Abstract

Numerical studies are carried out to investigate pressure distributions of a fluid-lubricated herringbone-grooved journal bearing with trapezoidal grooves of various angles. Additionally, the optimal trapezoidal groove geometry is discussed in terms of the radial load capacity and friction torque.

1. Introduction

Recently, herringbone-grooved journal bearings have a lot of applications on small rotating mechanisms such as hard disk and turbo machinery. As for a herringbone-grooved gas journal bearing under a narrow groove theory, Vohr and Pan [1] obtained numerical solutions for a special case of small eccentricity. Cheng and Pan [2] gave time-dependent solution of a nonlinear Reynolds equation under stable operation parameters for gas-lubricated bearings. Hamrock and Fleming [3] investigated optimal conditions of radial load capacity for self-acting herringbone-grooved journal bearings. The film in an incompressible fluid was analyzed numerically by Murata et al. [4] based on the potential flow theory. Bonneau and Absi [5] applied a finite element method (FEM) to a compressible Reynolds equation to get aerodynamic characteristics at 4 through 16 grooves with moderate eccentricity. Rondonuwu and Winoto [6] measured pressure distributions along hydrodynamic herringbone-grooved journal bearing for several groove patterns.

A fluid-lubricated herringbone-grooved journal bearing with trapezoidal grooves was introduced by Liu and Mochimaru [7], and the influence of viscous trapezoidal grooves on the bearing was evaluated later for various trapezoidal angles [8].

In this paper, the pressure distributions generated along a self-acting fluid-lubricated herringbone-grooved journal bearing with trapezoidal grooves were numerically investigated, using a spectral finite difference scheme. In addition, the optimal trapezoidal groove geometry is discussed in terms of the radial load capacity and friction torque.

2. Analytical Model

Consider a fluid-lubricated journal bearing equipped with herringbone groove as shown in Figure 1. The bearing length is and the groove is symmetric with respect to its center of bearing. The shaft itself rotates around its center with an angular velocity in the counterclockwise direction and revolves around the center of the bearing with an angular velocity in the counterclockwise direction. The eccentricity of the shaft is given by , and the outer bearing is fixed.

The radius of bearing is , the radius of shaft ignoring grooves is , the bearing clearance is defined as , and the groove depth, the groove width, and ridge width, and the groove angle are denoted by , , , and , respectively. For a trapezoidal groove, the groove geometry is characterized by the angles and as shown in Figure 2, where and are the apparent trapezoidal angles of groove in cross-section.

Two coordinate systems, and , are introduced as follows.(1)An inertial coordinate system is fixed in the center of the outer bearing.(2)A noninertial coordinate system is fixed at the center of the rotation shaft.

 Hereafter the superscript is meant for the non-inertial coordinate system.

3. Pressure Distribution Equation and Spectral Finite Difference Method

The pressure distribution in fluid film, , can be obtained through a modified Reynolds equation with curvature effect derived by Liu and Mochimaru [7] as where the dimensionless lubricant film thickness, , is defined as . The dimensionless velocities, and , at the surface of the rotating shaft are given by

where

In the study, a spectral finite difference method is applied for solving the pressure distribution equation, the lubricated film thickness, , is expressed in a Fourier series to the circumferential -direction, and (1) is decomposed into each component of the Fourier series as shown in (4a)–(4d), so that (1) can be integrated with respect to time independently of each component to get a steady-state solution. This process results in high resolution in space and high speed in computation as follows:

At , the groove shape is symmetric, the boundary conditions of pressure are and it is assumed that the fluid is open to the atmosphere at , so that boundary conditions of pressure are

And in the numerical procedure, in order to accurately represent the geometry of lubricant film in the Fourier series, according to the sampling theorem [8], the Fourier series terms should take a half of the total number of geometry data in the circumferential direction as shown in Figure 3.

4. Load Capacity, Attitude Angle, and Friction Torque

The dimensionless radial component of load force, , tangential component of load , and friction torque of shaft, , are where and are the - and -components of fluid force per unit area on the surface of shaft, which can be obtained as referenced in Liu and Mochimaru [9].

