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.
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October 2005
Technical Papers
Application of Computational Fluid Dynamics Analysis for Rotating Machinery—Part II: Labyrinth Seal Analysis
Toshio Hirano,
Toshio Hirano
Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
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Zenglin Guo,
Zenglin Guo
Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
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R. Gordon Kirk
R. Gordon Kirk
Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
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Toshio Hirano
Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Zenglin Guo
Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
R. Gordon Kirk
Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Contributed by the International Gas Turbine Institute (IGTI) of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS for publication in the ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Paper presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Atlanta, GA, June 16–19, 2003, Paper No. 2003-GT-38984. Manuscript received by IGTI, October 2002, final revision, March 2003. Associate Editor: H. R. Simmons.
J. Eng. Gas Turbines Power. Oct 2005, 127(4): 820-826 (7 pages)
Published Online: September 20, 2005
Article history
Received:
October 1, 2002
Revised:
March 1, 2003
Online:
September 20, 2005
Citation
Hirano , T., Guo , Z., and Kirk, R. G. (September 20, 2005). "Application of Computational Fluid Dynamics Analysis for Rotating Machinery—Part II: Labyrinth Seal Analysis ." ASME. J. Eng. Gas Turbines Power. October 2005; 127(4): 820–826. https://doi.org/10.1115/1.1808426
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