GAS TURBINE ENGINE COMBUSTION CHAMBER Russian patent published in 2017 - IPC F02C7/22 F23R3/28 

Abstract RU 2620187 C1

FIELD: engines and pumps.

SUBSTANCE: combustion chamber of the gas turbine engine contains an outer shell, a flame tube, a burner plate and nozzles, a ring manifold. The ring collector to which the fuel line is connected is installed in the front cavity on the burner plate. Inside the annular collector, two ring electrodes are concentrically made and connected by insulated high-voltage wires to a high-voltage unit.

EFFECT: increased completeness of fuel combustion in the combustion chamber of a gas turbine engine.

5 cl, 2 dwg

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RU 2 620 187 C1

Authors

Bolotin Nikolaj Borisovich

Dates

2017-05-23Published

2015-12-17Filed