FIELD: machine building.
SUBSTANCE: air-jet engine includes a fuel supply pump, an igniter, a combustion chamber and a nozzle. Housing, flow accelerators and combustion chamber form air chambers which are connected to atmosphere.
EFFECT: invention is aimed at reduction of engine weight and reduction of fuel consumption.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TRANSPORT SYSTEM | 2018 |
|
RU2698650C1 |
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| METHOD OF AND DEVICE FOR OPERATION OF RAMJET ENGINE | 2003 |
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| METHOD TO RECOVER SMALL-SIZE SOLID-PROPELLANT ROCKET ENGINES | 2010 |
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RU2429415C1 |
| HYBRID AIR-JET MAGNETOGASDYNAMIC ENGINE | 1998 |
|
RU2138668C1 |
Authors
Dates
2020-01-28—Published
2018-10-15—Filed