A slat support assembly 20 is disclosed. It comprises a slat support arm 22 which is movable to deploy a slat from a leading edge of an aircraft wing about an axis of rotation of the arm and a slat mount 27, 28 on a slat which is coupled to one end of said slat support arm by a joint 29, 32, 33. The joint is configured to allow the slat mount to slide in a direction of the axis of rotation of the arm.
A slat support assembly
Slatstützanordnung
Ensemble de support d'hypersustentateur de borde d'attaque
2021-04-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |