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Circumferential pressure distributions in a model labyrinth sealA research program to isolate and study leakage flow through labyrinth glands was initiated. Circumferential pressure distributions were measured in the labyrinth glands with geometry appropriate to the high pressure labyrinths in large steam turbines. Knowledge of this pressure distribution is essential as it is this unequal pressure field that results in the destabilizing force. Parameters that are likely to affect the pressure distributions are incorporated into the test rig. Some preliminary pressure profiles are presented.
Document ID
19830007373
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leong, Y. M. M. S.
(Heriot-Watt Univ. Edinburgh, United Kingdom)
Brown, R. D.
(Heriot-Watt Univ. Edinburgh, United Kingdom)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance
Subject Category
Mechanical Engineering
Accession Number
83N15644
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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