An aircraft stowage unit 200 configured to provide a footwell 202 for an adjacent seating unit 201. The stowage unit may comprise an upper section (301,fig3) and a lower(302,fig3) section, the lower section may be configured to provide the footwell for the adjacent seating unit. The aircraft stowage unit may be a galley unit and may comprise a heated unit or a refrigerated unit (405,fig4). The length of the stowage unit in the direction parallel to the longitudinal axis of the aircraft may be less than 70cm. The seat may recline into a bed. The seat may be positioned less than 90 degrees to a front surface 203 of the stowage unit, and less than 90 degrees to the longitudinal axis of the aircraft. The stowage unit may be a first stowage unit, there may be a second stowage unit where the distance between the front surface of the first stowage unit and the back surface 602 of the second stowage unit is less than 260 degrees.


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    Titel :

    Aircraft stowage unit


    Beteiligte:
    ROSS BURNS (Autor:in) / ANDREW JACOBS (Autor:in) / HELENA TEICHRIB (Autor:in)

    Erscheinungsdatum :

    19.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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