FIELD: space engineering. SUBSTANCE: heat exchanger mounted inside the gas-air path consists of two parallel sections. Heat-exchanger-generator and steam turbine are positioned inside the fuel path. The compressor of the engine comprises two stages. EFFECT: improved design. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HYPERSONIC CRYOGENIC AIR-JET ENGINE | 1997 |
|
RU2179255C2 |
| COMBINED AIRCRAFT ENGINE | 2018 |
|
RU2693951C1 |
| GAS-TURBINE ENGINE WITH TURBOCOOLER AT INLET | 2003 |
|
RU2239080C1 |
| COMBINED POWER PLANT OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2020 |
|
RU2758744C1 |
| HYBRID ROCKET TURBINE ENGINE | 1992 |
|
RU2106511C1 |
| TURBORAM AIR-JET ENGINE | 2015 |
|
RU2613755C1 |
| HYPERSONIC TURBO EJECTOR ENGINE | 2009 |
|
RU2386829C1 |
| METHOD AND AIR VEHICLE FOR MOVING IN PLANETARY ATMOSPHERE WITH SPEEDS ABOVE THE FIRST SPACE AND HIGHLY INTEGRATED HYPERSONIC VEHICLE APPARATUS (VERSIONS) FOR IMPLEMENTATION OF THE METHOD | 2012 |
|
RU2618831C2 |
| VORTEX GAS COMPRESSOR DEVICE FOR COMBINED AIR-JET ENGINE | 2019 |
|
RU2766496C2 |
| COMBINED CYCLE SYSTEM INTERACTING COMBUSTION CHAMBER AND NOZZLE | 2007 |
|
RU2413859C2 |
