A device for securing passenger seat frame structures (e.g., seat spreaders, legs) to a lateral crossbeam (130) includes a wedged clamping device (204) insertable into a pocket (308) directly adjacent to a passage allowing the crossbeam to pass through the seat frame structure. The wedged clamping device has an upper face providing a locking taper angle and a lower arcuate face opposite the upper face and in contact with the crossbeam. When inserted into the pocket, the wedged clamping device provides a clamping force securing the seat frame structure to the crossbeam without driving a bolt through, deforming, or otherwise compromising the integrity of the crossbeam. The wedged clamping device accepts a tuning bolt through a lateral face; tightening the tuning bolt can more precisely control the amount of clamping force provided on the crossbeam.


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    Titel :

    WEDGED CLAMPING DEVICE AND METHOD FOR AIRCRAFT SEAT FRAME


    Weitere Titelangaben:

    KLEMMKEILVORRICHTUNG UND -VERFAHREN FÜR EINEN FLUGZEUGSITZRAHMEN
    DISPOSITIF DE SERRAGE À COIN ET PROCÉDÉ POUR CADRE DE SIÈGE D'AÉRONEF


    Beteiligte:
    RALPH NEIL M (Autor:in) / SUHRE RYAN J (Autor:in) / PUGLISI STEPHEN A (Autor:in) / MCKEE ERIC M (Autor:in)

    Erscheinungsdatum :

    2023-10-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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