FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to vertical takeoff and landing gear. VTOL (vertical takeoff and landing aircraft) – "flying motorcycle" consists of housing (1) in form of hollow cylinder located vertically, power plant (2) resting on four-wheeled chassis (3), two coaxial vertical-axial rotors (4) and (5), on which are fixed replaceable weights (13) and blades (6), swash plate (7). Top platform (8) forms cockpit of pilot (9) containing control systems of aircraft (10), pilot seat (11) and parachute rescue system (12).
EFFECT: higher stabilization of aircraft and pilot safety level.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROTORCYCLE VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2019 |
|
RU2725833C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2017 |
|
RU2664851C1 |
| VERTICAL TAKE-OFF AND LANDING | 2016 |
|
RU2634469C2 |
| SMALL-SIZED VERTICAL TAKE-OFF/LANDING AIRCRAFT WITH AN INCREASED FLIGHT DISTANCE | 2017 |
|
RU2681464C1 |
| VERTICAL TAKE-OFF AND LANDING SEAPLANE WITH A MAIN ROTOR WITH FOLDING RETRACTABLE BLADES | 2021 |
|
RU2781817C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| TRANSFORMING HYBRID VEHICLE | 2018 |
|
RU2692311C1 |
| AIRCRAFT SINGLE-WING PROPULSOR | 2019 |
|
RU2735442C1 |
| FLYING VEHICLE | 0 |
|
SU1827363A1 |
| HYBRID AERONAUTICAL VEHICLE | 2018 |
|
RU2752039C2 |
