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Annular honeycomb seals: Test results for leakage and rotordynamic coefficients; comparisons to labyrinth and smooth configurationsTest results are presented for leakage and rotordynamic coefficients for seven honeycomb seals. All seals have the same radius, length, and clearance; however, the cell depths and diameters are varied. Rotordynamic data, which are presented, consist of the direct and cross-coupled stiffness coefficients and the direct damping coefficients. The rotordynamic-coefficient data show a considerable sensitivity to changes in cell dimensions; however, no clear trends are identifiable. Comparisons of test data for the honeycomb seals with labyrinth and smooth annular seals show the honeycomb seal had the best sealing (minimum leakage) performance, followed in order by the labyrinth and smooth seals. For prerotated fluid entering the seal, in the direction of shaft rotation, the honeycomb seal has the best rotordynamic stability followed in order by the labyrinth and smooth. For no prerotation, or fluid prerotation against shaft rotation, the labyrinth seal has the best rotordynamic stability followed in order by the smooth and honeycomb seals.
Document ID
19890013528
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Childs, Dara W.
(Texas A&M Univ. College Station, TX, United States)
Elrod, David
(Texas A&M Univ. College Station, TX, United States)
Hale, Keith
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Publication Information
Publication: NASA, Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1988
Subject Category
Mechanical Engineering
Accession Number
89N22899
Funding Number(s)
CONTRACT_GRANT: NAG3-181
CONTRACT_GRANT: F49620-82-K-0033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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