Invention Grant
US08876043B2 Aircraft engine exhaust nozzle system for jet noise reduction 有权
用于喷气降噪的飞机发动机排气喷嘴系统

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.
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