A pipe support for supporting a pipe of an aircraft fuel system is disclosed. The pipe support has first and second parts which together form a collar to retain the pipe. The first and second parts of the pipe support are able to be moved relative to each other between an open condition, in which the pipe is insertable between the first and second parts, and a closed condition, in which the first and second parts are brought together to retain the pipe. The collar is locatable in an opening in a structural member, such as a wing rib. When the collar is located in the opening in the wing rib, the pipe support is restricted from moving from the closed condition.


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    Titel :

    PIPE SUPPORT


    Beteiligte:
    BONTE ERIC (Autor:in) / QUAYLE STUART (Autor:in) / BRYANT ANTHONY (Autor:in) / PEACHEY DANIEL (Autor:in)

    Erscheinungsdatum :

    05.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16L PIPES , Rohre / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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