin4ī‚¶āˆ’2šœ‰3š‘ ī€·š‘¦ī…žš‘āˆ’š‘¦ī…žš‘”āˆ’šøš‘ī€øāˆ’Ī›cosšœ™š‘ 2ī€·š‘¦š‘āˆ’š‘¦š‘”āˆ’šøš‘ī€øāˆ’š‘“sinšœ™š‘ 2,š‘„š‘”ī…žī…ž=āˆ’2šœ‰4š‘ š‘„ī…žš‘”āˆ’1š‘ 2ī€·š‘„š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€ø+š›½š‘”ī‚µšœ™cos8ī‚¶+2šœ‰5š‘ ī€·š‘„ī…žš‘āˆ’š‘„ī…žš‘”āˆ’šøš‘ī€øāˆ’Ī›sinšœ™š‘”š‘ 2ī€·š‘„š‘āˆ’š‘„š‘”āˆ’šøš‘ī€ø,š‘¦cosšœ™š‘”ī…žī…ž=āˆ’2šœ‰4š‘ š‘¦ī…žš‘”āˆ’1š‘ 2ī€·š‘¦š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€ø+š›½š‘”ī‚µšœ™sin8ī‚¶+2šœ‰5š‘ ī€·š‘¦ī…žš‘āˆ’š‘¦ī…žš‘”āˆ’šøš‘ī€ø+Ī›cosšœ™š‘”š‘ 2ī€·š‘¦š‘āˆ’š‘¦š‘”āˆ’šøš‘ī€øāˆ’š‘“sinšœ™š‘”š‘ 2,š‘„1ī…žī…ž+2šœ‰1š‘ 1š‘„1ī…ž+1š‘ 12š‘„1+š›¼1š‘ 2š‘„13āˆ’12š¶1š‘š‘ 2ī€·š‘„š‘āˆ’š‘„1āˆ’šœ€1cosšœ‘1ī€øš‘¦=0,1ī…žī…ž+2šœ‰1š‘ 1š‘¦1ī…ž+1š‘ 12š‘¦1+š›¼1š‘ 2š‘¦13āˆ’12š¶š‘œš‘šš‘ 2ī€·š‘¦š‘āˆ’š‘¦1āˆ’šœ€1sinšœ‘1ī€ø+š‘“š‘ 2š‘„=0,2ī…žī…ž+2šœ‰6š‘ 2š‘„2ī…ž+1š‘ 22š‘„2+š›¼2š‘ 2š‘„23āˆ’12š¶2š‘š‘ 2ī€·š‘„š‘”āˆ’š‘„2āˆ’šœ€2cosšœ‘2ī€øš‘¦=0,2ī…žī…ž+2šœ‰6š‘ 2š‘¦2ī…ž+1š‘ 22š‘¦2+š›¼2š‘ 2š‘¦23āˆ’12š¶2š‘š‘ 2ī€·š‘¦š‘”āˆ’š‘¦2āˆ’šœ€2sinšœ‘2ī€ø+š‘“š‘ 2=0,(2.10) whereš›¼1=āˆ’šœ‡šæ3š‘…2š‘2,š›½1=ī€œšœ‹0sinšœƒcosšœƒī‚ƒī€·1+šœ€1ī€øcosšœƒ3ī€·š‘™āˆ’12āˆ—ī€ø2ī€·1+šœ€1ī€øī€·š‘™cosšœƒ+24āˆ—ī€ø3tanhī€·ī€·1+šœ€1ī€øcosšœƒ/2š‘™āˆ—ī€øī‚„š›¾š‘‘šœƒ,1=ī€œšœ‹0š‘š‘œš‘ 2šœƒī‚ƒī€·1+šœ€1ī€øcosšœƒ3ī€·š‘™āˆ’12āˆ—ī€ø2ī€·1+šœ€1ī€øī€·š‘™cosšœƒ+24āˆ—ī€ø3tanhī€·ī€·1+šœ€1ī€øcosšœƒ/2š‘™āˆ—ī€øī‚„š›æš‘‘šœƒ,1=ī€œšœ‹0sin2šœƒī‚ƒī€·1+šœ€1ī€øcosšœƒ3ī€·š‘™āˆ’12āˆ—ī€ø2ī€·1+šœ€1ī€øī€·š‘™cosšœƒ+24āˆ—ī€ø3tanhī€·ī€·1+šœ€1ī€øcosšœƒ/2š‘™āˆ—ī€øī‚„š›¼š‘‘šœƒ,2=āˆ’šœ‡šæ3š‘…2š‘2,š›½2=ī€œšœ‹0sinšœƒcosšœƒī‚ƒī€·1+šœ€2ī€øcosšœƒ3ī€·š‘™āˆ’12āˆ—ī€ø2ī€·1+šœ€2ī€øī€·š‘™cosšœƒ+24āˆ—ī€ø3tanhī€·ī€·1+šœ€2ī€øcosšœƒ/2š‘™āˆ—ī€øī‚„š›¾š‘‘šœƒ,2=ī€œšœ‹0cos2šœƒī‚ƒī€·1+šœ€2ī€øcosšœƒ3ī€·š‘™āˆ’12āˆ—ī€ø2ī€·1+šœ€2ī€øī€·š‘™cosšœƒ+24āˆ—ī€ø3tanhī€·ī€·1+šœ€2ī€øcosšœƒ/2š‘™āˆ—ī€øī‚„š›æš‘‘šœƒ,2=ī€œšœ‹0sin2šœƒī‚ƒī€·1+šœ€2ī€øcosšœƒ3ī€·š‘™āˆ’12āˆ—ī€ø2ī€·1+šœ€2ī€øī€·š‘™cosšœƒ+24āˆ—ī€ø3tanhī€·ī€·1+šœ€2ī€øcosšœƒ/2š‘™āˆ—ī€øī‚„š‘‘šœƒ,(2.11) where š‘™āˆ—=š‘™/š‘ is the dimensionless parameter for š‘™.

