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
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AIR-ASSISTED FUEL BURNER | 1995 |
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FORECHAMBER OF COMBUSTION CHAMBER | 1994 |
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COMBUSTION CHAMBER | 1993 |
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RING COMBUSTION CHAMBER FOR GAS-TURBINE ENGINE | 2004 |
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Authors
Dates
1998-03-27—Published
1993-07-01—Filed