An apparatus and method for supporting a load is provided. The apparatus comprises a structure (407) having an inner surface (470) with a shape configured to substantially conform to an outer surface (452) of a stringer (304). A number of pins (420) extend from the inner surface of the structure such that the number of pins are configured to engage holes (457) in the outer surface of the stringer when the structure is placed over the outer surface of the stringer. The pins support the structure with respect to the stringer when a load is applied to the structure. The structure comprises a number of members (411, 413) fixed with regard to each other by means of a flange (430) configured to support a hanger (440) for the load.


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    Titel :

    Clip attachment system connecting aircraft structures to each other


    Weitere Titelangaben:

    Klemmenbefestigungssystem zum Verbinden von Flugzeugstrukturen miteinander
    Système de fixation de pinces connectant des structures d'avions entre elles


    Beteiligte:

    Erscheinungsdatum :

    2017-11-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen



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