GAS TURBINE ENGINE ANNULAR COMBUSTION CHAMBER Russian patent published in 2013 - IPC F23R3/34 

Abstract RU 2476774 C2

FIELD: engines and pumps.

SUBSTANCE: proposed combustion chamber comprises housing with, at least, one air intake opening arranged at chamber inlet, and fuel feed device. The latter comprises multiple injectors arranged in circle, at least one of which is located with said air intake opening. Fuel feed device comprises means to decrease amount of fuel fed into injector arranged closer to intake opening than other fuel injectors.

EFFECT: smaller hot spots caused by intake in area behind combustion chamber.

9 cl, 5 dwg

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RU 2 476 774 C2

Authors

P'Esserg Kristof

Sandeli Deni Zhan Moris

Dates

2013-02-27Published

2008-10-30Filed