FIELD: aircraft engineering.
SUBSTANCE: flap extension device comprises a bracket fixed on the fuselage, a movable link connected to the bracket by a hinge to form a kinematic axis of rotation of the flap and directly connected to the flap by means of two hinged joints. Flap extension device also includes a drive lever pivotally connected to the movable link by means of a push rod. Bracket is attached directly to the fuselage at two points.
EFFECT: reduction of dimensions of installation zone of flap extension mechanism due to kinematic simplicity of the mechanism, namely arrangement on movable link of hinged joint of rod-pusher coming from rocker (lever) connected to reduction gear.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT WING FLAP SUSPENSION SYSTEM | 2023 |
|
RU2819458C1 |
| FLAP EXTENDING UNIT | 2001 |
|
RU2214347C2 |
| FLAP EXTENSION DEVICE | 2015 |
|
RU2583239C1 |
| FLAP FOR SHORT TAKEOFF AND LANDING AIRCRAFT | 2013 |
|
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| SLIT FLAP FOR SHORT TAKEOFF AND LANDING AIRCRAFT | 2017 |
|
RU2679746C1 |
| AIRPLANE WING FLAP CONTROL DEVICE | 2021 |
|
RU2764335C1 |
| AIRCRAFT WING FAN-TYPE FLAP DRIVE | 2014 |
|
RU2539018C1 |
| THREE-SLOT AIRCRAFT FLAP OF THE SHORT TAKE-OFF AND LANDING | 2017 |
|
RU2684206C1 |
| SLOTTED FLAP | 2003 |
|
RU2261821C2 |
| VTOL AIRCRAFT WING | 2008 |
|
RU2385261C1 |
