A fuselage is described that includes a plurality of frames and a plurality of seat rows spaced apart according to a seat pitch. Each frame includes a lateral floor beam, and each seat row of the plurality of seat rows includes a load-bearing structural base with a plurality of legs attached to a proximal lateral floor beam and a distal lateral floor beam. Each seat row also includes a seat or bank of seats attached to the load-bearing structural base, where the seat or bank of seats includes at least one seat bottom and at least one seat back. Further, each seat row includes an interface between (i) the load-bearing structural base and (ii) the seat or bank of seats to allow for attachment and detachment of the seat or bank of seats relative to the load-bearing structural base.


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    Title :

    INTEGRATED AIRCRAFT FUSELAGE AND LOAD-BEARING STRUCTURAL BASE FOR AIRCRAFT SEATS


    Additional title:

    INTEGRIERTER FLUGZEUGRUMPF UND LASTTRAGENDE STRUKTURBASIS FÜR FLUGZEUGSITZE
    FUSELAGE D'AÉRONEF INTÉGRÉ ET BASE STRUCTURALLE PORTEUSE DE CHARGE POUR SIÈGES D'AVION



    Publication date :

    2020-12-16


    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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