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Dynamic, High-Temperature, Flexible SealsDynamic, flexible ceramic seals developed for use at high temperatures in high-performance, variable-geometry, hypersonic airplane engines. Stacked ceramic wafers pressed against stationary sidewall by pressure in one or more metal bellows. Seals also used in hypersonic engines, two-dimensional convergent/divergent and vectored-thrust exhaust nozzles, airframes of reentry vehicles, casings of rocket motors furnaces, and other applications.
Document ID
19920000173
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Steinetz, Bruce M.
(NASA Lewis Research Center, Cleveland, OH.)
Sirocky, Paul J.
(Sverdrup Technologies, Inc.)
Date Acquired
August 15, 2013
Publication Date
March 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-14695
Accession Number
92B10173
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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