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Dynamics of face and annular seals with two-phase flowA detailed study was made of face and annular seals under conditions where boiling, i.e., phase change of the leaking fluid, occurs within the seal. Many seals operate in this mode because of flashing due to pressure drop and/or heat input from frictional heating. High pressure, water pumps, industrial chemical pumps, and cryogenic pumps are mentioned as a few of many applications. The initial motivation was the LOX-GOX seals for the space shuttle main engine, but the study was expanded to include any face or annular seal where boiling occurs. Some of the distinctive behavior characteristics of two-phase seals were discussed, particularly their axial stability. While two-phase seals probably exhibit instability to disturbances of other degrees of freedom such as wobble, etc., under certain conditions, such analyses are too complex to be treated at present. Since an all liquid seal (with parallel faces) has a neutral axial stiffness curve, and is stabilized axially by convergent coning, other degrees of freedom stability analyses are necessary. However, the axial stability behavior of the two-phase seal is always a consideration no matter how well the seal is aligned and regardless of the speed. Hence, axial stability is thought of as the primary design consideration for two-phase seals and indeed the stability behavior under sub-cooling variations probably overshadows other concerns. The main thrust was the dynamic analysis of axial motion of two-phase face seals, principally the determination of axial stiffness, and the steady behavior of two-phase annular seals. The main conclusions are that seals with two-phase flow may be unstable if improperly balanced. Detailed theoretical analyses of low (laminar) and high (turbulent) leakage seals are presented along with computer codes, parametric studies, and in particular a simplified PC based code that allows for rapid performance prediction. A simplified combined computer code for the performance prediction over the laminar and turbulent ranges of a two-phase seal is described and documented. The analyses, results, and computer codes are summarized.
Document ID
19910017165
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hughes, William F.
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Basu, Prithwish
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Beatty, Paul A.
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Beeler, Richard M.
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Lau, Stephen
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1989
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-4256
NAS 1.26:4256
E-4999
Report Number: NASA-CR-4256
Report Number: NAS 1.26:4256
Report Number: E-4999
Accession Number
91N26479
Funding Number(s)
CONTRACT_GRANT: NAG3-166
PROJECT: RTOP 591-41-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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