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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|---|---|---|---|
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 | RU2520784C1 | 
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 | RU2542652C1 | 
| HYPERSONIC RAMJET ENGINE AND CONCEPT OF COMBUSTION | 2012 | 
 | RU2516735C1 | 
| HYPERSONIC RAMJET ENGINE AND METHOD OF ORGANIZATION OF COMBUSTION | 2003 | 
 | RU2262000C2 | 
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 | RU2775105C1 | 
| METHOD OF IGNITION AND COMBUSTION OF FUEL IN ATHODYD | 2013 | 
 | RU2550209C1 | 
| HYPERSONIC RAMJET ENGINE | 2017 | 
 | RU2691702C2 | 
| SWIRL BURNER | 2006 | 
 | RU2310794C1 | 
| AIRCRAFT POWER UNIT | 2013 | 
 | RU2601690C2 | 
Authors
Dates
2015-11-10—Published
2013-11-15—Filed