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Dynamic, High-Temperature, Flexible SealNew seal consists of multiple plies of braided ceramic sleeves filled with small ceramic balls. Innermost braided sleeve supported by high-temperature-wire-mesh sleeve that provides both springback and preload capabilities. Ceramic balls reduce effect of relatively high porosity of braided ceramic sleeves by acting as labyrinth flow path for gases and thereby greatly increasing pressure gradient seal can sustain. Dynamic, high-temperature, flexible seal employed in hypersonic engines, two-dimensional convergent/divergent and vectorized-thrust exhaust nozzles, reentry vehicle airframes, rocket-motor casings, high-temperature furnaces, and any application requiring non-asbestos high-temperature gaskets.
Document ID
19890000197
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Steinetz, Bruce M.
(NASA Lewis Research Center, Cleveland, OH.)
Sirocky, Paul J.
(Sverdrup Technology, Inc.)
Date Acquired
August 14, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14672
Accession Number
89B10197
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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