FIELD: fuel combustion in gas-turbine engine. SUBSTANCE: the fuel-air furnace of gas turbine engine has a double-level swirler with a vane swirler with an open outlet end installed in the inner level. Located on the inlet end of the axial vane swirler is a partition made, for example, in the form of a ring. EFFECT: expanded field of starting and stable operation of the combustion chamber due to the increase of the spray-cone angle of the fuel-air mixture at the swirler outlet and intensified mixing. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL-AIR BURNER OF THE COMBUSTION CHAMBER OF A GAS TURBINE ENGINE | 2004 |
|
RU2267710C1 |
| AIR-FUEL BURNER AND FRONTAL DEVICE OF COMBUSTION CHAMBER | 2020 |
|
RU2749434C1 |
| FUEL-AIR BURNER OF COMBUSTION CHAMBER OF GAS-TURBINE ENGINE | 2001 |
|
RU2224954C2 |
| FUEL-AIR BURNER FOR GAS-TURBINE ENGINE COMBUSTION CHAMBER | 2003 |
|
RU2264584C2 |
| COMBUSTION CHAMBER OF GAS-TURBINE ENGINE | 2004 |
|
RU2273798C2 |
| FUEL-AND-AIR BURNER OF GAS-TURBINE ENGINE COMBUSTION CHAMBER | 1997 |
|
RU2134839C1 |
| COMBUSTION CHAMBER FUEL-AIR BURNER | 2024 |
|
RU2825500C1 |
| AIR-AND-FUEL BURNER OF COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 2009 |
|
RU2406934C1 |
| AIR-ASSISTED FUEL BURNER | 1995 |
|
RU2157954C2 |
| BURNER | 2002 |
|
RU2197685C1 |
