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Aircraft Engine Exhaust Nozzle System for Jet Noise ReductionThe aircraft exhaust engine nozzle system includes a fan nozzle to receive a fan flow from a fan disposed adjacent to an engine disposed above an airframe surface of the aircraft, a core nozzle disposed within the fan nozzle and receiving an engine core flow, and a pylon structure connected to the core nozzle and structurally attached with the airframe surface to secure the engine to the aircraft.
Document ID
20150003369
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Thomas, Russell H.
Czech, Michael J.
Elkoby, Ronen
Date Acquired
March 20, 2015
Publication Date
November 4, 2014
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-13/214,469
Patent Number: US-Patent-8,876,043
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,876,043
Patent Application
US-Patent-Appl-SN-13/214,469

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