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Rotordynamic coefficients and leakage flow of parallel grooved seals and smooth sealsBased on Childs finite length solution for annular plain seals an extension of the bulk flow theory is derived to calculate the rotordynamic coefficients and the leakage flow of seals with parallel grooves in the stator. Hirs turbulent lubricant equations are modified to account for the different friction factors in circumferential and axial direction. Furthermore an average groove depth is introduced to consider the additional circumferential flow in the grooves. Theoretical and experimental results are compared for the smooth constant clearance seal and the corresponding seal with parallel grooves. Compared to the smooth seal the direct and cross-coupled stiffness coefficients as well as the direct damping coefficients are lower in the grooved seal configuration. Leakage is reduced by the grooving pattern.
Document ID
19870012773
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nordmann, R.
(Kaiserslautern Univ. Germany)
Dietzen, F. J.
(Kaiserslautern Univ. Germany)
Janson, W.
(Kaiserslautern Univ. Germany)
Frei, A.
(Kaiserslautern Univ. Germany)
Florjancic, S.
(Sulzer Bros. Ltd. Winterthur, Switzerland)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Lewis Research Center Rotordynamic Instability Problems in High-Performance Turbomachinery, 1986
Subject Category
Mechanical Engineering
Accession Number
87N22206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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