ACOUSTIC OSCILLATION GENERATOR FOR SUPERSONIC AIR BREATHER ENGINE COMBUSTION CHAMBER

摘要

FIELD: aircraft engineering.SUBSTANCE: claimed generator comprises ignition plug, fuel atomisers, shaped geometry of flow section, mixing chamber, vortex chamber, outlet diffuser, blade-type swirler and supersonic diffuser.EFFECT: decreased emission of nitrogen oxides, higher fuel efficiency, no power consumption for pressure development.1 dwg