FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to VTOL aircraft load bearing systems. VTOL aircraft wing comprises stiff sliding panels installed at upper part, slotted flaps wit carriages and support rollers, flap driving guide rails and IN/OUT drives. Note here that sliding panels are articulated via folding links with deflector board sliding in the flap main link head part. Top link of folding link is articulated with flap IN/OUT drive.
EFFECT: higher efficiency of proposed wing at takeoff and landing.
8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLAP FOR SHORT TAKEOFF AND LANDING AIRCRAFT | 2013 |
|
RU2549593C2 |
| THREE-SLOT AIRCRAFT FLAP OF THE SHORT TAKE-OFF AND LANDING | 2017 |
|
RU2684206C1 |
| SLIT FLAP FOR SHORT TAKEOFF AND LANDING AIRCRAFT | 2017 |
|
RU2679746C1 |
| VTOL AIRCRAFT WING | 2008 |
|
RU2385261C1 |
| SLOTTED FLAP | 2003 |
|
RU2261821C2 |
| AIRPLANE WING FLAP CONTROL DEVICE | 2021 |
|
RU2764335C1 |
| VTOL AIRCRAFT LIFT INCREASING DEVICE | 2013 |
|
RU2561886C2 |
| AIRCRAFT WING FAN-TYPE FLAP DRIVE | 2014 |
|
RU2539018C1 |
| WING LEADING EDGE FLAP UNIT | 1996 |
|
RU2181332C2 |
| DEVICE FOR CONTROLLING FLAPS | 1988 |
|
SU1804039A1 |
