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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
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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