FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering. Aircraft with variable geometry of the wings comprises a fuselage and wings arranged symmetrically to the longitudinal axis of the fuselage, each of which consists of a fixed on the fuselage base and pivotally mounted on the base with the ability to turn the console. Bases of the wings are fixed on the fuselage hingedly with the possibility of turning. Consoles are mounted on the bases with the possibility of turning with respect to the bases, with the axes of rotation of the consoles in the plane of the wing and placed at an angle to the axis of rotation of the bases. Bases and consoles are pivotally connected to rods hinged with their control devices placed in the fuselage. Axis of rotation of the bases is at an angle to the longitudinal axis of the fuselage. Rotating on their axes, the bases and consoles are controlled by rods pivotally connected to control devices.
EFFECT: invention is aimed at improving performance.
3 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WITH OSCILLATING SLATS | 2010 |
|
RU2457154C2 |
| AIRCRAFT | 2008 |
|
RU2466907C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| VERTICAL TAKEOFF AND LANDING FLYING VEHICLE | 2003 |
|
RU2244661C2 |
| AIRCRAFT | 2008 |
|
RU2438926C1 |
| AIRCRAFT | 2014 |
|
RU2577824C1 |
| LIGHT FLYING VEHICLE | 1995 |
|
RU2082651C1 |
| AIRCRAFT WING FAN-TYPE FLAP DRIVE | 2014 |
|
RU2539018C1 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| MULTI-PURPOSE HEAVIER-THAN-AIR FLYING VEHICLE | 2003 |
|
RU2230688C1 |
