Thrust bearing design for high-speed composite air spindles

被引:9
作者
Bang, KG [1 ]
Lee, DG [1 ]
机构
[1] Korea Adv Inst Sci & Technol, Dept Mech Engn, Yusong Gu, Taejon 305701, South Korea
关键词
thrust bearing; high-speed composite air spindle; centrifugal force; nonlinear air spring; fatigue life; load capability; natural frequency;
D O I
10.1016/S0263-8223(02)00067-3
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The air spindles whose shafts are made of carbon fiber composite are appropriate for high-speed and high-precision machining such as small hole drilling of printed circuit board (PCB) or wafer cutting for manufacturing semiconductors because the carbon fiber composite shaft has low rotational inertia, high damping ratio and high fundamental natural frequency. The axial load capability and stiffness of air spindles for drilling operation are dependent on thrust bearings that are composed of air supply part mounted on the housing and rotating part mounted on the rotating shaft of spindle,. Since the stresses induced in the rotating part of thrust bearing by centrifugal force are very high at high-speed rotation, the axial stiffness and load capability of an air spindle should be designed considering the stresses induced by the centrifugal force as well as the natural frequency of rotating shaft to avoid the resonant whip vibration of the spindle. In this work, the air Supply part of a thrust air bearing for a high-speed composite air spindle was designed considering its axial stiffness and load capability. The rotating part of the thin thrust bearing was designed through finite element analysis considering the static and dynamic characteristics under axial load and the centrifugal force during high-speed rotation. (C) 2002 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:149 / 160
页数:12
相关论文
共 16 条
[1]   DISTORTION ANALYSIS OF LARGE THRUST BEARING ON ELASTIC SUPPORT [J].
ASHOUR, NMAE ;
ATHRE, K ;
NATH, Y ;
BISWAS, S .
WEAR, 1991, 147 (02) :421-430
[2]   Design of carbon fiber composite shafts for high speed air spindles [J].
Bang, KG ;
Lee, DG .
COMPOSITE STRUCTURES, 2002, 55 (02) :247-259
[3]  
Beek A. V., 1996, WEAR, V201, P45, DOI [10.1016/S0043-1648(96)06987-6, DOI 10.1016/S0043-1648(96)06987-6]
[4]   EXPERIMENTAL INVESTIGATION INTO THE PERFORMANCE OF AN AEROSTATIC INDUSTRIAL THRUST BEARING [J].
BOFFEY, DA ;
BARROW, AA ;
DEARDEN, JK .
TRIBOLOGY INTERNATIONAL, 1985, 18 (03) :165-168
[5]  
CUI C, 1994, T JPN SOC MECH ENG-C, V60, P1775
[6]   Comparison between externally pressurized gas thrust bearings with different orifice and porous feeding systems [J].
Fourka, M ;
Bonis, M .
WEAR, 1997, 210 (1-2) :311-317
[7]  
HENRY SD, 1995, FATIGUE DATA BOOK LI, P71
[8]   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
[9]   Analysis of an aerodynamic compliant foil thrust bearing: Method for a rapid design [J].
Iordanoff, I .
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 1999, 121 (04) :816-822
[10]   A tolerancing procedure for inherently compensated, rectangular aerostatic thrust bearings [J].
Kwan, YBP ;
Post, JB .
TRIBOLOGY INTERNATIONAL, 2000, 33 (08) :581-585