FIELD: transportation.
SUBSTANCE: flying vehicle comprises body, fuel tank and instrumentation module, gas-turbine engine comprising compressor, turbine, multi-section combustion chamber equipped with fuel systems comprising fuel flow controllers for every section. Inside jet nozzle there might be emergency landing engine installed.
EFFECT: improved flight characteristics of engine capacity, maneuverability and safety of flying vehicle.
3 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRBORNE VEHICLE OF "FLYING SAUCER" TYPE | 2011 |
|
RU2471676C1 |
| FLAYING SAUCER-TYPE AIRCRAFT | 2011 |
|
RU2475417C1 |
| AIRCRAFT | 2011 |
|
RU2470834C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2698497C1 |
| HELICOPTER | 2018 |
|
RU2710839C1 |
| HELICOPTER | 2018 |
|
RU2701083C1 |
| HELICOPTER POWER PLANT | 2019 |
|
RU2705857C1 |
| HYDROGEN AIR-JET ENGINE | 2014 |
|
RU2553052C1 |
| HELICOPTER | 2018 |
|
RU2701076C1 |
| DOUBLE-FUEL AIR-JET ENGINE | 2014 |
|
RU2561773C1 |
