FIELD: engines and pumps.
SUBSTANCE: turboram air-jet engine comprises a turbojet engine with an afterburner and a jet nozzle (ATE), gas temperature measurement system behind the main combustion chamber of the turbojet engine, as well as direct-flow circuit positioned coaxially to the turbojet engine. The direct-flow circuit is connected to the air intake of the aircraft via the shut-off device, comprising a diffuser, a jet nozzle and a combustion chamber. The internal channel of the turbojet engine afterburner is connected to the internal cavity of the direct-flow circuit combustion chamber via the radial flame stabilizers of V-shaped profile for the supply of combustion products from the afterburner to the direct-flow circuit combustion chamber channel.
EFFECT: higher efficiency of the aircraft ducted jet engine intended to fly in a wide range of flight velocity from subsonic to Mach equal to 4 or higher.
6 cl, 1 dwg
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