Conventional labyrinth seal applications in turbomachinery encounter a permanent teeth tip damage and wear during transitional operations. This is the dominant issue that causes unpredictable seal leakage performance degradation. Since the gap between the rotor and the stator changes depending on engine transitional operations, labyrinth teeth located on the rotor/stator wear against the stator/rotor. This wear is observed mostly in the form of the labyrinth teeth becoming a mushroom shape. It is known that, as a result of this tooth tip wear, leakage performance permanently decreases, which negatively affects the engine's overall efficiency. However, very limited information about leakage performance degradation caused by mushroom wear is available in open literature. This paper presents a study that numerically quantifies leakage values for various radii of mushroom-shaped labyrinth teeth by changing tooth-surface clearance, pressure ratio, number of teeth, and rotor speed. Analyzed parameters and their ranges are mushroom radius (R = 0–0.508 mm), clearance (cr = 0.254–2.032 mm), pressure ratio (Rp = 1.5–3.5), number of teeth (nt = 1–12), and rotor speed (n = 0–80 krpm). Computational fluid dynamics (CFD) analyses were carried out by employing compressible turbulent flow in 2D axisymmetrical coordinate system. CFD leakage results were also compared with well-known labyrinth seal semi-empirical correlations. Given a constant clearance, leakage increases with the size of the mushroom radius that forms on the tooth. This behavior is caused by less flow separation and flow disturbance, and the vena contracta effect for flow over the smoothly shaped mushroom tooth tip compared to the sharp-edged tooth tip. This leakage increase is higher when the tooth tip wear is considered as an addition to the unworn physical clearance, since the clearance dominates the leakage. The leakage affected by the number of teeth was also quantified with respect to the mushroom radius. The rotational effect was also studied as a secondary parameter.

References

1.
Ludwig
,
L. P.
, and
Johnson
,
R. L.
,
1974
, “
Sealing Technology for Aircraft Gas Turbine Engines
,” NASA Lewis Research Center, Cleveland, OH,
NASA
Paper No. TM-X-71607.
2.
Chupp
,
R. E.
,
Hendricks
,
R. C.
,
Lattime
,
S. B.
, and
Steinetz
,
B. M.
,
2006
, “
Sealing in Turbomachinery
,” NASA Glenn Research Center, Cleveland, OH,
NASA
Paper No. TM 2006-214341.
3.
Eldin
,
A. M. G.
,
2007
, “
Leakage and Rotordynamic Effects of Pocket Damper Seals and See-Through Labyrinth Seal
,” Ph.D. thesis, Texas A&M University, College Station, TX.
4.
Suryanarayanan
,
S.
,
2009
, “
Labyrinth Seal Leakage Equation
,” M.Sc. thesis, Texas A&M University, College Station, TX.
5.
Waschka
,
W.
,
Wittig
,
S.
, and
Kim
,
S.
,
1992
, “
Influence of High Rotational Speeds on the Heat Transfer and Discharge Coefficients in Labyrinth Seals
,”
ASME J. Turbomach.
,
114
(
2
), pp.
462
468
.
6.
Willenborg
,
K.
,
Kim
,
S.
, and
Wittig
,
S.
,
2001
, “
Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal
,”
ASME J. Turbomach.
,
123
(
4
), pp.
815
822
.
7.
Suryanarayanan
,
S.
, and
Morrison
,
G. L.
,
2009
, “
Analysis of Flow Parameters Influencing Carry-Over Coefficient of Labyrinth Seals
,”
ASME
Paper No. GT2009-59245.
8.
Suryanarayanan
,
S.
, and
Morrison
,
G. L.
,
2009
, “
Effect of Tooth Height, Tooth Width and Shaft Diameter on Carry-Over Coefficient of Labyrinth Seals
,”
ASME
Paper No. GT2009-59246.
9.
Jun
,
L.
,
Xin
,
Y.
, and
Zhengping
,
F.
