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Stowable Mechanical Sound SuppressorStowable sound suppressor conceived for high-speed commercial transport (HSCT) engines. Suppressor is located just aft of variable nozzle of engine. During takeoff, when suppression of noise required, multisegmented system of separators rotates out of center plug across nozzle stream. Actuation accomplished by single ball-screw drive and links, similar to spokes in umbrella. With iris nozzle translated forward, circumferential row of tubes exposed. Pattern of tubes and separators form suppressor configuration. Flow stream through slots and tubes sized to takeoff area. Useful on any turbo-jet engine in which active suppression of sound required.
Document ID
19900000125
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Thompson, Edward R.
(United Technologies Corp.)
Date Acquired
August 14, 2013
Publication Date
March 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LAR-14158
Report Number: LAR-14158
ISSN: 0145-319X
Accession Number
90B10125
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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