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Hybrid Active/Passive Jet Engine Noise Suppression SystemA novel adaptive segmented liner concept has been developed that employs active control elements to modify the in-duct sound field to enhance the tone-suppressing performance of passive liner elements. This could potentially allow engine designs that inherently produce more tone noise but less broadband noise, or could allow passive liner designs to more optimally address high frequency broadband noise. A proof-of-concept validation program was undertaken, consisting of the development of an adaptive segmented liner that would maximize attenuation of two radial modes in a circular or annular duct. The liner consisted of a leading active segment with dual annuli of axially spaced active Helmholtz resonators, followed by an optimized passive liner and then an array of sensing microphones. Three successively complex versions of the adaptive liner were constructed and their performances tested relative to the performance of optimized uniform passive and segmented passive liners. The salient results of the tests were: The adaptive segmented liner performed well in a high flow speed model fan inlet environment, was successfully scaled to a high sound frequency and successfully attenuated three radial modes using sensor and active resonator arrays that were designed for a two mode, lower frequency environment.
Document ID
19990032037
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Parente, C. A.
(Northrop Grumman Corp. Bethpage, NY United States)
Arcas, N.
(Northrop Grumman Corp. Bethpage, NY United States)
Walker, B. E.
(Hersh Acoustical Engineering, Inc. Westlake Village, CA United States)
Hersh, A. S.
(Hersh Acoustical Engineering, Inc. Westlake Village, CA United States)
Rice, E. J.
(Rice (E. J.) Consulting Westlake, OH United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1999
Subject Category
Acoustics
Report/Patent Number
E-11570
NASA/CR-1999-208875
NSL-RPT-98-002
NAS 1.26:208875
Report Number: E-11570
Report Number: NASA/CR-1999-208875
Report Number: NSL-RPT-98-002
Report Number: NAS 1.26:208875
Funding Number(s)
CONTRACT_GRANT: NCC3-379
PROJECT: RTOP 538-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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