FIELD: aeronautical and space engineering. SUBSTANCE: flying vehicle includes case 1, jet engines 2, engine and wing position control actuator and control system. Jet engines are mounted on panels 3 and have horizontal and vertical axes of rotation 6. Jet engines 2 are mounted for rotation through 360 deg. Flying vehicle is provided with wings 7 mounted on panels. Wings may rotate through 360 deg irrespective of jet engines. EFFECT: possibility of performing flight with fin forwards. 2 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| THREE-MEDIUM VEHICLE | 2020 |
|
RU2743310C1 |
| FIFTEEN-SEAT THREE-MEDIUM VEHICLE | 2022 |
|
RU2791582C1 |
| TRANSFORMABLE AMPHIBIAN AIRCRAFT OF VERTICAL TAKE-OFF AND LANDING | 2017 |
|
RU2662311C1 |
| TRAIN POWERED FROM TROLLEY (VERSIONS) | 2018 |
|
RU2692345C1 |
| VTOL PASSENGER AIRCRAFT | 2023 |
|
RU2818261C1 |
| CONVERTIPLANE | 2017 |
|
RU2657706C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| CONVERTIPLANE WITH ROTORS JET DRIVE CONTROLLED BY ROTORS VIA WOBBLE PLATE AND CONTROL LEVERS WITH NO EXTRA CONTROL MEANS | 2013 |
|
RU2570241C2 |
| CONVERTER PLANE | 2011 |
|
RU2456208C1 |
| HOVERCRAFT WITH PROPULSION SYSTEM MADE AS PER MULTICOPTER SCHEME | 2023 |
|
RU2833275C1 |
