A galley insert system for an aircraft galley comprises a galley support structure (12; 52), a galley insert (10; 50) configured to be coupled to the support structure (12; 52), and a latch mechanism (14; 54) for coupling the insert (10; 50) to the support structure (12; 52), the latch mechanism (14; 54) configured to automatically engage to couple the insert (10; 50) to the support structure (12; 52) when the insert (10; 50) is moved into a latching position on the support structure (12; 52), wherein the latch mechanism (14; 54) comprises a control mechanism (28; 90) configured to be actuated to disengage the latch mechanism (14; 54).


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    Title :

    GALLEY INSERT SYSTEM


    Additional title:

    KOMBÜSENEINSATZSYSTEM
    SYSTÈME D'INSERTION DE CUISINE



    Publication date :

    2024-01-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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