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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    Title :

    Adjustable support structure for aircraft cabin ceiling


    Contributors:

    Publication date :

    2018-08-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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