FIELD: mechanical engineering. SUBSTANCE: device is designed for providing uniform temperature field of gas flow behind combustion chambers of gas-turbine engine. Proposed device makes it possible to adjust fuel rate through fuel nozzles by means of adjusting valves installed before fuel nozzle to provide uniform temperature of gas flow after nozzles. EFFECT: improved reliability and increased service life of parts of gas-turbine engine. 2 cl, 1 dwg
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Authors
Dates
2003-11-20—Published
2001-10-01—Filed