FIELD: transport.
SUBSTANCE: group of inventions relates to collapsible rear wing of a vehicle. Rear wing shape corresponds exactly to stylized surface of vehicle body in retracted position and can adaptively change its cross-section in extended position to form high-efficiency aerodynamic profile with built-in Gurney flap. Moreover, adaptive change of cross-section and extension of Gurney flap is provided by means of lever mechanism using drive mechanism of the main deployment system.
EFFECT: reduced aerodynamic resistance.
11 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WING TRAILING EDGE CONTROL SURFACE | 2006 |
|
RU2405715C2 |
| DEVICE AND METHOD TO DESCRIBE LIFT | 2006 |
|
RU2399553C2 |
| ROTARY ELEMENT TO INCREASE LIFT, PARTICULARLY, DEFLECTING WING TIP WITH HIGH AERODYNAMIC CHARACTERISTIC | 2006 |
|
RU2414386C2 |
| TRANSFORMING HYBRID VEHICLE | 2018 |
|
RU2692311C1 |
| AIRCRAFT WING | 2000 |
|
RU2222472C2 |
| REUSABLE MISSILE AND AIRCRAFT UNIT AND WAY TO RETURN IT TO SPACEPORT | 2010 |
|
RU2442727C1 |
| DEVICE FOR COMPLEX DISPLACEMENT | 2010 |
|
RU2575913C2 |
| DRIVE SYSTEM TO INCREASE LIFT AT WING LEADING EDGE | 2008 |
|
RU2478521C2 |
| SYSTEM PROVIDING HIGH LIFT AT AIRCRAFT AIRFOIL | 2008 |
|
RU2463211C2 |
| VTOL AIRCRAFT WING | 2008 |
|
RU2385261C1 |
