To provide a joining structure of a door panel for a lavatory of an aircraft lavatory unit, which is advantageous in preventing rattling of a door panel and deterioration in design. By alternately arranging a plurality of structural frame side hinge portions (34) and a plurality of door panel side hinge portions (48) in an vertical direction, a plurality of pairs of end surfaces (38, 54) of a structural frame side hinge portion end surface (38) and a door panel side hinge portion end surface (54) facing each other in the vertical direction are provided at intervals in the vertical direction. Bearing members (24) each formed in a cylindrical shape and including a shaft insertion hole (2402) are disposed between at least two pairs of end surfaces (38, 54) adjacent to each other in the vertical direction, of the plurality of pairs of end surfaces (38, 54). Both surfaces of the bearing member (24) are in contact with each of the two pairs of end surfaces (38, 54).


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    Title :

    JOINT STRUCTURE FOR BATHROOM DOOR BODY OF AIRPLANE BATHROOM UNIT


    Additional title:

    GELENKSTRUKTUR FÜR TOILETTENTÜRKÖRPER EINER FLUGZEUGTOILETTENEINHEIT
    STRUCTURE DE JOINT D'ÉTANCHÉITÉ POUR CORPS DE PORTE DE SALLE DE BAINS D'UNE UNITÉ DE SALLE DE BAINS D'AVION


    Contributors:

    Publication date :

    2022-12-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    E05D Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel , HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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