METHOD OF TURBOJET AFTERBURNING AND ENGINE TO THIS END (VERSIONS) Russian patent published in 2013 - IPC F02K3/08 F02C3/20 

FIELD: engines and pumps.

SUBSTANCE: proposed method consists in feeding gas mixture into combustion chamber, and/or upstream of compressor, and/or in compressor stage, in amount sufficient to complete combustion a portion of it and cooling of formed gases by evaporation of excess gas mixture. On increasing gas mixture feed to stoichiometric ratio into combustion chamber, and/or compressor and/or compressor stage, feed of vaporising incombustible fluid is increased which, with stoichiometric ratio reached, is substituted by feed of gas mixture. Water or its mix with glycols and/or wetting agents and/or oil emulsion while combustible fluid represents kerosene or ethyl ether, or alcohol, or propane, or methane.

EFFECT: higher thrust and power output.

13 cl, 6 dwg