A system for operating a droop panel on an air vehicle, the droop panel positioned between a fixed structure and a trailing edge flap on the wing. The system includes a pin joint linkage assembly coupled between and to the fixed structure, the droop panel, and the trailing edge flap. The assembly has a first link attached to the fixed structure; and a second link coupled to the first link, and pivotably connected to a third pin joint, connected to a fourth pin joint, and an angled portion pivotably connected to a second pin joint. The assembly has a third link coupled to the second link, and coupled to the fourth pin joint and to a fifth pin joint attached to the trailing edge flap. The assembly is configured to operate the droop panel by concurrently moving the droop panel and the trailing edge flap in a single coordinated motion.


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    Titel :

    SYSTEM AND METHOD FOR OPERATING A DROOP PANEL USING A PIN JOINT LINKAGE ASSEMBLY


    Beteiligte:
    TSAI KEVIN R (Autor:in)

    Erscheinungsdatum :

    2016-09-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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