Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a trailing edge high lift assembly (9) movably arranged at a trailing edge of the main wing (5), the trailing edge high lift assembly (9) comprising a flap (11) and a connection assembly (13) movably mounting the flap (11) to the main wing (5), such that the flap (11) is movable between a retracted position (15) and at least one extended position (17), wherein the connection assembly (13) comprises an actuator unit (21) for moving the flap (11) between the retracted position (15) and the at least one extended position (17), wherein the flap comprises a leading edge part (23) and a trailing edge part (27) mounted to the leading edge part (23) in a manner pivotable about a pivot axis (31). The object to provide a wing having a trailing edge high lift assembly with a simplified actuation concept, is achieved in that the actuator unit (21) is coupled to the leading edge part (23) via a first linkage (35) and is coupled to the trailing edge part (27) via a second linkage (37), and in that the actuator unit (21) is configured to move both the leading edge part (23) via the first linkage (35) and the trailing edge part (27) via the second linkage (37).
WING FOR AN AIRCRAFT
FLÜGEL FÜR EIN FLUGZEUG
AILE D'AÉRONEF
2023-10-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT WING TORSION BOX, AIRCRAFT WING AND AIRCRAFT
Europäisches Patentamt | 2019
|Aircraft wing and an aircraft comprising such aircraft wing
Europäisches Patentamt | 2017
|AIRCRAFT WING AND AN AIRCRAFT COMPRISING SUCH AIRCRAFT WING
Europäisches Patentamt | 2015
|