A panel assembly (200) for installation onto a track beam (202) including a beam flange (206) having a non-linear edge (208) is disclosed. The panel assembly (200) includes a panel (218) and a lockable catch (228) moveably connected to the panel (218). The lockable catch (228) includes a lockable mating edge (230) configured to selectively mate with the non-linear edge (208) of the beam flange (206) of the track beam (202). The lockable catch (228) also includes a lockable catch edge (232) extending beyond the lockable mating edge (230). The lockable catch (228) is moveable on a lower surface (222) of the panel (218) between an unlocked position and a locked position. In the unlocked position the lockable catch edge (232) is retracted. In the locked position, the lockable mating edge (230) mates with the non-linear edge (208) of the beam flange (206) and the lockable catch edge (232) retains the panel (218) on the track beam (202). (-218 29217->4 ,-./,-210 216Nj


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    Titel :

    Locking panel assembly


    Beteiligte:
    SCOTT STEVEN A (Autor:in) / OSBORNE JOHN C (Autor:in)

    Erscheinungsdatum :

    2021-12-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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