FIELD: engines and pumps.
SUBSTANCE: claimed gas turbine engine comprises the air channel including the air intake and at least one compressor stage, combustion chamber, gas turbine, at least one shaft engaging the compressor and gas turbine, jet nozzle and fuel feed system. Said gas turbine engine includes the air activator arrange outside the engine and its inlet is communicated with the compressor outlet while activator outlet is communicated with the combustion chamber.
EFFECT: enhanced power output.
19 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HYDROGEN GAS TURBINE ENGINE | 2014 |
|
RU2554392C1 |
| HYDROGEN GAS TURBINE ENGINE | 2014 |
|
RU2561764C1 |
| HYDROGEN GAS-TURBINE ENGINE | 2014 |
|
RU2552012C1 |
| GAS COMPRESSOR UNIT | 2015 |
|
RU2610631C1 |
| GAS-COMPRESSOR UNIT | 2015 |
|
RU2625885C2 |
| HYDROGEN AIR-JET ENGINE | 2014 |
|
RU2553052C1 |
| RETURN STAGE OF ROCKET VEHICLE, METHOD OF ITS OPERATION AND GAS TURBINE ENGINE | 2015 |
|
RU2609664C1 |
| RETURN CARRIER ROCKET STAGE, METHOD OF ITS OPERATION AND GAS TURBINE ENGINE | 2015 |
|
RU2602656C1 |
| DOUBLE-FUEL AIR-JET ENGINE | 2014 |
|
RU2561773C1 |
| THREE-COMPONENT AIR-JET ENGINE | 2014 |
|
RU2561757C1 |