Equation (2.10) describes a nonlinear dynamic system. In the current study, the approximate solutions of these coupled non-linear differential equations are obtained using the fourth-order Runge-Kutta numerical scheme.

3. Analytical Tools for Observing Nonlinear Dynamics of Gear-Bearing System

In the present study, the nonlinear dynamics of the gear-bearing system shown in Figure 1 are analyzed using PoincarĆ© maps, bifurcation diagrams, Lyapunov exponent, and fractal dimension. The dynamic trajectories of the gear-bearing system provide a basic indication as to whether the system behavior is periodic or nonperiodic. The projection of the PoincarĆ© section on the š‘¦(š‘›š‘‡) plane is referred to as the PoincarĆ© map of the dynamic system. When the system performs quasiperiodic motion, the return points in the PoincarĆ© map form a closed curve. For chaotic motion, the return points form a fractal structure comprising many irregularly distributed points. Finally, for š‘›š‘‡-periodic motion, the return points have the form of n discrete points. In this study, the spectrum components of the motion performed by the gear-bearing system are analyzed by using the Fast Fourier Transformation method to derive the power spectrum of the displacement of the dimensionless dynamic transmission error. In the analysis, the frequency axis of the power spectrum plot is normalized using the rotational speed, šœ”.

A bifurcation diagram summarizes the essential dynamics of a gear-train system and is therefore a useful means of observing its nonlinear dynamic response. In the present analysis, the bifurcation diagrams are generated using the dimensionless rotational speed ratio, š‘ , to be a control parameter. In each case, the bifurcation control parameter is varied with a constant step and the state variables at the end of one integration step are taken as the initial values for the next step. The corresponding variations of the š‘¦(š‘›š‘‡) coordinates of the return points in the PoincarĆ© map are then plotted to form the bifurcation diagram.

The Lyapunov exponent of a dynamic system characterizes the rate of separation of infinitesimally close trajectories and provides a useful test for the presence of chaos. In a chaotic system, the points of nearby trajectories starting initially within a sphere of radius šœ€0 form after time š‘” an approximately ellipsoidal distribution with semiaxes of length šœ€š‘—(š‘”). The Lyapunov exponents of a dynamic system are defined by šœ†š‘—=limš‘”ā†’āˆž(1/š‘”)log(šœ€š‘—(š‘”)/šœ€0), where šœ†š‘— denotes the rate of divergence of the nearby trajectories. The exponents of a system are usually ordered into a Lyapunov spectrum, that is, šœ†1>šœ†2>ā‹Æ>šœ†š‘š. A positive value of the maximum Lyapunov exponent (šœ†1) is generally taken as an indication of chaotic motion.

