FIELD: machine building.
SUBSTANCE: combustion chamber comprises tube bundle, which passes in radial direction through at least part of combustion chamber. Said tube bundle has upstream surface separated from downstream surface in axial direction. Tubes pass from upstream surface through downstream surface, wherein each tube provides flow communication through tube bundle. Between adjacent tubes inside tube bundle deflector passes in axial direction. Method of fuel distribution in combustion chamber includes provision of fuel passing to overpressure chamber, confined by, at least, partially upstream surface, downstream surface, casing and tubes, passing from upstream to downstream surface.
EFFECT: said method further includes provision of fuel collision with deflector, which passes in axial direction inside increased pressure fuel chamber between adjacent tubes.
20 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SYSTEM FOR WORKING FLUID SUPPLY INTO COMBUSTION CHAMBER (VARIANTS) | 2013 |
|
RU2613764C2 |
| COMBUSTION CHAMBER (VERSIONS) | 2013 |
|
RU2614887C2 |
| LOCATION OF COMBUSTION CHAMBER BURNERS | 2015 |
|
RU2642971C1 |
| SYSTEM FOR FUEL SUPPLY TO COMBUSTION CHAMBER (VERSIONS) | 2013 |
|
RU2618765C2 |
| FIREBOX (VERSIONS) AND METHOD OF FUEL DISTRIBUTION IN FURNACE | 2012 |
|
RU2611551C2 |
| FUEL NOZZLES UNIT AND UNIT OF COMBUSTION CHAMBER | 2012 |
|
RU2605164C2 |
| SYSTEM (OPTIONS) AND METHOD FOR DAMPING DYNAMIC PROCESSES IN COMBUSTION CHAMBER | 2013 |
|
RU2661440C2 |
| MODULAR INJECTION HEAD FOR THE COMBUSTION CHAMBER OF A GAS TURBINE | 2018 |
|
RU2769773C2 |
| COMBUSTION CHAMBER AND GAS TURBINE ENGINE COMPRISING SUCH COMBUSTION CHAMBER | 2019 |
|
RU2738248C1 |
| INJECTION HEAD FOR THE COMBUSTION CHAMBER OF A GAS TURBINE | 2018 |
|
RU2769616C2 |
