An aircraft galley configuration extending along a longitudinal axis of a fuselage of an aircraft and on one side of the aircraft includes a forward end of the galley closest to the front of the aircraft and a rear end of the galley on an opposite longitudinal end of the galley and closest to a passenger section of the aircraft, and a plurality of galley modules disposed in the galley between the forward and rear ends of the galley. The galley modules comprise a storage module, a heating module, a preparation module, and a service module. The storage module is disposed at the forward end of the galley and the service module is disposed at the rear end of the galley. An efficient work flow in the direction of the passenger section is created by the galley configuration.


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    Titel :

    AIRCRAFT GALLEY CONFIGURATION


    Weitere Titelangaben:

    CONFIGURATION D'OFFICE D'AERONEF


    Beteiligte:
    MIRON BRUNO (Autor:in) / TREMBLAY MICHEL (Autor:in) / LADD GRADYN (Autor:in) / TREMBLAY BENJAMIN (Autor:in)

    Erscheinungsdatum :

    29.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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