Application of Computational Fluid Dynamics Analysis for Rotating Machinery—Part II: Labyrinth Seal Analysis

Author:

Hirano Toshio1,Guo Zenglin1,Kirk R. Gordon1

Affiliation:

1. Mechanical Engineering Department, Rotor Dynamics Laboratory, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Abstract

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.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference13 articles.

1. Iwatsubo, T., 1980, “Evaluation of Instability Forces of Labyrinth Seals in Turbines or Compressors,” Proc. Rotordynamic Instability Problems in High Performance Turbomachinery, NASA CP-2133, Texas A&M University, pp. 139–167.

2. Scharrer, J. K., 1987, “Theory Versus Experiment for the Rotordynamic Coefficients of Labyrinth Gas Seals: Part I—A Two Control Volume Model,” Proc. ASME 11th Biennial Conference on Mechanical Vibration and Noise, Rotating Machinery Dynamics Volume Two, pp. 411–426.

3. Childs, D. W., and Scharrer, J. K., 1987, “Theory Versus Experiment for the Rotordynamic Coefficients of Labyrinth Gas Seals: Part II—A Comparison to Experiment,” Proc. ASME 11th Biennial Conference on Mechanical Vibration and Noise, Rotating Machinery Dynamics Volume Two, pp. 427–434.

4. Kirk, R. G. , 1988, “Evaluation of Aerodynamic Instability Mechanisms for Centrifugal Compressors—Part II: Advanced Analysis,” ASME J. Vib., Acoust., Stress, Reliab. Des., 110, No. 2, pp. 207–212.

5. Kirk, R. G. , 1990, “A Method for Calculating Labyrinth Seal Inlet Swirl Velocity,” ASME J. Vibr. Acoust., 112, No. 3, pp. 380–383.

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