FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed wing comprises element (1; 11) coupled with wing (2) and extending to form slot region (9) between wing (2) and element (1; 11), as well as separating surface (6; 7) arranged to displace, with element (1; 11) extended, into said slot region (9) and pass along flow interface line (13) located between region (12) of vortex flows and slot airflow (10) moving in slot region (9) between element (1; 11) and wing (2). Separating surface (6; 7) represents surface with n stable states moved between discrete positions by actuator (3; 3a, 3b; 4; 4a, 4b; 5; 5a, 5b).
EFFECT: simplified design.
32 cl, 15 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WING WITH EXTENDING SLAT | 2006 |
|
RU2397108C2 |
| SYSTEM PROVIDING HIGH LIFT FOR AIRCRAFT WITH MAIN WING AND REPOSITIONABLE WING SLAT | 2008 |
|
RU2483976C2 |
| DEVICE FOR REDUCING AERODYNAMIC NOISE ON PASSENGER AIRCRAFT SLAT | 2002 |
|
RU2296695C2 |
| AIRCRAFT MECHANISED WING | 2012 |
|
RU2502635C1 |
| RETRACTABLE TURBULENCE PROMOTER TO REDUCE STALL SPEED | 2012 |
|
RU2600014C2 |
| GROUND-EFFECT VEHICLE | 2019 |
|
RU2716303C1 |
| AIRCRAFT WING | 2017 |
|
RU2672234C1 |
| LEADING EDGE FLAP AND METHOD OF ITS FLOWING | 2010 |
|
RU2487051C2 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| WING OF AIRCRAFT WITH RETRACTING AIR SCREW | 2016 |
|
RU2637277C1 |