Then the dimensionless load capacity, , is given by and the attitude angle, , is

5. Results and Discussion

In case of ,  deg, , , , , , , and , numerical results are shown in Figures 48.

Figure 4 displays an isobar diagram in the -plane with eccentricity changes, it shows that the pressure gradient in - and -direction is not zero even in the case of eccentricity equal to zero, which confirm the fact that the herringbone grooves have the pumping effect. And Figure 5 gives the pressure distribution with trapezoidal angle increases, as long as the trapezoidal angle is smaller than 30 deg, the high pressure zone is slightly increased with trapezoidal angle increase, but in cases that the groove angle is larger than 30 deg, the high pressure zone decreases and the lower pressure zone increases with an increase of trapezoidal angle.

There are three types of asymmetric trapezoidal grooves as shown in Figure 6. Figure 7(a) presents an isobar diagram in the -plane, and the circumferential pressure distribution at the center of the shaft (at ) is shown in Figure 7(b), where the dashed line is for the pressure distribution of the plane journal bearing case. In addition, the load capacity, attitude angle, and friction torque with trapezoidal angle changes are evaluated as shown in Figure 8, it shows that the lower pressure zone is the least area in the case of type 3, which is a favorable status to prevent cavitation, but in the case of type 1, the radial load capacity is maximum and the friction torque is minimum; it is useful for application on the miniaturization electronic device.

6. The Optimal Parameters of Trapezoidal Groove Geometry

Comparing with plane journal bearing, groove journal bearing has some distinguished advantages such as lower noise, higher stability but also has disadvantages such as small radial load capacity and larger friction torque. The optimal trapezoidal groove geometry can be estimated by the value, , which is given by the ratio of radial load capacity to friction torque as

The common parameters of groove geometry are given as , , , , , , , and . Figure 9 presents with respect to trapezoidal angle; in case of  deg, , and , it shows the optimal trapezoidal angle is 20 deg  deg.

In case of , and  deg, with the groove angle of values from 10 to 80 degrees are evaluated as a function of in Figure 10, which shows that when grooves angle is approximately 30 degree; has a maximum value.

Moreover, in case of  deg,  deg, the most suitable groove depth, , is 1.4 times of the bearing clearance for the maximum value as shown in Figure 11.

7. Conclusions

The pressure distributions generated along a fluid-lubricated herringbone-grooved journal bearing with trapezoidal groove are investigated at several cases of trapezoidal angles of groove. Regarding , which is given by the ratio of radial load capacity to friction torque, in the case of , , , , , , , and , the optimal parameters of trapezoidal grooves geometry are found as follows.(1)The trapezoidal angle is 20 deg  deg.(2)The groove depth is 1.4 times of the bearing clearance.(3)The grooves angle is approximately 30 degree.

Nomenclature

:Grooves width, ridge width
:Bearing clearance
:Eccentricity, dimensionless eccentricity
:Dimensionless -component of fluid force per unit area which acts on surface of shaft
:Dimensionless -component of fluid force per unit area which acts on surface of shaft
:Dimensionless radial component of load
:Dimensionless tangential component of load
:Dimensionless fluid film thickness
:Bearing length, dimensionless bearing length
:Number of grooves
:Dimensionless pressure
:Atmospheric pressure
:Inertial coordinates
:Radius of bearing
:Radius of shaft without grooves
:Radial component of coordinate at surface of shaft
:Dimensionless radial component of coordinate at surface of shaft
:Estimation value
:Time, dimensionless time
:Dimensionless friction torque of rotating shaft
:Dimensionless circumferential velocity at surface of rotating shaft
:Dimensionless radial velocity at surface of rotating shaft
:Dimensionless load capacity of bearing
:Groove angle
:Groove depth, dimensionless groove depth
:Viscosity of fluid
:Bearing number
:Dimensionless number
:Attitude angle of shaft
:Trapezoidal angle of groove
:Angle between the fixed axis of abscissa and the axis of eccentricity
:Dimensionless angle between the fixed axis of abscissa   and the axis of eccentricity
:Rotation velocity of shaft
:Swirl velocity of shaft
Superscript  :Noninertial coordinate.