FIELD: fuel combustion device for gas-turbine engines.
SUBSTANCE: proposed device has case, as well as fixed and movable flow separators wherein fuel is supplied to flame-stabilizing fuel manifolds built of fixed and movable parts and provided with coaxial holes. Movable sleeve is inserted in movable part of stabilizing manifold. Holes are disposed in movable part of stabilizing manifold and in sleeve at right angle to stabilizing manifold axis, and in fixed part holes have their sectional area contracting toward outlet. Springs are installed between movable part of stabilizing manifold and sleeve.
EFFECT: enhanced operating efficiency of combustion chamber throughout entire operating range of engine.
1 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
COMBUSTION CHAMBER FOR GAS TURBINE ENGINE | 2006 |
|
RU2311589C1 |
SPRAYER WITH OXYGEN REPLENISHMENT | 2005 |
|
RU2300052C1 |
DEVICE TO BURN FUEL IN GAS TURBINE ENGINE | 2013 |
|
RU2531477C1 |
METHOD AND DEVICE FOR FUEL COMBUSTION IN HIGH- TEMPERATURE GAS-TURBINE ENGINE | 1994 |
|
RU2124676C1 |
GTE COMBUSTION CHAMBER FRONT DEVICE FUEL-AIR MODULE | 2010 |
|
RU2439435C1 |
METHOD AND DEVICE FOR SUPPLYING FUEL TO MAIN COMBUSTION CHAMBER | 2004 |
|
RU2285204C2 |
COMBUSTION CHAMBER WITH CIRCULAR ULTRASONIC SELF-EXCITED OSCILLATOR FOR FUEL ATOMIZING | 2000 |
|
RU2170884C1 |
GAS TURBINE ENGINE COMBUSTION AFTERBURNER FRONT DEVICE | 2017 |
|
RU2663965C1 |
DEVICE FOR FUEL COMBUSTION IN GAS TURBINE ENGINE | 2015 |
|
RU2651692C2 |
GTE COMBUSTION CHAMBER INJECTOR MODULE | 2010 |
|
RU2439430C1 |
Authors
Dates
2006-10-27—Published
2005-05-05—Filed