COMBUSTION CHAMBER OF A GAS TURBINE ENGINE Russian patent published in 2018 - IPC F23R3/30 

FIELD: motors and pumps.

SUBSTANCE: combustion chamber of a gas turbine engine contains a flame chamber with holes, nozzles, a fuel line and electrodes connected by high-voltage insulated wires, and a heating chamber. Heating chamber is connected by a channel with a flame chamber. Inside the heating chamber is mounted a heating element and ceramic partitions with holes with the possibility of circulation and heating of air flows. Inside the heating element, chambers are made with the possibility of heating the fuel to a gaseous state. Inputs of the chambers are connected by pipes to the fuel line, and the outlets are connected by pipes with horizontal nozzles mounted in the channel. Channel is equipped with vertical nozzles connected to the fuel line. Inside the horizontal and vertical nozzles placed electrodes. Blade is installed inside the channel. Heating chamber is made in the form of a housing where inside the rings of different diameters are mounted. High-temperature heat-insulating layer is mounted on the inner surfaces of the heating chamber and the channel.

EFFECT: invention is aimed to increase the combustion of fuel.

8 cl, 5 dwg