Effects of partition wall type, partition wall number and cavity depth on the leakage and rotordynamic characteristics of the pocket damper seal (PDS) were numerically investigated using a presented 3D transient computational fluid dynamics (CFD) method based on the multifrequency elliptical whirling orbit model. The accuracy and availability of this transient CFD method and the multifrequency elliptical whirling orbit model were demonstrated with the experimental data of the experimental eight-bladed fully partitioned pocket damper seal (FPDS). The leakage flow rates and frequency-dependent rotordynamic coefficients of PDS were computed for two types of partition wall (namely conventional PDS and fully partitioned PDS), four partition wall numbers including the labyrinth seal (no partition wall) and six cavity depths including the plain smooth seal (zero cavity depth) at operational conditions with or without inlet preswirl and 15,000 rpm rotational speed. The numerical results show that the FPDS has the similar leakage performance and more superior stability capacity than the conventional PDS. The FPDS possesses slightly larger leakage flow rate (∼2.6–4.0% larger) compared to the labyrinth seal. Eight is a preferable value for the partition wall number to gain the best leakage performance of the FPDS with the least manufacturing cost. The FPDS possesses significantly larger stiffness and damping than the labyrinth seal. Increasing partition wall number results in a significant increase in the direct stiffness but limited desirable effect on the effective damping. The FPDS possesses the lowest leakage flow rate when the cavity depth is about 2.0 mm. Compared to the plain smooth seal, the FPDS possesses larger positive direct stiffness and significantly less direct damping and effective damping. Increasing cavity depth results in a significant decrease in the stabilizing direct damping and the magnitude of the destabilizing cross-coupling stiffness. H= 3.175 mm is a preferable value of the cavity depth for which the effective damping of the FPDS is largest, especially for the concerned frequencies (80–120 Hz) where most multistage high-pressure centrifugal compressors have stability problem.

References

1.
Lakshminarayana
,
B.
,
1996
,
Fluid Dynamics and Heat Transfer of Turbomachinery
,
Wiley
,
New York
, pp.
339
347
.
2.
Chupp
,
R. E.
,
Hendricks
,
R. C.
,
Lattime
,
S. B.
, and
Steinetz
,
B. M.
,
2006
, “
Sealing in Turbomachinery
,”
J. Propul. Power
,
22
(
2
), pp.
313
349
.10.2514/1.17778
3.
Muszynska
,
A.
,
2005
,
Rotordynamics
,
CRC Press, Taylor & Francis Group
,
Boca Raton, FL
, pp.
214
222
.
4.
Vance
,
J. M.
,
2010
,
Machinery Vibration and Rotordynamics
,
Wiley
,
New York
, pp.
271
278
.
5.
Zeidan
,
F.
,
Perez
,
R.
, and
Stephenson
,
E.
,
1993
, “
The Use of Honeycomb Seals in Stabilizing Two Centrifugal Compressors
,”
22nd Turbomachinery Symposium, Turbomachinery Laboratory
, Texas A&M University, College Station, TX, Sept. 14–16, pp.
3
15
.
6.
Richards
,
R. L.
,
Vance
,
J. M.
, and
Zeidan
,
F. Y.
,
1995
, “
Using a Damper Seal to Eliminate Subsynchronous Vibrations in Three Back-to-Back Compressors
,”
24th Turbomachinery Symposium, Turbomachinery Laboratory
, Texas A&M University, College Station, TX, Sept. 26–28, pp.
370
376
.
7.
Vance
,
J.
, and
Schultz
,
R.
,
1993
, “
A New Damper Seal for Turbomachinery
,” 14th Biennial ASME Conference on Vibration and Noise, Albuquerque, NM, Sept. 19–22, pp.139–148.
8.
Shultz
,
R.
,
1996
, “
Analytical and Experimental Investigations of a Labyrinth Seal Test Rig and Damper Seals for Turbomachinery
,” M.S. thesis, Mechanical Engineering Department, Texas A&M University, College Station, TX.
