Patent Number: 8,876,043

Title: Aircraft engine exhaust nozzle system for jet noise reduction

Abstract: The 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.

Inventors: Thomas; Russell H. (Yorktown, VA), Czech; Michael J. (Issaquah, WA), Elkoby; Ronen (Los Angeles, CA)

Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration

International Classification: B64D 33/04 (20060101); B64D 27/26 (20060101); B64D 27/00 (20060101)

Expiration Date: 2019-11-04 0:00:00