FIELD: heavier-than-air flying vehicles. SUBSTANCE: flying vehicle includes main rotor rotated by counter-flow air, platform, drive made in form of internal-combustion gas turbine mounted on shaft together with two air turbines mounted under platform symmetrically relative to air propulsive jet nozzles. Provision is made for change of direction of air flow from nozzles. EFFECT: enhanced maneuverability. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
| INTERNAL-COMBUSTION GAS ENGINE | 1996 |
|
RU2116480C1 |
| AIRCRAFT WITH SHORT OR VERTICAL TAKE-OFF AND LANDING WITH HYBRID POWER PLANT | 2019 |
|
RU2729750C1 |
| COMBINATION BLADE OF FLYING VEHICLE MAIN ROTOR AND METHOD OF FLIGHT OF FLYING VEHICLE | 1998 |
|
RU2149799C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2698497C1 |
| HELICOPTER | 2018 |
|
RU2701083C1 |
| HELICOPTER | 2018 |
|
RU2710839C1 |
| JET ENGINE | 1997 |
|
RU2157907C2 |
| HELICOPTER | 2018 |
|
RU2701076C1 |
| COMPENSATION FOR REACTIVE MOMENT OF ROTOR | 2012 |
|
RU2514010C1 |
