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Measured effect of step axial location on labyrinth seal leakageAn advanced, finite volume code has been extensively used in a parametric design study of simple stepped seals, in order to ascertain a leakage-minimizing optimal design and test it, in conjunction with the baseline case of the wear-ring seal of a high pressure pump. It is found that a significant leakage effect arises from this shifting of the rotor and stator sealing surfaces; at extremely low rpm, a significant shaft speed effect occurs for the optimized design in some shaft locations.
Document ID
19930030503
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Morrison, G. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rhode, D. L.
(Texas A & M Univ. College Station, United States)
Date Acquired
August 15, 2013
Publication Date
December 1, 1992
Publication Information
Publication: Journal of Propulsion and Power
Volume: 8
Issue: 6
ISSN: 0748-4658
Subject Category
Mechanical Engineering
Accession Number
93A14500
Distribution Limits
Public
Copyright
Other

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