FIELD: aviation.
SUBSTANCE: invention relates to aviation. Aircraft comprises fuselage, horizontal and vertical tail surfaces, power plant, preferably of two engines, sleek horizontal beams, chassis, propeller horizontal thrust, transmission and rotating in opposite directions around wings. Wings are able braking rotation of any of them. Each wing has radially disposed around perimeter of oscillating blades that make complete cycle of oscillation in vertical plane in one revolution of wing. In operation, blades in plane of blade oscillation may exclude oscillation of blades and set them in plane of fixed wing.
EFFECT: achieved by improving performance, reducing design complexity.
3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| "SAMPO 2" AIRCRAFT | 2016 |
|
RU2647294C2 |
| GYROPLANE | 2019 |
|
RU2730082C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| FLAPPING DIAPHRAGM-TYPE PROPULSOR (VERSIONS) AND FLAPPING AIRCRAFT ON ITS BASE | 1996 |
|
RU2123455C1 |
| UNMANNED HIGH-SPEED HELICOPTER-AIRPLANE | 2017 |
|
RU2653953C1 |
| HIGH-SPEED HELICOPTER-AMPHIBIOUS AIRCRAFT | 2017 |
|
RU2655249C1 |
| MULTIPURPOSE HELICOPTER AIRPLANE WITH REMOTE CONTROL | 2008 |
|
RU2370414C1 |
| CONVERTIPLANE | 2004 |
|
RU2282566C2 |
| CONVERTIPLANE | 2017 |
|
RU2657706C1 |
| HIGH-SPEED HYBRID ROTORCRAFT | 2017 |
|
RU2652868C1 |
