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.


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    Title :

    LINKAGE ASSEMBLIES FOR AIRCRAFT WING HINGED PANELS


    Additional title:

    GESTÄNGEANORDNUNGEN FÜR SCHARNIERTE FLUGZEUGFLÜGELPLATTEN
    ENSEMBLES DE LIAISON POUR PANNEAUX ARTICULÉS D'AILE D'AÉRONEF


    Contributors:

    Publication date :

    2023-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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