FIELD: gas-turbine engines. SUBSTANCE: proposed fuel injector has cylindrical fuel chamber with fuel nozzle connected to it and main and additional gas nozzles directed tangentially through side wall; injector is also provided with outlet nozzle. Additional gas nozzles are made in form of tangential slots directed to the same side as main nozzles. They are located before outlet nozzle. Ratio of diameter of vortex chamber to equivalent diameter of gas nozzle is selected from relationship given in Invention. EFFECT: increased power of acoustic oscillations; possibility of regulation of fuel jet. 3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
GAS TURBINE ENGINE RING COMBUSTION CHAMBER | 2002 |
|
RU2210034C1 |
REHEAT UNIT OF DOUBLE-FLOW TURBOJET ENGINE | 2002 |
|
RU2209992C1 |
METHOD FOR RECORDING FUEL INGNITION IN AFTERBURNER OF GAS TURBINE ENGINE | 2002 |
|
RU2211934C1 |
METHOD OF TESTING ROTOR PARTS OF GAS TURBINE ENGINE FOR PRESET SERVICE LIFE IN ENGINE SYSTEM | 2001 |
|
RU2210067C1 |
METHOD OF TESTING GAS TURBINE ENGINES WITH DUE ACCOUNT OF SEASON WHEN TESTS ARE CARRIED OUT | 2001 |
|
RU2210066C1 |
CATALYTIC IGNITER | 2002 |
|
RU2232349C1 |
TRANSPORTABLE MODULAR GAS-TURBINE POWER PLANT | 2001 |
|
RU2189477C1 |
GAS-TURBINE UNIT | 2001 |
|
RU2189454C1 |
REHEATED TURBOJET ENGINE THRUST CONTROL METHOD | 2002 |
|
RU2220305C1 |
FAN CHARACTERISTICS READOUT DEVICE IN BYPASS TURBOJET ENGINE WITH SEPARATED NOZZLES OF OUTER AND INNER LOOPS | 2003 |
|
RU2238419C1 |
Authors
Dates
2003-08-10—Published
2001-12-27—Filed