FIELD: engines and pumps.
SUBSTANCE: proposed method comprises producing recesses intended for reducing efflux noise all around outlet hole for at least one of cold and hot flows of turbo fan engine. Said recesses are blind and cut in one of converging circular surfaces that form outlet hole, without cutting into the other converging circular surfaces. Another invention of the set relates to turbo fan engine implemented in compliance with abode described method.
EFFECT: reduced noise of efflux and aerodynamic drag of noise attenuators.
9 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOFAN ENGINE WITH PRECOOLER | 2006 |
|
RU2376205C1 |
TURBOFAN GAS TURBINE ENGINE WITH REDUCED JET NOISE | 2006 |
|
RU2379536C1 |
BYPASS GAS TURBINE ENGINE WITH LOW NOISE LEVEL FOR AIRCRAFT | 2009 |
|
RU2449150C1 |
AIRCRAFT TURBOFAN ENGINE | 2002 |
|
RU2243399C2 |
NOISE-PROTECTION CHEVRON FOR NOZZLE, AS WELL AS NOZZLE AND JET TURBINE ENGINE, WHICH ARE EQUIPPED WITH SUCH CHEVRON | 2008 |
|
RU2466290C2 |
AIRCRAFT TURBOJET LOW-NOISE ENGINE | 2008 |
|
RU2451814C2 |
SEAL FOR TURBO-FAN ENGINE | 2014 |
|
RU2641421C2 |
AIRCRAFT TURBOFAN ENGINE | 2003 |
|
RU2261999C2 |
TURBOFAN WITH DUAL FLOW | 2007 |
|
RU2472961C2 |
TURBOJET ENGINE NACELLE COMPRISES A SECONDARY LOOP NOZZLE WITH ROTATABLE FLAPS | 2015 |
|
RU2688082C2 |
Authors
Dates
2010-04-27—Published
2006-09-01—Filed