FIELD: combustion chambers of gas-turbine engines working mainly on gaseous fuel. SUBSTANCE: each burner of combustion zone and pilot combustion zone. Combustion process in pilot zone is organized at excess air coefficient of α = 1.2 to 1.4 and in main combustion zone at excess air coefficient of α = 1.8 to 2.0. EFFECT: enhanced efficiency. 2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIR-GAS BURNER | 1997 |
|
RU2146788C1 |
| GAS-TURBINE ENGINE FUEL-FEED CONTROL METHOD | 1997 |
|
RU2162953C2 |
| ANNULAR COMBUSTION CHAMBER | 1996 |
|
RU2161756C2 |
| AIR-ASSISTED FUEL BURNER | 1995 |
|
RU2157954C2 |
| RING COMBUSTION CHAMBER | 1993 |
|
RU2099640C1 |
| FORECHAMBER OF COMBUSTION CHAMBER | 1994 |
|
RU2086857C1 |
| COMBUSTION CHAMBER | 1993 |
|
RU2087805C1 |
| RING COMBUSTION CHAMBER FOR GAS-TURBINE ENGINE | 2004 |
|
RU2280814C1 |
| INJECTION BURNER | 1994 |
|
RU2118753C1 |
| IGNITER | 1994 |
|
RU2103610C1 |
Authors
Dates
1998-03-27—Published
1993-07-01—Filed