ACOUSTIC OSCILLATION GENERATOR FOR SUPERSONIC AIR BREATHER ENGINE COMBUSTION CHAMBER Russian patent published in 2015 - IPC F02K7/10 

Abstract RU 2567528 C2

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

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RU 2 567 528 C2

Authors

Piralishvili Shota Aleksandrovich

Gur'Janov Aleksandr Igorevich

Vereshchagin Ivan Mikhajlovich

Bogdanov Vasilij Ivanovich

Dates

2015-11-10Published

2013-11-15Filed