An aircraft interior assembly comprising a fixed element, a sliding element movable between a lockable position and a released position, and a latch mechanism. The latch mechanism comprises a locking arm, mounted on one of the fixed element and the sliding element, which is rotatable around a rotating axis between a locked position and an unlocked position. The latch mechanism further comprises an engagement plate, mounted on the other of the fixed element and the sliding element. When the sliding element is in the lockable position and the locking arm is in the locked position, the locking arm contacts the engagement plate to prevent the sliding element moving out of the lockable position. Conversely, when the sliding element is in the lockable position and the locking arm is in the unlocked position, the locking arm is not in contact with the engagement plate, and the sliding element is free to move out of the lockable position.


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    Title :

    AIRCRAFT INTERIOR ASSEMBLY


    Additional title:

    FLUGZEUGINNENEINRICHTUNG
    ENSEMBLE INTÉRIEUR D'AÉRONEF


    Contributors:

    Publication date :

    2024-07-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    E05B LOCKS , Schlösser / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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