FIELD: engines and pumps.
SUBSTANCE: proposed engine comprises casing that, together with nacelle, makes circular channel for secondary airflow developed by blower to pass through. First-circuit nozzle is secured on nacelle, behind the engine, to direct primary hot airflow developed by the engine. Said nozzle has inner wall on its one side and outer wall in contact with secondary on its opposite side. Said inner wall incorporated noise killer device and sheet element furnished with cooling air distributor along inner wall. Said noise killer device is arranged downstream of cooling air distributer. Outer wall comprises device cooling inner wall. Another invention of the set relates to first-circuit nozzle designed as described above.
EFFECT: possibility to use lower-density and lower-thermostability materials to compensate for weight of noise killer.
10 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBO-JET PLANT FOR AIRCRAFT | 2007 |
|
RU2436988C2 |
AIRCRAFT AIR INTAKE | 2019 |
|
RU2791797C2 |
TURBOJET NACELLE EQUIPPED WITH NACELLE COMPONENT COOLING ASSY | 2011 |
|
RU2552574C2 |
NACELLE OF JET TURBINE ENGINE, WHICH IS EQUIPPED WITH REDUCTION DEVICES OF NOISE CREATED WITH SUCH ENGINE | 2007 |
|
RU2445489C2 |
SOUND-ABSORBING DEVICE IN TWO-CIRCUIT TURBOJET ENGINE | 2002 |
|
RU2230208C2 |
TURBOFAN ENGINE WITH PRECOOLER | 2006 |
|
RU2376205C1 |
AIRCRAFT BYPASS GAS TURBINE ENGINE FURNISHED WITH PRECOOLER | 2007 |
|
RU2382221C1 |
SOUND-ABSORBING PANEL FOR EJECTOR NOZZLE | 2009 |
|
RU2526215C2 |
SEAL WITH INTEGRATED JOINT SURFACE | 2008 |
|
RU2463511C2 |
NACELLE FOR DOUBLE-FLOW JET TURBINE ENGINE WITH HIGH BYPASS RATIO | 2007 |
|
RU2435056C2 |
Authors
Dates
2010-08-20—Published
2005-05-17—Filed