Actuation assembly for a trailing edge flap of an aircraft wing, comprising: a base unit configured to be fixated to a main body of the aircraft wing; an intermediate unit movably connected to the base unit and configured to be hingeably connected to the flap at a leading edge of the flap about a first hinging axis extending along the leading edge of the flap, wherein the movability provides adjustability of the flap between a retracted flap position and an extended flap position; and a second actuator configured to controllably rotate the flap with respect to the intermediate unit about the first hinging axis, the second actuator being configured to be movable along with the intermediate unit with respect to the at least one base unit.
ACTUATION ASSEMBLY FOR A TRAILING EDGE FLAP OF AN AIRCRAFT WING
BETÄTIGUNGSANORDNUNG FÜR EINE HINTERKANTENKLAPPE EINES FLUGZEUGFLÜGELS
ENSEMBLE D'ACTIONNEMENT POUR VOLET DE BORD DE FUITE D'UNE AILE D'AÉRONEF
13.08.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ACTUATION ASSEMBLY FOR A TRAILING EDGE FLAP OF AN AIRCRAFT WING
Europäisches Patentamt | 2025
|Actuation assembly for a trailing edge flap of an aircraft wing
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2023
|Sub-wing mounted trailing edge double fold flap for aircraft wing
Europäisches Patentamt | 2024
|