A slat support assembly is disclosed. It comprises a slat support arm 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 on a slat which is coupled to one end of said slat support arm by a joint. The joint is configured to allow the slat mount to slide in a direction of the axis of rotation of the arm.
Slat support assembly
29.03.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |