An aircraft interior configuration includes a first passageway extending along a longitudinal axis of a fuselage of the aircraft and a second passageway extending along the longitudinal axis. A transitional region is disposed between the first passageway and the second passageway. The transitional region extends perpendicularly to the longitudinal axis, between starboard and port sides of the aircraft. The transitional region is configurable from at least a first configuration to at least a second configuration.


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    Titel :

    Aircraft interior configuration


    Beteiligte:

    Erscheinungsdatum :

    2019-05-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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