FIELD: power engineering, transport engineering and chemical engineering; combustion chambers of gas turbines. SUBSTANCE: fuel is first fed to first-loop burners and then to parallel burners of next loops; differentials of fuel and air pressures are maintained constant in all operating loops but for one loop. EFFECT: enhanced efficiency. 3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
COMBUSTION CHAMBER | 1993 |
|
RU2087805C1 |
COMBUSTION CHAMBER | 1997 |
|
RU2116575C1 |
BURNER | 1996 |
|
RU2099639C1 |
COMBUSTION CHAMBER | 1992 |
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COMBUSTION CHAMBER | 1999 |
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RU2162194C1 |
BURNER | 2007 |
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RU2343352C1 |
BURNER OF GAS-TURBINE ENGINE COMBUSTION CHAMBER | 1993 |
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COMBUSTIBLE CHAMBER | 1991 |
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HEATER | 2007 |
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RU2348864C2 |
FUEL COMBUSTION METHOD AND DEVICE FOR REALIZATION OF SAID METHOD | 2006 |
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Authors
Dates
1997-07-10—Published
1993-11-02—Filed