The presence of chaotic vibration in a system is generally detected using either the Lyapunov exponent or the fractal dimension property. The Lyapunov exponent test can be used for both dissipative systems and nondissipative (i.e., conservative) systems, but it is not easily applied to the analysis of experimental data. Conversely, the fractal dimension test can only be used for dissipative systems, but it is easily applied to experimental data. In contrast to Fourier transform-based techniques and bifurcation diagrams, which provide only a general indication of the change from periodic motion to chaotic behavior, dimensional measures allow chaotic signals to be differentiated from random signals. Although many dimensional measures have been proposed, the most commonly applied measure is the correlation dimension š‘‘šŗ defined by Grassberger and Procaccia due to its computational speed and the consistency of its results. However, before the correlation dimension of a dynamic system flow can be evaluated, it is first necessary to generate a time series of one of the system variables using a time-delayed pseudo-phase-plane method. Assume an original time series of š‘„š‘–={š‘„(š‘–šœ);š‘–=1,2,3,ā€¦š‘}, where šœ is the time delay (or sampling time). If the system is acted upon by an excitation force with a frequency šœ”, the sampling time, šœ, is generally chosen such that it is much smaller than the driving period. The delay coordinates are then used to construct an n-dimensional vector š‘‹=(š‘„(š‘—šœ), š‘„[(š‘—+1)šœ], š‘„[(š‘—+2)šœ],ā€¦, š‘„[(š‘—+š‘›āˆ’1)šœ]), where š‘—=1,2,3,ā€¦(š‘āˆ’š‘›+1). The resulting vector comprises a total of (š‘āˆ’š‘›+1) vectors, which are then plotted in an n-dimensional embedding space. Importantly, the system flow in the reconstructed n-dimensional phase space retains the dynamic characteristics of the system in the original phase space. In other words, if the system flow has the form of a closed orbit in the original phase plane, it also forms a closed path in the n-dimensional embedding space. Similarly, if the system exhibits a chaotic behavior in the original phase plane, its path in the embedding space will also be chaotic. The characteristics of the attractor in the n-dimensional embedding space are generally tested using the function āˆ‘š‘š‘–,š‘—=1š»(š‘Ÿāˆ’|š‘„š‘–āˆ’š‘„š‘—|) to determine the number of pairs (š‘–,š‘—) lying within a distance |š‘„š‘–āˆ’š‘„š‘—|<š‘Ÿ in {š‘„š‘–}š‘š‘–=1, where š» denotes the Heaviside step function, š‘ represents the number of data points, and r is the radius of an n-dimensional hyper-sphere. For many attractors, this function exhibits a power law dependence on š‘Ÿ as š‘Ÿā†’0, that is, š‘(š‘Ÿ)āˆš‘Ÿš‘‘šŗ. Therefore, the correlation dimension, š‘‘šŗ, can be determined from the slope of a plot of [logš‘(š‘Ÿ)] versus [logš‘Ÿ]. Grassberger and Procaccia [26] showed that the correlation dimension represents the lower bound to the capacity or fractal dimension š‘‘š‘ and approaches its value asymptotically when the attracting set is distributed more uniformly in the embedding phase space. A set of points in the embedding space is said to be fractal if its dimension has a finite noninteger value. Otherwise, the attractor is referred to as a ā€œstrange attractor.ā€ To establish the nature of the attractor, the embedding dimension is progressively increased, causing the slope of the characteristic curve to approach a steady-state value. This value is then used to determine whether the system has a fractal structure or a strange attractor structure. If the dimension of the system flow is found to be fractal (i.e., to have a noninteger value), the system is judged to be chaotic.

4. Numerical Results and Discussions

The nonlinear dynamic equations presented in (2.10) for the gear-bearing system with nonlinear suspension effects, couple-stress fluid effect, strongly nonlinear oil-film force, and nonlinear gear mesh force were solved using the fourth-order Runge-Kutta method. The time step in the iterative solution procedure was assigned a value of šœ‹/300 and the termination criterion was specified as an error tolerance of less than 0.0001. The time series data corresponding to the first 800 revolutions of the two gears were deliberately excluded from the dynamic analysis to ensure that the analyzed data related to steady-state conditions. The sampled data were used to generate the dynamic trajectories, PoincarĆ© maps, and bifurcation diagrams of the spur-gear system in order to obtain a basic understanding of its dynamic behavior. The maximum Lyapunov exponent and the fractal dimension measure were then used to identify the onset of chaotic motion. For convenience, only the data of the displacements in the vertical direction were used to generate diagrams.

