Influence of leakage flow through labyrinth seals on rotordynamics: numerical calculations and experimental measurements

An extensive investigation of the influence of the leakage flow through a labyrinth seal at supply pressure of 12 bar on the rotordynamics was performed by using numerical calculations and experimental measurements. Toward this end, an experimental rotor setup was established in Shanghai Jiao Tong University. Two labyrinth seals were chosen for comparison, e.g., an interlocking seal and a stepped one. The numerical calculations based on the bulk-flow theory and the perturbation analysis were accomplished. Simultaneous acquisitions of the fluctuating static pressure at the stator wall and the displacement of the whirling rotor were made. The influence of the aerodynamic forcing on the rotor was analyzed in terms of the axial distribution of the mean static pressure, the circumferential distribution of the fluctuating pressure, the fist critical speed and the destabilization rotating speed of the rotor. The experimental results demonstrated that the sinusoidal distribution of the fluctuating static pressure on the stator wall was closely related to the whirling motion of the rotor. The first critical speed of the rotor was reduced by the aerodynamic forcing, resulting in intensified destabilization of the rotor system. Furthermore, the numerical analyses were in good agreement to the experimental measurements.

[1]  Weizhe Wang,et al.  Computation of rotordynamic coefficients associated with leakage steam flow through labyrinth seal , 2007 .

[2]  Ugur Yücel Calculation of leakage and dynamic coefficients of stepped labyrinth gas seals , 2004, Appl. Math. Comput..

[3]  G. G. Hirs A Bulk-Flow Theory for Turbulence in Lubricant Films , 1973 .

[4]  Dara W. Childs,et al.  Theory Versus Experiment for the Rotordynamic Coefficients of Annular Gas Seals: Part 2—Constant-Clearance and Convergent-Tapered Geometry , 1986 .

[5]  C. Kim,et al.  Test Results for Rotordynamic Coefficients of Anti-Swirl Self-Injection Seals , 1994 .

[6]  R. Nordmann,et al.  Calculating Rotordynamic Coefficients of Seals by Finite-Difference Techniques , 1987 .

[7]  George T. Flowers,et al.  Comparison of the Dynamic Characteristics of Smooth Annular Seals and Damping Seals , 2001 .

[8]  D. Childs,et al.  Measurements Versus Predictions for the Dynamic Impedance of Annular Gas Seals—Part II: Smooth and Honeycomb Geometries , 2002 .

[9]  J. S. Alford,et al.  Protecting Turbomachinery From Self-Excited Rotor Whirl , 1965 .

[10]  J. Jeffrey Moore,et al.  Three-Dimensional CFD Rotordynamic Analysis of Gas Labyrinth Seals , 2003 .

[11]  Stephen Phillips,et al.  Measurements Versus Predictions for the Dynamic Impedance of Annular Gas Seals—Part I: Test Facility and Apparatus , 2002 .

[12]  Dursun Eser,et al.  Rotordynamic coefficients in stepped labyrinth seals , 2002 .

[13]  J. Y. Kazakia,et al.  Air flow in cavities of labyrinth seals , 1995 .

[14]  Dara W. Childs,et al.  Dynamic Analysis of Turbulent Annular Seals Based On Hirs’ Lubrication Equation , 1983 .

[15]  Dudley D. Fuller,et al.  Theory and Practice of Lubrication for Engineers , 1956 .

[16]  Dara W. Childs,et al.  Theory versus experiment for the rotordynamic coefficients of annular gas seals. Part 1: Test facility and apparatus , 1986 .

[17]  C. C. Nelson Analysis for leakage and rotordynamic coefficients of surface-roughened tapered annular gas seals , 1984 .

[18]  Dara W. Childs,et al.  Finite-Length Solutions for Rotordynamic Coefficients of Turbulent Annular Seals , 1983 .

[19]  Dara W. Childs,et al.  Experimental rotordynamic coefficient results for teeth-on-rotor and teeth-on-stator labyrinth gas seals , 1986 .

[20]  Dara W. Childs,et al.  An Iwatsubo-Based Solution for Labyrinth Seals: Comparison to Experimental Results , 1986 .