Rotor dynamic and leakage coefficients are presented for a labyrinth seal that was tested at a supply pressure of 70 bar-a and speeds up to 20,200 rpm. Tests were conducted at clearances of 0.1 mm and 0.2 mm, pressure ratios of 0.10, 0.31, and 0.52, and three preswirls ratios. Comparisons are made between test data and predictions from one-control-volume and two-control-volume bulk-flow models. Generally, theoretical predictions agree poorly with the test results, with the one-control volume model giving better predictions. The one-control-volume model provides a conservative prediction for effective damping; i.e., this parameter is underestimated. Both models under predict leakage rates. Comparisons are also made between rotordynamic coefficients of labyrinth and hole-pattern seals.
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October 2005
Technical Papers
Rotordynamic Coefficients for a Tooth-on-Stator Labyrinth Seal at 70 Bar Supply Pressures: Measurements Versus Theory and Comparisons to a Hole-Pattern Stator Seal
Arthur Picardo,
Arthur Picardo
Test Engineer
Flowserve Corp.
Vernon, CA 90058
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Dara W. Childs
Dara W. Childs
Leland T. Jordan Professor of Mechanical Engineering
Turbomachinery Laboratory,
e-mail: dchilds@mengr.tamu.edu
Texas A&M University
, College Station, TX 77843
Search for other works by this author on:
Arthur Picardo
Test Engineer
Flowserve Corp.
Vernon, CA 90058
Dara W. Childs
Leland T. Jordan Professor of Mechanical Engineering
Turbomachinery Laboratory,
Texas A&M University
, College Station, TX 77843e-mail: dchilds@mengr.tamu.edu
J. Eng. Gas Turbines Power. Oct 2005, 127(4): 843-855 (13 pages)
Published Online: March 1, 2004
Article history
Received:
October 1, 2003
Revised:
March 1, 2004
Citation
Picardo, A., and Childs, D. W. (March 1, 2004). "Rotordynamic Coefficients for a Tooth-on-Stator Labyrinth Seal at 70 Bar Supply Pressures: Measurements Versus Theory and Comparisons to a Hole-Pattern Stator Seal." ASME. J. Eng. Gas Turbines Power. October 2005; 127(4): 843–855. https://doi.org/10.1115/1.1924634
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