Rub-Groove Width and Depth Effects on Flow Predictions for Straight-Through Labyrinth Seals

Author:

Rhode David L.1,Adams Richard G.2

Affiliation:

1. Mechanical Engineering Department, Texas A&M University, College Station, TX 77843-3123

2. Texaco E & P, Inc., New Orleans, LA 70130

Abstract

A fully compressible, two-dimensional axisymmetric, turbulent Navier-Stokes code using the finite-volume discretization approach was utilized to obtain an enhanced understanding of the effects of rub-grooves in straight-through, abradable labyrinth seals. The high-Re form of the k-ε turbulence model was used. The code was first validated against measurements of straight-through honeycomb labyrinths, and accurate results were obtained. It was found that in most of the cases considered (tooth tip outside of its rub groove), the presence of rub-grooves increases the leakage, except for the case of the large pre-rub clearance and narrow rub-groove width. The presence of the large- or the intermediate-width rub-grooves allows the rub-groove depth to exert a fairly large effect on the leakage, especially for the smallest pre-rub radial clearance. Further, the presence of a narrow rub-groove with the smallest pre-rub radial clearance gives a dramatic effect on the streamwise (i.e., cavity-to-cavity) variation in overall flow patten.

Publisher

ASME International

Subject

Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials

Reference13 articles.

1. Zimmerman, H., Kammerer, A., and Wolff, K. H., 1994, “Performance of Worn Labyrinth Seals,” ASME 94-GT-131.

2. Stocker, H. L., Cox, D. M., and Holle, G. F., 1977, “Aerodynamic Performance of Conventional and Advanced Design Labyrinth Seals with Solid-Smooth, Abradable, and Honeycomb Lands,” Detroit Diesel Allison, Division of GMC, Indianapolis, IN, prepared for NASA, Contract NAS 3-20056.

3. Yu, Z., and Childs, D. W., 1995, “Experimental Rotordynamic Coefficient and Static Characteristic Results for a Labyrinth Rotor Running Against a Grooved Stator with L/D=0.466,Cr/r=0.0036,” Mechanical Engineering Department, Turbomachinery Laboratories, Texas A&M University.

4. Rhode, D. L., and Allen, B. F., 1998, “Visualization and Measurements of Rub-Groove Leakage Effects on Straight-Through Labyrinth Seals,” ASME Paper 98-GT-506, presented at the ASME International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm.

5. Rhode, D. L., and Allen, B. F., 2001, “Measurement and Visualization of Leakage Effects of Rounded Teeth Tips and Rub-Grooves on Stepped Labyrinths,” ASME J. Eng. Gas Turbines Power, 123, pp. 604–611.

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