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Self-acting shaft sealsReport reviews operating principles and design of self-acting seals. Influences of adverse operating conditions are considered also. Elements of analysis used in seal performance predictions are described and evaluated. Mathematical models for obtaining seal force balance and equilibrium film thickness are outlined. Self-acting seals are nonrubbing, have lower leakage rates than labyrinth seals, and are well suited for advanced aircraft engines.
Document ID
19800000109
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Ludwig, L. P.
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 1
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-13229
Accession Number
80B10109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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