DocumentCode :
3543606
Title :
Comparative study of the performance on a constant flow annular hydrostatic thrust bearing having multi-circular recess and sector recess
Author :
Yu, Xiaodong ; Meng, Xiuli ; Shao, Junpeng ; Zhang, Yanqin ; Wu, Bo ; Shi, Zhimin
Author_Institution :
Harbin Univ. of Sci. & Technol. Harbin, Harbin, China
fYear :
2009
fDate :
16-19 Aug. 2009
Abstract :
A theoretical comparative study concerning performance of a constant flow hydrostatic thrust bearing having multi-circular recess and sector recess is described. The Computational Fluid Dynamics and the Finite Volume Method have been used to compute the characteristics of a constant fluid hydrostatic thrust bearing with circular and sector recesses. The performance has been compared, namely, recess pressure, pressure distribution and oil flow rate, on the basis of the same pocket area and the same pocket number. The results demonstrate that bearing recess shape has a great influence on the behavior of the hydrostatic thrust bearing. The computed results indicate that to get an improved performance from a constant flow hydrostatic thrust bearing, a proper selection of the geometric shape of the recess is essential.
Keywords :
computational fluid dynamics; finite volume methods; hydrostatics; machine bearings; rotational flow; annular hydrostatic thrust bearing; computational fluid dynamics; constant flow thrust bearing; finite volume method; multicircular recess; oil flow rate; pressure distribution; recess geometric shape; sector recess; Damping; Fluid flow measurement; Instruments; Machinery production industries; Optical films; Performance analysis; Shape; Temperature; Thermal conductivity; Viscosity; comparative study; constant flow; hydrostatic thrust bearing; recess shape;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-3863-1
Electronic_ISBN :
978-1-4244-3864-8
Type :
conf
DOI :
10.1109/ICEMI.2009.5274402
Filename :
5274402
Link To Document :
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