Related Experiment Video
Updated: Jul 17, 2026

Uncoupling Coriolis Force and Rotating Buoyancy Effects on Full-Field Heat Transfer Properties of a Rotating Channel
Published on: October 5, 2018
Numerical investigation of a three-lobe gas foil bearing with a double-ring microgrooved top foil based on
Yiheng Zhang1, Peigang Jiao2, Changhui Zheng1
1Shandong Key Laboratory of Technologies and Systems for Intelligent Construction Equipment, Shandong Jiaotong University, Jinan, 250357, China.
Abstract:
Foil gas bearings are critical supporting components in high-speed oil-free rotating machinery. However, their limited hydrodynamic load-carrying capacity remains a fundamental challenge. To enhance the gas film pressure distribution and load-carrying performance of three-lobe aerodynamic foil bearings, a double-ring circumferential microgroove structure is proposed on the inner surface of the top foil. Based on compressible gas lubrication theory and the fluid-structure interaction method, a numerical model is established to compare grooveless, single-ring microgroove, and double-ring microgroove bearings with different groove spacings under the condition of constant total grooved area. The effects of groove spacing are investigated under rotational speeds of 30000[Formula: see text]70000[Formula: see text] and eccentricity ratios of 0.4[Formula: see text]0.8. The results show that, under different rotational speeds, the grooved structures increase the maximum gas film pressure to approximately 1.04[Formula: see text]1.14 times that of the grooveless bearing, while the load-carrying capacity increases to approximately 1.06[Formula: see text]1.13 times. Under different eccentricity ratios, the maximum gas film pressure increases to approximately 1.02[Formula: see text]1.16 times the original value, and the bearing capacity increases to approximately 1.09[Formula: see text]1.17 times the original value. When the groove spacing of the double-ring microgroove is 4 [Formula: see text], the distribution of the axial high-pressure zone is more continuous, the pressure integration effect is better, and the bearing achieves the optimal load-bearing performance, Compared with the single-ring microgroove structure, this structure reduces the maximum deformation of the ripple foil by 4.7%. The findings demonstrate that a properly designed double-ring microgroove configuration can reshape the axial pressure distribution and increase the effective bearing area, which contributes to improved load-carrying capacity.
Related Concept Videos
Steady, Laminar Flow Between Parallel Plates
Design Example: Deciding Thickness of Lubricating Fluid in a Shaft
To calculate the required thickness of the lubricant layer, the tangential velocity at the shaft's surface must first be determined. This velocity is calculated by converting the rotational speed to angular velocity...
Steady, Laminar Flow in Circular Tubes
Fluid Pressure over Curved Plate of Constant Width
Fluid Pressure over Flat Plate of Constant Width
The resultant force...
Fluid Pressure over Flat Plate of Variable Width
The pressure distribution on the plate can be calculated by determining the force that acts on a differential area strip of the plate. Thus, the magnitude of the force is equal to the...

