FIELD: engines and pumps.
SUBSTANCE: proposed ramjet comprises air intake, fuel nozzle arranged ahead of said air intake along its axis and connected therewith by pylons, combustion chamber, igniter and nozzle. Fuel nozzle is composed by gas-jet resonator with sharp leading edge, resonator inlet is combined with engine front part to face incoming flow. Resonator side and rear walls are porous and feature controlled open ratio. At fuel combustion in combustion chamber, nano-dispersed fuel is fed in two flows via fuel nozzle, said fuel including carbon nanotubes with hydrogen encapsulated therein: via gas-jet resonator inlet towards incoming flow and via its porous walls to create pulsating electric field in combustion zone, its intensity exceeding 20 V/cm.
EFFECT: higher completeness of fuel combustion and engine fuel efficiency.
2 cl, 1 dwg
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