FIELD: engines and pumps.
SUBSTANCE: method of forcing the turbojet engine, consisting of an input device, a turbocharger, in which the turbine blades are cooled by air drawn from a compressor, the output device. The input to the compressor is supplied with water. Water is supplied to the flight speed more than 3.2 Mach numbers at the gas temperature before the turbine blades of more than 2300 K, and the compressor rotational speed exceeding more than 1.3 times the speed of the compressor under takeoff.
EFFECT: method allows aircraft with turbojet engines todevelop hypersonic flight speed, can be used as interceptor aircraft.
3 cl, 5 dwg
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