FIELD: military equipment.
SUBSTANCE: group of inventions relates to military equipment, particularly, to aircraft engines. Forcing of double-flow ejector pulsating air-jet engine consists in fuel supply to aerodynamic valve of the second circuit, its further jet mixing with fuel in combustion chamber and ignition. Supply of fuel to engine at suction cycle is performed simultaneously through two circuits of aerodynamic inlet valves – with further arrangement of intensive mixing in combustion chamber by jet blowing of combustion zone with formation of annular vortices. Besides, additionally braking of back emission of gases through inlet system is performed due to installation of triangular channel into the first mixer and annular shell at the inlet of the second mixer and return flow to resonator pipe due to performance of partial diffuser opening.
EFFECT: claimed group of inventions makes it possible to increase thermodynamic efficiency by increasing amplitude of pressure pulsations occurring at increase of volume of cyclic blowdown of combustion chamber.
3 cl, 3 dwg
Title | Year | Author | Number |
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METHOD FOR FORCING TWO-CIRCUIT EJECTOR PULSATING AIR-JET ENGINE AND FORCED TWO-CIRCUIT EJECTOR PULSATING AIR-JET ENGINE | 2020 |
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TWO-CIRCUIT EJECTOR PULSATING AIR-JET ENGINE | 2020 |
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FORCED DUAL-CIRCUIT EJECTOR PULSATING AIR-JET ENGINE | 2019 |
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RU2717479C1 |
METHOD OF PULSE JET ENGINE DOUBLE-FLOW BLOWING AND DOUBLE-FLOW PULSE JET ENGINE | 2015 |
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PRECHAMBER PULSATING JET ENGINE | 2021 |
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PULSATING AIR-BREATHING DETONATION ENGINE | 2010 |
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PULSEJET ENGINE | 2005 |
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METHOD TO IMPLEMENT CYCLIC DETONATION BURNING IN INTERMITTENT AIR JET ENGINE | 2011 |
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RU2493399C2 |
Authors
Dates
2020-02-17—Published
2019-07-10—Filed