FIELD: engine devices and pumps.
SUBSTANCE: hybrid air-breathing engine consists of a compressor, gas-turbine engine, which is followed by a compression and straight-flow combustion chamber, which surrounds the first, with propulsion nozzles, and of a turbine.
EFFECT: creation of a reliable power unit with small weight and dimensions.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| VERSATILE AIR-BREATHER ENGINE | 2015 |
|
RU2608426C2 |
| TURBOJET | 2015 |
|
RU2623588C2 |
| TWO-WHEEL GAS TURBINE ENGINE | 2018 |
|
RU2685170C1 |
| DOUBLE-ROW GAS TURBINE ENGINE | 2017 |
|
RU2673838C2 |
| INTERMITTENT-CYCLE GAS TURBINE ENGINE | 2015 |
|
RU2617222C2 |
| AIRCRAFT GAS-TURBINE ENGINE | 1998 |
|
RU2162957C2 |
| GAS-TURBINE ENGINE | 1997 |
|
RU2161714C2 |
| INTERMITTENT-CYCLE GAS TURBINE ENGINE (IGTE) | 2011 |
|
RU2478804C2 |
| HYBRID JET ENGINE | 2005 |
|
RU2272926C1 |
| GAS-TURBINE ENGINE | 1995 |
|
RU2096639C1 |