9.
Li
,
J.
, and
Vance
,
J. M.
,
1995
, “
Effects of Clearance and Clearance Ratio on Two and Three Bladed TAMSEALS
,” Turbomachinery Laboratory Research Progress Report, Texas A&M University, College Station, TX, Report No. TRC-Seal-4-95.
10.
Ertas
,
B. H.
,
Gamal
,
A. M.
, and
Vance
,
J. M.
,
2006
, “
Rotordynamic Force Coefficients of Pocket Damper Seals
,”
ASME J. Turbomach.
,
128
(
4
), pp.
725
737
.10.1115/1.2221327
11.
Li
,
J.
,
Kushner
,
F.
, and
Choudhury
,
P. D.
,
2002
, “
Experimental Evaluation of Slotted Pocket Gas Damper Seals on a Rotating Test Rig
,”
ASME
Paper No. GT2002-30634.10.1115/GT2002-30634
12.
Ertas
,
B. H.
, and
Vance
,
J. M.
,
2007
, “
Rotordynamic Force Coefficients for a New Pocket Damper Seals
,”
ASME J. Tribol.
,
129
(
2
), pp.
365
374
.10.1115/1.2464138
13.
Ertas
,
B. H.
,
Delgado
,
A.
, and
Vannini
,
G.
,
2012
Rotordynamic Force Coefficients for Three Types of Annular Gas Seals With Inlet Preswirl and High Differentail Pressure Ratio
,”
ASME J. Eng. Gas Turbines Power
,
134
(
4
), p.
042503
.10.1115/1.4004537
14.
Li
,
J.
,
San Andrés
,
L.
, and
Vance
,
J. M.
,
1999
, “
A Bulk-Flow Analysis of Multiple-Pocket Gas Damper Seals
,”
ASME J. Eng. Gas Turibines Power
,
121
(
2
), pp.
355
362
.10.1115/1.2817128
15.
Armendariz
,
R. A.
,
2002
, “
Rotordynamic Analysis of A Pocket Damper Seal Using Circular Orbits of Large Amplitude
,” Ph.D. thesis, Mechanical Engineering Department, Texas A&M University, College Station, TX.
16.
Gamal
,
A. M.
,
2003
, “
Analytical and Experimental Evaluation of the Leakage and Stiffness Characteristics of High Pressure Pocket Damper Seals
,” M.S. thesis, Mechanical Engineering Department, Texas A&M University, College Station, TX.
17.
Gamal
,
A. M.
,
2007
, “
Leakage and Rotordynamic Effects of Pocket Damper Seals and See-Through Labyrinth Seals
,” Ph.D. thesis, Mechanical Engineering Department, Texas A&M University, College Station, TX.
18.
Jun
,
L.
,
Zhigang
,
L.
, and
Zhenping
,
F.
,
2012
Investigations on the Rotordynamic Coefficients of Pocket Damper Seals Using the Multi-Frequency, One-Dimensional, Whirling Orbit Model and RANS Solutions
,”
ASME J. Eng. Gas Turbines Power
,
134
(
10
), p.
102510
.10.1115/1.4007063
19.
Zhigang
,
L.
,
Jun
,
L.
, and
Xin
,
Y.
,
2013
, “
Multiple Frequencies Elliptical Whirling Orbit Model and Transient RANS Solution Approach to Rotordynamic Coefficients of Annual Gas Seals Prediction
,”
ASME J. Vib. Acoust.
,
135
(
3
), p.
031005
.10.1115/1.4023143
20.
AEA Technology GmbH
,
2004
, “
CFX-TASCflow User Documentation
,”
AEA Technology, Software Ltd.
,
Waterloo, ON, Canada
.
21.
Childs
,
D. W.
,
1993
,
Turbomachinery Rotordynamics: Phenomena, Modeling and Analysis
,
Wiley
,
New York
, p.
292
.
You do not currently have access to this content.