A main goal of noncontacting mechanical seals is to provide minimal leakage during operation. This may be achieved by specifying a small clearance between the mating faces that is just enough to avoid rubbing contact while allowing some tolerable leakage. The amount of leakage flow is reduced through the acceleration and deceleration of the fluid through a tortuous path, so the sealing performance depends on the geometric characteristics of the leakage path. This study focuses on annular hole-pattern seals, which are noncontacting mechanical seals commonly used in high pressure compressors. A design of experiments (DOE) approach is used to investigate the effects of various geometric variables on the leakage rate of a hole-pattern seal during normal operating conditions. The design space, defined by the ranges of hole diameter, hole depth, axial space between holes and number of holes in circumferential direction, is discretized using the simple random sampling method. Then, steady-state computational fluid dynamics (CFD) simulations are performed at each design point to evaluate seal performance. To better understand the sensitivity of the hole-pattern seal leakage rate with respect to design variables selected, response surfaces are built through its values at design points using quadratic polynomial fitting. The results show that the optimal solution had a better leakage control ability over the base model design. It is believed that the results of this study will assist in improving the design of annular hole-pattern seals.

References

1.
Von Pageneau
,
G. L.
,
1982
, “
Damping Seals for Turbomachinery
,” NASA Technical Paper No. 1987.
2.
Childs
,
D. W.
, and
Moyer
,
D.
,
1985
, “
Vibration Characteristics of the HPOTP (High-Pressure Oxygen Turbopump) of the SSME (Space Shuttle Main Engine)
,”
ASME J. Eng. Gas Turb. Power
,
107
(1), pp.
152
159
.10.1115/1.3239676
3.
Yu
,
Z.
, and
Childs
,
D. W.
,
1998
, “
A Comparison of Experimental Rotordynamic Coefficients and Leakage Characteristics Between Hole-Pattern Gas Damper Seals and Honeycomb Seal
,”
ASME J. Eng. Gas Turb. Power
,
120
(
10
), pp.
778
783
.10.1115/1.2818467
4.
Childs
,
D. W.
, and
Fayolle
,
P.
,
1999
, “
Test Results for Liquid Damper Seals Using a Round-Hole Roughness Pattern for the Stators
,”
ASME J. Tribol.
,
121
(
1
), pp.
42
49
.10.1115/1.2833809
5.
Nielson
,
K. K.
,
Jonck
,
K.
, and
Underbakke
,
H.
,
2012
, “
Hole-Pattern and Honeycomb Seal Rotordynamic Forces: Validation of CFD-Based Prediction Techniques
,”
ASME J. Eng. Gas Turb. Power
,
134
(
12
), p.
122505
.10.1115/1.4007344
6.
Vannarsdall
,
M.
, and
Childs
,
D. W.
,
2014
, “
Static and Rotordynamic Characteristics for a New Hole-Pattern Annular Gas Seal Design Incorporating Larger Diameter Holes
,”
ASME J. Eng. Gas Turb. Power
,
136
(
2
), p.
022507
.10.1115/1.4025536
7.
Childs
,
D. W.
, and
Wade
,
J.
,
2004
, “
Rotordynamic-Coefficient and Leakage Characteristics for Hole-Pattern-Stator Annular Gas Seals—Measurements Versus Predictions
,”
ASME J. Tribol.
,
126
(
2
), pp.
326
333
.10.1115/1.1611502
8.
Untaroiu
,
A.
,
Migliorini
,
P. J.
,
Wood
,
H. G.
,
Allaire
,
P. E.
, and
Kocur
,
J. A.
,
2009
, “
Hole-Pattern Seals: A Three Dimensional CFD Approach for Computing Rotordynamic Coefficient and Leakage Characteristics
,”
ASME
Paper No. IMECE2009-11558.10.1115/IMECE2009-11558
9.
Yan
,
X.
,
Li
,
J.
, and
Feng
,
Z.
,
2011
, “
Investigations on the Rotordynamic Characteristics of a Hole-Pattern Seal Using Transient CFD and Periodic Circular Orbit Model
,”
ASME J. Vib. Acoust.
,
133
(
4
), p.
041007
.10.1115/1.4003403
10.
Migliorini
,
P. J.
,
Untaroiu
,
A.
,
Wood
,
H. G.
, and
Allaire
,
P. E.
,
2012
, “
A Computational Fluid Dynamics/Bulk-Flow Hybrid Method for Determining Rotordynamic Coefficients of Annular Gas Seals
,”
ASME J. Tribol.
,
134
(2), p.
022202
.10.1115/1.4006407
11.
Gentle
,
J.
,
2003
,
Random Number Generation and Monte Carlo Methods
,
Springer
,
Berlin
.
12.
Petelet
,
M.
,
Iooss
,
B.
,
Asserin
,
O.
, and
Loredo
,
A.
,
2010
, “
Latin Hypercube Sampling With Inequality Constraints
”,
AStA Adv. Stat. Anal.
,
94
(
4
), pp.
325
339
.10.1007/s10182-010-0144-z
13.
Pirie
,
W.
2004
, “
Spearman Rank Correlation Coefficient
,”
Encyclopedia of Statistical Sciences
. 10.1002/0471667196.ess2499
14.
Untaroiu
,
A.
,
Hayrapetian
, V
.
,
Untaroiu
,
C. D.
,
Wood
,
H. G.
,
Schiavello
,
B.
,
McGuire
,
J.
,
2013
, “
On the Dynamic Properties of Pump Liquid Seals
,”
ASME J. Fluids Eng.
,
135
(
5
), p.
051104
.10.1115/1.4023653
15.
Untaroiu
,
A.
,
Untaroiu
,
C. D.
,
Wood
,
H. G.
, and
Allaire
,
P. E.
,
2013
, “
Numerical Modeling of Fluid-Induced Rotordynamic Forces in Seals With Large Aspect Ratios
,”
ASME J. Eng. Gas Turb. Power
,
135
(
1
), p.
012501
.10.1115/1.4007341
16.
Untaroiu
,
A.
,
Wood
,
H. G.
,
Dimond
,
T.
, and
Allaire
,
P. E.
,
2008
, “
Calculation of Dynamic Coefficients for a Magnetically Levitated Artificial Heart Pump Using a CFD Approach
,”
ASME
Paper No. IMECE2008-67802. 10.1115/IMECE2008-67802
17.
Untaroiu
,
C. D.
, and
Untaroiu
,
A.
,
2010
, “
Constrained Design Optimization of Rotor-Tilting Pad Bearings Systems
,”
ASME J Eng. Gas Turb. Power
,
132
(
12
), p.
122502
.10.1115/1.4001811
You do not currently have access to this content.