A New Structural Stiffness Model for Bump-Type Foil Bearings: Application to Generation II Gas Lubricated Foil Thrust Bearing

被引:52
作者
Gad, Abdelrasoul M. [1 ,2 ]
Kaneko, Shigehiko [1 ]
机构
[1] Univ Tokyo, Sch Engn, Dept Mech Engn, Bunkyo Ku, Tokyo 1138656, Japan
[2] Assiut Univ, Dept Mech Engn, Assiut 71516, Egypt
来源
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME | 2014年 / 136卷 / 04期
基金
日本学术振兴会;
关键词
structural stiffness model; generation II foil thrust bearings; elastohydrodynamic lubrication; COULOMB-FRICTION; FINITE-ELEMENT;
D O I
10.1115/1.4027601
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A new structural stiffness model for the compliant structure in foil gas bearings is introduced in the first part of this work. The model investigates the possibility that the flat segment between bumps, in bump foil strip, may deflect laterally and separate from the rigid bearing surface, and it also considers the interaction between bumps in the bump foil strip, the friction between the bump foil, and the surrounding structure. The validity of the analytical solution was verified through direct comparison with previous numerical and analytical models. In the second part of this work, the introduced bump foil model is used to investigate the static characteristics of generation II gas foil thrust bearing. The numerical simulations of the coupled fluid-structure interactions revealed that the foil thrust bearings share many features with their rigid bearing counterpart and the results showed clearly that the load carrying capacity of foil thrust bearings increases nonlinearly with the rotation speed and is expected to reach an asymptote as the rotation speed exceeds a certain value. The effects of ramp height and interface friction (i.e., friction at bump foil/rigid bearing interface and bump foil/top foil interface) on the static characteristics of generation II foil thrust bearings are investigated.
引用
收藏
页数:13
相关论文
共 28 条
[1]  
Beer F. P., 2008, MECH MAT
[2]  
Bores A. P., 2003, ADV MECH MAT
[3]  
Bruckner R.J., 2004, Ph.D. Thesis
[4]  
Bruckner R. J., 2011, SUPERCRIT CO2 POWER
[5]  
DellaCorte C., 2010, NASATM2010216762
[6]  
Dickman J.R., 2010, Masters Thesis
[7]  
Dykas B., 2006, Ph.D. Thesis
[8]   Analytical Model of Bump-Type Foil Bearings Using a Link-Spring Structure and a Finite-Element Shell Model [J].
Feng, Kai ;
Kaneko, Shigehiko .
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 2010, 132 (02) :1-11
[9]  
Hamrock B.J., 1994, FUNDAMENTALS FLUID F
[10]   Analysis of gas lubricated foil thrust bearings using coupled finite element and finite difference methods [J].
Heshmat, CA ;
Xu, DS ;
Heshmat, H .
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 2000, 122 (01) :199-204