,
2006
, “
Effects of Pressure Ratio and Fin Pitch on Leakage Flow Characteristics in High Rotating Labyrinth Seals
,”
ASME
Paper No. GT2006-91145.
10.
Kurz
,
R.
, and
Brun
,
K.
,
2000
, “
Degradation in Gas Turbine Systems
,” International Gas Turbine and Aeroengine Congress & Exhibition, Munich, Germany, May 8–11,
ASME
Paper No. 2000-GT-345.
11.
Xu
,
J.
,
2006
, “
Effects of Operating Damage of Labyrinth Seal on Seal Leakage and Wheelspace Hot Gas Ingress
,” Ph.D. thesis, Texas A&M University, College Station, TX.
12.
Rhode
,
D. L.
, and
Adams
,
R. G.
,
2001
, “
Computed Effect of Rub-Groove Size on Stepped Labyrinth Seal Performance
,”
Tribol. Trans.
,
44
(
4
), pp.
523
532
.
13.
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
(
3
), pp.
604
611
.
14.
Rhode
,
D. L.
, and
Adams
,
R. G.
,
2004
, “
Rub-Groove Width and Depth Effects on Flow Predictions for Straight-Through Labyrinth Seals
,”
ASME J. Tribol.
,
126
(
4
), pp.
781
787
.
15.
Yan
,
X.
,
Lei
,
L.
,
Li
,
J.
, and
Feng
,
Z.
,
2014
, “
Effect of Bending and Mushrooming Damages on Heat Transfer Characteristic in Labyrinth Seals
,”
ASME J. Eng. Gas Turbines Power
,
136
(
4
), p.
041901
.
16.
ESDU 09004
,
2009
,
Labyrinth Seal Flow
,
The Institution of Mechanical Engineers
,
London
.
17.
Denecke
,
J.
,
Schramm
,
V.
,
Kim
,
V.
, and
Wittig
,
S.
,
2003
, “
Influence of Rub-Grooves on Labyrinth Seal Leakage
,”
ASME J. Turbomach.
,
125
(
2
), pp.
387
393
.
18.
Ghasripoor
,
F.
,
Turnquist
,
N. A.
, and
Kowalczyk
,
M.
,
2004
, “
Wear Prediction of Strip Seals Through Conductance
,”
ASME
Paper No. GT2004-53297.
19.
Neef
,
M.
,
Sulda
,
E.
,
Sürken
,
N.
, and
Walkenhorst
,
J.
,
2006
, “
Design Features and Performance Details of Brush Seals for Turbine Applications
,”
ASME
Paper No. GT2006-90404.
20.
Team CCJ, 2014, “
501F&G Users Benefit From Presentations by Non-OEM Equipment/Services Providers (1 of 2)
,” 501 F&G Users Group, Combined Cycle Journal, accessed Oct. 20,
2014
, http://www.ccj-online.com/501fg-users-benefit-from-presentations-by-non-oem-equipmentservices-providers-1-of-2/
21.
Yücel
,
U.
,
2004
, “
Calculation of Leakage and Dynamic Coefficients of Stepped Labyrinth Gas Seals
,”
Appl. Math. Comput.
,
152
(
2
), pp.
521
533
.
22.
Micio
,
M.
,
Facchini
,
B.
,
Innocenti
,
L.
, and
Simonetti
,
F.
,
2011
, “
Experimental Investigation on Leakage Loss and Heat Transfer in a Straight Through Labyrinth Seal
,”
ASME
Paper No. GT2011-46402.
23.
Wensheng
,
M.
,
Zhaobo
,
C.
, and
Yinghou
,
J.
,
2011
, “
Leakage and Whirl Speed Study in Labyrinth Seal Using CFD
,”
International Conference on Electronic & Mechanical Engineering and Information Technology
(
EMEIT
), Harbin, China, Aug. 12–14, pp. 592-595.
You do not currently have access to this content.