The rotational speed ratio š‘  is commonly used as a control parameter for bifurcation diagrams to analyze nonlinear behaviors of rotor-dynamics, gear-dynamics, bearing systems or machine tools. Accordingly, the dynamic behavior of the current gear-bearing system was examined using the dimensionless rotational speed ratio š‘  as a bifurcation control parameter. Figures 2, 3, 4 and 5 are the bifurcation diagrams for the gear-bearing system displacement against the dimensionless rotational speed ratio, š‘ , for non-Newtonian lubricating fluid with š‘™āˆ—=0.0,0.1,0.3, and 0.5 to describe corresponding dynamic responses. It can be observed that the dynamic behaviors of bearing center and gear center show abundant nonperiodic responses at low speeds. The dynamic behaviors become steady and come into subharmonic motions as rotating with high speed but would behave nonperiodic vibrations and higher amplitude for higher rotating speeds (i.e., š‘ >3.0). It is said that the couple-stress fluid can improve lubricating conditions and therefore can enhance dynamic responses for turbomachineries. According to bifurcation results, we would find dynamic behaviors show different results with different š‘™āˆ—. When š‘™āˆ—=0.0, lubricating fluid as Newtonian fluid and the effect of couple-stress fluid would be greater as š‘™āˆ— becomes greater. The results show that the range of nonperiodic motions or subharmonic vibrations would be shortened and the amplitude of the systems would also be suppressed as š‘™āˆ— increases. Nevertheless, higher values of š‘™āˆ— could not suppress nonperiodic vibrations occurring at high speeds. We also find that the dynamic behaviors of bearing center and gear center are nonsynchronous and the couple-stress fluid can not also improve gear-dynamics as š‘™āˆ— increases.

Figures 6(a) and 6(b) present the bifurcation diagrams for the gear-bearing system displacement against the dimensionless rotational speed ratio, š‘ , for non-Newtonian lubricating fluid with š‘™āˆ—=0.3 and some dynamic trajectories and PoincarĆ© maps (e.g., š‘ =0.1, 0.6, 0.8, 1.3, 2.0, 3.4, and 5.0) are exemplified to describe corresponding dynamic responses. The bifurcation diagram of bearing center shows quasiperiodic responses at low speeds as š‘ <0.15 and turns to nonperiodic or even chaotic motions as š‘ >0.15. When rotating speed becomes greater (š‘ >1.39), the dynamic responses behave š‘›š‘‡-periodic motions, but dynamic responses of bearing center present strongly nonperiodic motions and the amplitude of the system is also greater than the amplitude of lower rotating speeds. Figures 7, 8, 9, 10, 11, and 12 are simulation results of phase diagrams, power spectra, PoincarĆ© maps, Lyapunov exponent and fractal dimension with š‘ =0.8, 1.0, 1.2, 3.6, 4.2, and 5.0 for š‘¦1 (š‘™āˆ—=0.3). In the above case, the phase diagrams are highly disordered and the power spectra reveal numerous excitation frequencies. Furthermore, it can be seen that the return points in the PoincarĆ© maps form geometrically fractal structures and the maximum Lyapunov exponent is positive in each case. In other words, the results presented in these figures all indicate that the gear center exhibits a chaotic behavior at those values.

5. Conclusions

This study has performed a numerical analysis of the nonlinear dynamic response of a gear-bearing system subject to nonlinear suspension effects, couple-stress fluid effect, nonlinear oil-film force, and nonlinear gear mesh force. The dynamics of the system have been analyzed by reference to its dynamic trajectories, power spectra, PoincarĆ© maps, bifurcation diagrams, maximum Lyapunov exponents, and fractal dimensions. When rotating machineries are turned on, they must meet low rotating speeds and according to the results shown in the bifurcation diagrams, the dynamic behaviors are strongly nonperiodic responses at low rotating speeds. As š‘™āˆ— increases, we can find that the range of nonperiodic motions becomes shorter and amplitude of the systems is also suppressed. Thus, we may conclude that couple-stress fluid can be used to improve dynamics of systems and help the systems escaping nonperiodic responses to be steady.


