Linkage assemblies for aircraft wing hinged panels are described herein. An example linkage assembly (300) includes a flap follower arm (312) coupled between a spoiler support beam (302) and a flap (202), a rocker (340), a panel link (338) coupled between the hinged panel and the rocker, and a cross-bar link (342) coupled between the flap follower arm and the rocker. The flap follower arm, the rocker, the panel link, and the cross-bar link are configured to coordinate adjustment of positions of the hinged panel and the flap relative to each other.
LINKAGE ASSEMBLIES FOR AIRCRAFT WING HINGED PANELS
GESTÄNGEANORDNUNGEN FÜR SCHARNIERTE FLUGZEUGFLÜGELPLATTEN
ENSEMBLES DE LIAISON POUR PANNEAUX ARTICULÉS D'AILE D'AÉRONEF
2023-05-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |