Application of computational fluid dynamics analysis for rotating machinery - Part II: Labyrinth seal analysis

被引:105
作者
Hirano, T [1 ]
Guo, ZL [1 ]
Kirk, RG [1 ]
机构
[1] Virginia Polytech Inst & State Univ, Dept Mech Engn, Rotor Dynam Lab, Blacksburg, VA 24061 USA
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2005年 / 127卷 / 04期
关键词
D O I
10.1115/1.1808426
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Labyrinth seals are used in various kinds of turbo machines to reduce internal leakage flow. The working fluid, or the gas passing through the rotor shaft labyrinth seals, often generates driving force components that may increase the unstable vibration of the rotor. It is important to know the accurate rotordynamic force components for predicting the instability of the rotor-bearing-seal system. The major goals of this research were to calculate the rotordynamic force of a labyrinth seals utilizing a commercial CFD program and to further compare those results to an existing bulk flow computer program currently used by major US machinery manufacturers. The labyrinth seals of a steam turbine and a compressor eye seal are taken as objects of analysis. For each case, a 3D model with eccentric rotor was solved to obtain the rotordynamic force components. The leakage flow and rotor dynamics force predicted by CFX TASCFlow are compared with the results of the existing bulk flow analysis program DYNLAB. The results show that the bulk flow program gives a pessimistic prediction of the destabilizing forces for the conditions under investigation. Further research work will be required to fully understand the complex leakage flows in turbo machinery.
引用
收藏
页码:820 / 826
页数:7
相关论文
共 13 条
[1]  
*AEA TECHN, 2001, CFX TASCFLOW 2 11 1
[2]  
[Anonymous], SHOCK VIB DIG
[3]  
CHILDS DW, 1987, P ASME 11 BIENN C ME, P427
[4]  
GUO Z, 2003, ASME, V127, P445
[5]   Prediction of rotordynamic forces in a labyrinth seal based on three-dimensional turbulent flow computation [J].
Ishii, E ;
Kato, C ;
Kikuchi, K ;
Ueyama, Y .
JSME INTERNATIONAL JOURNAL SERIES C-MECHANICAL SYSTEMS MACHINE ELEMENTS AND MANUFACTURING, 1997, 40 (04) :743-748
[6]  
Iwatsubo T., 1980, P NASA LEWIS RES CTR, P139
[7]  
KIRK RG, 1990, ASME, V112, P380
[8]  
KRIK RG, 1988, ASME, V110, P207
[9]  
Kwanka K., 2000, ASME INT GAS TURB AE
[10]  
Moore J. J, 2001, P DETC 01