š‘:Radial clearance, š‘=š‘…āˆ’š‘Ÿ
š¶:Damping coefficient of the gear mesh
š¶1:Damping coefficients of the supported structure for bearing 1
š¶2:Damping coefficients of the supported structure for bearing 2
š¶1š‘:Dimensionless parameter, š¶1š‘=š‘š1/š‘šš‘
š¶01:Dimensionless parameter, š¶01=š¾/š‘˜1
š¶2š‘:Dimensionless parameter, š¶2š‘=š‘š2/š‘šš‘
š¶02:Dimensionless parameter, š¶02=š¾/š‘˜2
š‘’:Static transmission error and varies as a function of time
š‘’š‘–:Offset of the journal center of the rotor relative to the š‘‹-coordinate direction
š‘“:Dimensionless parameter, š‘“=š‘šš‘š‘”/š‘‘š¾
š‘“š‘”:Dimensionless parameter, š‘“š‘”=š¾š‘”/š‘‘š‘šš‘
š‘“š‘’, š‘“šœ‘:Components of the fluid film force in radial and tangential directions
š‘”:Acceleration of gravity
š¾:Stiffness coefficient of the gear mesh
š¾11, š¾12:Stiffness coefficients of the springs supporting the two bearing housings for bearing 1
š¾21, š¾22:Stiffness coefficients of the springs supporting the two bearing housings for bearing 2
š¾š‘1, š¾š‘2:Stiffness coefficients of the shafts
šæ:Bearing length
š‘š1:Mass of the bearing housing for bearing 1
š‘š2:Mass of the bearing housing for bearing 2
š‘šš‘:Mass of the pinion
š‘šš‘”:Mass of the gear
š‘‚1:Geometric centers of the bearing 1
š‘‚2:Geometric centers of the bearing 2
š‘‚š‘—1:Geometric centers of the journal 1
š‘‚š‘—2:Geometric centers of the journal 2
š‘‚š‘”:Center of gravity of the gear
š‘‚š‘:Center of gravity of the pinion
š‘:Pressure distribution in the fluid film
š‘…:Inner radius of the bearing housing
š‘Ÿ:Radius of the journal
š‘ :Rotational speed ratio, š‘ =(šœ”2/šœ”š‘›2)1/2
š‘ 1:Dimensionless parameter, š‘ 12=š¶š‘œ1š¶1š‘š‘ 2
š‘ 2:Dimensionless parameter, š‘ 22=š¶š‘œ2š¶2š‘š‘ 2
š‘‹, š‘Œ, š‘:Horizontal, vertical and axial coordinates
š‘„š‘—, š‘¦š‘—:š‘‹š‘—/š‘, š‘Œš‘—/š‘,ā€‰ā€‰š‘—=1,2,š‘—1,š‘—2,š‘,š‘”
š›¼1:Dimensionless parameter, š›¼1=š¾12š‘‘2š¾/š‘š1š‘šš‘
š›¼2:Dimensionless parameter, š›¼2=š¾22š‘‘2š¾/š‘š2š‘šš‘
šœ‰1:Dimensionless parameter, šœ‰1=š¶1āˆš/2š¾1š‘š1
šœ‰2:Dimensionless parameter, šœ‰2āˆš=š¶/2š¾š‘šš‘
šœ‰3:Dimensionless parameter, šœ‰3=š¶š‘šāˆš/2š¾š‘šš‘
šœ‰4:Dimensionless parameter, šœ‰4āˆšāˆ¶š¶/2š¾/š‘šš‘š‘šš‘”
šœ‰5:Dimensionless parameter, šœ‰5=š¶š‘šāˆšš‘šš‘/2š‘šš‘”āˆšš¾
šœ‰6:Dimensionless parameter, šœ‰6=š¶2āˆš/2š¾2š‘š2
Ī›:Dimensionless parameter, Ī›=š¾š‘š/š¾
Ī›š‘”:Dimensionless parameter, Ī›š‘”=š¾š‘šš‘š2š‘/š‘šš‘”š¾2
šœŒ:Mass eccentricity of the rotor
šœ™:Rotational angle, šœ™=šœ”š‘”
šœ”:Rotational speed of the shaft
šœƒ:The angular position
šœ‡:Oil dynamic viscosity
šœ€:Eccentricity ratio, šœ€=š‘’/š‘
šœ”š‘›:Natural frequency, šœ”š‘›=āˆšš¾/š‘šš‘
šœ”š‘”:Dimensionless parameter, šœ”š‘”=šœ”š‘›/8
šœ”š‘:Dimensionless parameter, šœ”š‘=šœ”š‘›/4
šœ‘š‘–:Attitude angle of the rotor relative to the š‘‹-coordinate direction.


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