A system for adjusting a height of a ceiling panel in an aircraft and a corresponding method is disclosed. The system includes an arm and at least one ceiling support latch, wherein each of the at least one ceiling support latches is attached to the arm. The system further includes an adjustable fitting attached to the arm, wherein the adjustable fitting includes (i) a first sliding block attached to the arm, (ii) a second sliding block attached to a support structure, and (iii) an adjustment screw. Adjustment of the adjustment screw forces the first and second sliding blocks to move relative to one another.


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    Titel :

    Adjustable support structure for aircraft cabin ceiling


    Beteiligte:
    KING TIMOTHY TODD (Autor:in) / DAVIS KENNETH G (Autor:in) / THOMAS MATTHEW R (Autor:in) / NADVORNICK MARK J (Autor:in) / MCCUNE JAMES R (Autor:in) / MULLINS JASON W (Autor:in)

    Erscheinungsdatum :

    21.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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