Frame of a fuselage section of an aircraft that receives external loads, such as the rear section that receives the loads of the tail planes, comprising a first sector (11) configured specifically to withstand these external loads and a second sector along the remaining perimeter of the fuselage, said first sector (11) comprising the following structural elements: a) a foot piece (21) to be joined to the fuselage skin (13); b) a head piece (23); c) a web (25) comprising one or more fitting-pieces (27, 27') for receiving said external loads and a plurality of X-shaped pieces (31) joined by its ends to said foot piece (21) and said head piece (23); d) two connecting pieces (39, 39') of the ends of said foot piece (21) and said head piece (23) with the second sector of the frame.


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    Titel :

    Highly loaded frame of an aircraft fuselage with a lattice structured web


    Weitere Titelangaben:

    Hochbelasteter Rahmen eines Flugzeugsrumpfes mit einer Gitterstrukturversteifung
    Cadre fortement chargé d'un fuselage d'avion doté d'un réseau structuré de treillis



    Erscheinungsdatum :

    2017-07-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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