Selected test results are presented for an annular gas seal using a smooth rotor and a hole-pattern-roughness stator for a supply pressure of 70 bar, three pressure ratios, three speeds up to 20,000 rpm, two clearances, and three preswirl ratios. Dynamic data include frequency-dependent direct and cross-coupled stiffness and damping coefficients. Static data include leakage and upstream and downstream pressures and temperatures. Very good agreements are found between measurements and predictions from a two-control-volume bulk-flow model.
Issue Section:
Technical Papers
1.
Childs
, D.
, and Moyer
, D.
, 1985
, “Vibration Characteristics of the HPOTP (High Pressure Oxygen Turbopump) of the SSME (Space Shuttle Main Engine)
,” ASME J. Eng. Gas Turbines Power
, 107
, pp. 152
–159
.2.
Yu
, Z.
, and Childs
, D. W.
, 1998
, “A Comparison of Experimental Rotordynamic Coefficients and Leakage Characteristics Between Hole-Pattern Gas Damper Seals and a Honeycomb Seal
,” ASME J. Eng. Gas Turbines Power
, 120
(4
), pp. 778
–783
.3.
Moore, J., Walker, S., and Kuzdal, M., 2002, “Rotordynamic Stability Measurements During Full Load Testing of a 6000 psi Reinjection Centrifugal Compressor,” Proceedings, 31st Texas A&M University Turbomachinery Symposium, pp. 29–38.
4.
Gelin, A., Pugnet, J.-M., Bolusset, D., and Friez, P., 1996, “Experience in Full Load Testing Natural Gas Compressors for Rotordynamic Improvements,” International Gas Turbine Conference, ASME Paper No. 96-GT-378.
5.
Memmott, E., 1994, “Stability of a High Pressure Centrifugal Compressor Through Application of Shunt Holes and a Honeycomb Labyrinth,” 13th Machinery Dynamics Seminar, CMVA, September, 12–13.
6.
Scharrer, J., 1989, written discussion of reference (7), ASME J. of Tribology, p. 301.
7.
Childs
, D.
, Elrod
, D.
, and Hale
, K.
, 1989
, “Annular Honeycomb Seals: Test Results for Leakage and Rotordynamic Coefficients; Comparisons to Labyrinth and Smooth Configurations
,” ASME J. Tribol.
, 111
, pp. 293
–301
.8.
Childs, D., and Kleynhans, G., 1992, “Experimental Rotordynamic and Leakage Results for Short (L/D=1/6) Honeycomb and Smooth Annular Pressure Seals,” IMechE Proceedings, Fifth International Conference on Vibrations in Rotating Machinery, September 7–10, Bath, England.
9.
Holt
, C.
, and Childs
, D.
, 2002
, “Theory Versus Experiment Results for the Dynamic Impedances of Two Hole-Pattern Annular Gas Seals
,” ASME J. Tribol.
, 24
, pp. 137
–143
.10.
Kleynhans
, G.
, and Childs
, D.
, 1997
, “The Acoustic Influence of Cell Depth on the Rotordynamic Characteristics of Smooth-Rotor/Honeycomb-Stator Annular Gas Seals
,” ASME J. Eng. Gas Turbines Power
, 4
, pp. 949
–957
.11.
Dawson
, M.
, Childs
, D.
, Holt
, C.
, and Phillips
, S.
, 2002
, “Theory Versus Experiments for the Dynamic Impedances of Annular Gas Seals: Part2—Smooth and Honeycomb Seals
,” ASME J. Eng. Gas Turbines Power
, 24
, pp. 963
–970
.12.
Childs
, D.
, and Hale
, K.
, 1994
, “A Test Apparatus and Facility to Identify the Rotordynamic Coefficients of High-Speed Hydrostatic Bearings
,” ASME J. Tribol.
, 116
, pp. 337
–334
.13.
Dawson
, M.
, Childs
, D.
, Holt
, C.
, and Phillips
, S.
, 2002
, “Theory Versus Experiments for the Dynamic Impedances of Annular Gas Seals: Part 1—Test Facility and Apparatus
,” ASME J. Eng. Gas Turbines Power
, 24
, pp. 958
–963
.14.
Weatherwax, M., and Childs, D. 2002, “The Influence of Eccentricity on the Leakage and Rotordynamic Coefficients of a High-Pressure Honeycomb Annular Gas Seal, Measurements Versus Predictions,” ASME Paper 2002-TRIB-207.
15.
Marquette
, O.
, Childs
, D.
, and San Andres
, L.
, 1997
, “Eccentricity Effects on the Rotordynamic Coefficients of Plain Annular Seals: Theory Versus Experiment
,” Transactions of the ASME J. Tribology
, 119
, pp. 443
–448
.16.
Picardo, A., 2003, “High Pressure Testing of Labyrinth Seals,” M.S. thesis, Department of Mechanical Engineering, Texas A&M University, College Station, TX.
17.
Kurtin
, K.
, Childs
, D.
, San Andres
, L.
, and Hale
, K.
, 1993
, “Experimental Versus Theoretical Characteristics of a High-Speed Hybrid (Combination Hydrostatic and Hydrodynamic) Bearing
,” ASME J. Tribol.
, 115
, pp. 160
–169
.18.
Ha
, T. W.
, and Childs
, D. W.
, 1992
, “Friction-Factor Data for Flat-Plate Tests of Smooth and Honeycomb Surfaces
,” ASME J. Tribol.
, 14
, pp. 722
–730
.19.
D’Souza
, R.
, and Childs
, D.
, 2002
, “A Comparison of Rotordynamic-Coefficient Predictions of Annular Honeycomb Gas Seals Using Different Friction-Factor Models
,” ASME J. Tribol.
, 124
, pp. 524
–529
.20.
Ha
, T.-W.
, and Childs
, D.
, 1994
, “Annular Honeycomb-Stator Turbulent Gas Seal Analysis Using A New Friction-Factor Model Based on Flat Plate Tests
,” ASME J. Tribol.
, 116
, pp. 352
–360
.21.
Ha
, T.-W.
, Morrison
, G.
, and Childs
, D.
, 1992
, “Friction-Factor Characteristics for Narrow-Channels With Honeycomb Surfaces
,” ASME J. Tribol.
, 114
, pp. 714
–721
.<Copyright © 2004
by ASME
You do not currently have access to this content.