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Multiple pure tone elimination strut assemblyAn acoustic noise elimination assembly is disclosed which has a capability for disrupting the continuity of fields of sound pressures forwardly projected from fans or rotors of a type commonly found in the fan or compressor first stage for air-breathing engines, when operating at tip speeds in the supersonic range. The assembly includes a tubular cowl defining a duct for delivering an air stream axially into the intake for a jet engine. A sound barrier, defined by a number of intersecting flat plates or struts has a line of intersection coincident with a longitudinal axis of the tubular cowl, which serves to disrupt the continuity of rotating fields of multiple pure tonal components of noise.
Document ID
19820008926
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Burcham, F. W.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 4, 2013
Publication Date
November 17, 1981
Subject Category
Acoustics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-185869
Patent Number: US-PATENT-4,300,656
Patent Number: NASA-CASE-FRC-11062-1
Accession Number
82N16800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,300,656|NASA-CASE-FRC-11062-1
Patent Application
US-PATENT-APPL-SN-185869
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