FIELD: engine building.
SUBSTANCE: group of inventions relates to equipment, primarily military, namely, to engines of aerial vehicles, and can be used, most likely, in engines of small unmanned aerial vehicles, such as surface-to-air, aviation, and tactical missiles, unmanned reconnaissance aircrafts, flying targets, etc. Forcing of a dual-flow ejector pulse jet engine (DFEPJE) consists in accelerating the combustion process by implementing the mechanism of oxidative methane pyrolysis forming acetylene. In order to implement the described process, coolable plates are installed in the second intake mixer pipe of the DFEPJE, and a coolable channel is installed in the back wall of the combustion chamber. Upon completion of the working cycle, burning gases containing methane, being cooled on the coolable plates and walls of the coolable channel, form acetylene further entering the combustion chamber at the suction cycle and causing acceleration of burning and growth of jet thrust.
EFFECT: claimed group of inventions allows for an increase in the jet thrust of the DFEPJE in the range of 15 to 20%.
2 cl, 5 dwg
Title | Year | Author | Number |
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METHOD FOR BOOSTING DOUBLE-FLOW EJECTOR PULSATING AIR-JET ENGINE AND FORCED DOUBLE-FLOW EJECTOR PULSATING AIR-JET ENGINE | 2021 |
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RU2760339C1 |
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METHOD FOR BOOSTING DOUBLE-FLOW EJECTOR PULSATING AIR-JET ENGINE AND FORCED DOUBLE-FLOW EJECTOR PULSATING AIR-JET ENGINE | 2019 |
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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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RU2608427C1 |
PRECHAMBER PULSATING JET ENGINE | 2021 |
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PULSEJET ENGINE | 2005 |
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PULSEJET ENGINE | 2005 |
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RU2493399C2 |
Authors
Dates
2022-02-01—Published
2020-12-14—Filed