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.

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
.
6.
Rhode
,
D. L.
, and
Adams
,
R. G.
,
2001
, “
Computed Effect of Rub-Groove Size on Stepped Labyrinth Seal Performance
,”
STLE Tribol. Trans.
,
44
(
4
), pp.
523
532
.
7.
Leonard
,
B. P.
,
1979
, “
A Stable and Accurate Convective Modeling Procedure Based on Quadratic Upstream Interpolation
,”
Comput. Methods Appl. Mech. Eng.
,
19
, pp.
59
98
.
8.
Rhode
,
D. L.
,
Demko
,
J. A.
,
Traegner
,
U. K.
,
Morrison
,
G. L.
, and
Sobolik
,
S. R.
,
1986
, “
Predictions of Incompressible Flow in Labyrinth Seals
,”
ASME J. Fluids Eng.
,
108
, pp.
19
25
.
9.
Rhode
,
D. L.
, and
Sobolik
,
S. R.
,
1986
, “
Simulation of Subsonic Flow Through a Generic Labyrinth Seal
,”
ASME J. Eng. Gas Turbines Power
,
108
, pp.
674
680
.
10.
Van Doormaal
,
J. P.
, and
Rathby
,
G. D.
,
1984
, “
Enhancements of the Simple Method for Predicting Incompressible Fluid Flows
,”
Numer. Heat Transfer
,
7
, pp.
147
163
.
11.
Launder, B. E., and Spalding, D. B., 1972, Mathematical Models of Turbulence, Academic Press, London.
12.
Egli
,
A.
,
1935
, “
The leakage of Steam Through Labyrinth Seals
,”
Trans. ASME
,
57
, pp.
115
122
.
13.
Moody
,
L. F.
,
1944
Friction Factors for Pipe Flow
,”
Trans. ASME
,
66
(
8
), pp.
671
684
.
You do not currently have access to this content.