Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft

Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft

US Patent 7810335 · Granted Oct 12, 2010

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Attachment pylon for a turbine engine2018
Tail cone for a microjet rotary turbine engine2018
Primary cowl of a turbofan comprising a rotating ring having micro-jets2017
Bypass turbojet2017
Device for reducing the noise emitted by the jet of an aircraft propulsion engin2016
Method of processing acoustic waves emitted at the outlet of a turbo engine of a2016
Turboshaft engine supporting pylon covered with a porous material and turboshaft2014
Turbine engine with nonstreamlined impellers2014
Bypass turbomachine with reduction of jet noise2011
Variable-section flow mixer for a double-flow turbojet for a supersonic airplane2010
Variable-section flow mixer for a double-flow turbojet for a supersonic airplane2010
Rotary motion mixer for a converging-stream nozzle of a turbomachine2010