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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Authors
Dates
2015-11-10—Published
2013-11-15—Filed