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NASA NTRS · 19890000197

Dynamic, High-Temperature, Flexible Seal

Abstract

New 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.

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BibTeXRIS

Steinetz, Bruce M., Sirocky, Paul J.. 1989-04-01. Dynamic, High-Temperature, Flexible Seal. https://ntrs.nasa.gov/citations/19890000197

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