In aerostatic bearing analysis, determining film pressure by solving the Reynolds equation in a numerical model is more effective than conducting bearing experiments or performing computational fluid dynamics (CFD) simulations. However, the discharge coefficient of an orifice-type restrictor is generally a given number that dominates model accuracy. This study investigated the influence of geometry and flow parameters on this discharge coefficient. The results indicate that this discharge coefficient is sensitive to the orifice diameter and film thickness and that the effects of the supply pressure, bearing radius, supply orifice length, supply passage diameter, conicity depth, and conicity angle can be disregarded. This study also built a surrogate model of this discharge coefficient based on the orifice diameter and film thickness by using artificial neural networks (ANNs).
Skip Nav Destination
Article navigation
January 2015
Research-Article
Discharge Coefficients in Aerostatic Bearings With Inherent Orifice-Type Restrictors
S. H. Chang,
S. H. Chang
1
Department of Mechanical Engineering,
Advanced Institute of Manufacturing With
High-Tech Innovations,
e-mail: shchang314@gmail.com
Advanced Institute of Manufacturing With
High-Tech Innovations,
National Chung Cheng University
,Ming-Hsiung, Chiayi County 621
, Taiwan
e-mail: shchang314@gmail.com
1Corresponding author.
Search for other works by this author on:
C. W. Chan,
C. W. Chan
Department of Mechanical Engineering,
Advanced Institute of Manufacturing With
High-Tech Innovations,
e-mail: addison0827@gmail.com
Advanced Institute of Manufacturing With
High-Tech Innovations,
National Chung Cheng University
,Ming-Hsiung, Chiayi County 621
, Taiwan
e-mail: addison0827@gmail.com
Search for other works by this author on:
Y. R. Jeng
Y. R. Jeng
Department of Mechanical Engineering,
Advanced Institute of Manufacturing With
High-Tech Innovations,
e-mail: imeyrj@ccu.edu.tw
Advanced Institute of Manufacturing With
High-Tech Innovations,
National Chung Cheng University
,Ming-Hsiung, Chiayi County 621
, Taiwan
e-mail: imeyrj@ccu.edu.tw
Search for other works by this author on:
S. H. Chang
Department of Mechanical Engineering,
Advanced Institute of Manufacturing With
High-Tech Innovations,
e-mail: shchang314@gmail.com
Advanced Institute of Manufacturing With
High-Tech Innovations,
National Chung Cheng University
,Ming-Hsiung, Chiayi County 621
, Taiwan
e-mail: shchang314@gmail.com
C. W. Chan
Department of Mechanical Engineering,
Advanced Institute of Manufacturing With
High-Tech Innovations,
e-mail: addison0827@gmail.com
Advanced Institute of Manufacturing With
High-Tech Innovations,
National Chung Cheng University
,Ming-Hsiung, Chiayi County 621
, Taiwan
e-mail: addison0827@gmail.com
Y. R. Jeng
Department of Mechanical Engineering,
Advanced Institute of Manufacturing With
High-Tech Innovations,
e-mail: imeyrj@ccu.edu.tw
Advanced Institute of Manufacturing With
High-Tech Innovations,
National Chung Cheng University
,Ming-Hsiung, Chiayi County 621
, Taiwan
e-mail: imeyrj@ccu.edu.tw
1Corresponding author.
Contributed by the Tribology Division of ASME for publication in the JOURNAL OF TRIBOLOGY. Manuscript received August 4, 2014; final manuscript received September 29, 2014; published online November 6, 2014. Assoc. Editor: George K. Nikas.
J. Tribol. Jan 2015, 137(1): 011705 (7 pages)
Published Online: November 6, 2014
Article history
Received:
August 4, 2014
Revision Received:
September 29, 2014
Citation
Chang, S. H., Chan, C. W., and Jeng, Y. R. (November 6, 2014). "Discharge Coefficients in Aerostatic Bearings With Inherent Orifice-Type Restrictors." ASME. J. Tribol. January 2015; 137(1): 011705. https://doi.org/10.1115/1.4028737
Download citation file:
Get Email Alerts
Related Articles
Tribological Study of a Slider Bearing in the Supersonic Regime
J. Tribol (October,2016)
Effects of Grooving in a Hydrostatic Circular Step Thrust Bearing With Porous Facing
J. Tribol (July,2015)
Design Optimization of Gas Foil Thrust Bearings for Maximum Load Capacity
J. Tribol (May,2017)
Surrogate Model Development for Air Foil Thrust Bearings With Chevron-Patterned Trailing Edge
J. Tribol (August,2024)
Related Proceedings Papers
Related Chapters
Antilock-Braking System Using Fuzzy Logic
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3
Hydrodynamic Lubrication
Design of Mechanical Bearings in Cardiac Assist Devices
Compressive Deformation of Hot-Applied Rubberized Asphalt Waterproofing
Roofing Research and Standards Development: 10th Volume