METHOD OF GAS TURBINE ENGINE AFTERBURNING Russian patent published in 2014 - IPC F02K3/10 

Abstract RU 2523510 C1

FIELD: engines and pumps.

SUBSTANCE: proposed method consists in the fuel feed into combustion chamber or compressor in amount required for its complete combustion. Besides, extra fuel is fed into combustion chamber in amount required for decrease in the temperature of gases in combustion chamber to safe limit (atmospheric supercharging). At activation of said atmospheric supercharging and exiting from the turbine igniter of whatever type is fired at a time.

EFFECT: perfected process.

2 cl

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RU 2 523 510 C1

Authors

Staroverov Nikolaj Evgen'Evich

Dates

2014-07-20Published

2013-02-19Filed