FIELD: gas turbine engine engineering.
SUBSTANCE: system comprises hollow tubular structure (41) for flowing the fuel-air mixture to combustion chamber (12), means (38) for fuel injection arranged at the front end of the hollow tubular structure, means (28) and (32) for blowing air arranged downstream of means (38) for fuel injection, means (42) for generating cold plasma and mounted downstream of means (28) for air blowing, and means for control of the means (42) for generating cold plasma depending on the regime of operation of the gas turbine engine.
EFFECT: reduced toxicity of gas emission.
16 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-STAGE SYSTEM FOR INJECTING FUEL-AIR MIXTURE INTO COMBUSTION CHAMBER OF TURBINE MACHINE | 2002 |
|
RU2293862C2 |
| SYSTEM FOR SUPPLYING FUEL-AIR MIXTURE TO COMBUSTION CHAMBER | 2003 |
|
RU2303199C2 |
| TUBULAR-RING COMBUSTION CHAMBER WITH STAGED AND TANGENTIAL FUEL-AIR NOZZLES FOR USE IN GAS TURBINE ENGINES | 2011 |
|
RU2611217C2 |
| GAS-TURBINE COMBUSTION SYSTEM | 2013 |
|
RU2561956C2 |
| TUBULAR COMBUSTION CHAMBER OF GAS-TURBINE ENGINE AND DIFFUSION ADJUSTABLE NOZZLE FOR PRELIMINARY PREPARATION OF MIXTURE | 1991 |
|
RU2076276C1 |
| GTE COMBUSTION CHAMBER FRONT DEVICE FUEL-AIR MODULE | 2010 |
|
RU2439435C1 |
| FOAMING ATOMISER FOR AERO-MECHANICAL INJECTION SYSTEM OF AIR-AND-FUEL MIXTURE TO COMBUSTION CHAMBER OF TURBOMACHINE, AERO-AND-FUEL INJECTION SYSTEM, COMBUSTION CHAMBER OF TURBOMACHINE, AND TURBOMACHINE | 2005 |
|
RU2382942C2 |
| METHOD OF FUEL INJECTION INTO COMBUSTION CHAMBER OF GAS TURBINE ENGINE AND INJECTION SYSTEM FOR ITS IMPLEMENTATION | 2012 |
|
RU2598502C2 |
| FRONT DEVICE OF COMBUSTION CHAMBER OF GAS-TURBINE ENGINE | 2017 |
|
RU2667820C1 |
| MIXING OF COMBUSTIBLE SUBSTANCES PROCEDURE FOR GAS TURBINE ENGINE COMBUSTION CHAMBER | 2011 |
|
RU2619673C2 |
