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Sound suppression mixerA gas turbine engine flow mixer includes at least one chute having first and second spaced apart sidewalls joined together at a leading edge, with the sidewalls having first and second trailing edges defining therebetween a chute outlet. The first trailing edge is spaced longitudinally downstream from the second trailing edge for defining a septum in the first sidewall extending downstream from the second trailing edge. The septum includes a plurality of noise attenuating apertures.
Document ID
20080004006
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Brown, William H.
Date Acquired
August 24, 2013
Publication Date
March 8, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-PATENT-5,291,672
Patent Application Number: US-PATENT-APPL-SN-987833
Funding Number(s)
CONTRACT_GRANT: NAS3-25415
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,291,672
Patent Application
US-PATENT-APPL-SN-987833
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