FIELD: engines and pumps.
SUBSTANCE: each pylon has three channels plugged from side, open ends of two of these channels are closed by plugs, channels are connected by holes, and in central channel there is a damper with several holes.
EFFECT: elimination of pylons burnout at high thermal loads, enhanced reliability of blisk of fuel supply, expanded performance range of fuel consumption at practically constant pressure drop on nozzles for improvement of combustion efficiency of fuel-air mixture.
2 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
HYPERSONIC RAMJET ENGINE AND METHOD OF ORGANIZATION OF COMBUSTION | 2003 |
|
RU2262000C2 |
ANNULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE AND METHOD OF ITS OPERATION | 2007 |
|
RU2347144C1 |
PYLON-AUTOIGNITER OF FUEL | 2010 |
|
RU2428576C1 |
GENERATOR OF HIGH-ENTHALPY AIRFLOW AND METHOD OF ITS OPERATION | 2009 |
|
RU2395795C1 |
METHOD OF THERMO ABRASIVE TREATMENT AND MACHINE "CASTOR" FOR ITS IMPLEMENTATION | 2005 |
|
RU2338638C2 |
INJECTOR | 2010 |
|
RU2447362C1 |
HIGH SPEED RAMJET ENGINE | 2013 |
|
RU2544105C1 |
SELF-IGNITION OF FUEL MIX IN RAMJET ENGINE | 2010 |
|
RU2444639C1 |
METHOD OF SETTING-UP COMBUSTION IN HYPERSONIC RAMJET ENGINE AND HYPERSONIC RAMJET ENGINE FOR REALIZATION OF THIS METHODS (VERSIONS) | 1994 |
|
RU2082017C1 |
FUEL INJECTOR OF GTE | 2018 |
|
RU2699111C1 |
Authors
Dates
2018-01-25—Published
2016-12-26—Filed