A transport element support assembly (300) comprises a front plate (302), a back plate (304), and a grommet (306). The front plate (302) has a first opening (310) and a first set of holes (313). The back plate (304) has a second opening (320) and a second set of holes (323). A chamber is formed by the first opening and the second opening and is configured to hold a transport element. The grommet (306) is positioned within the chamber. The transport element support assembly (300) formed by the front plate (302), the back plate (304), and the grommet (306) is configured to provide electrical isolation between the transport element and an aircraft structure.


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    Title :

    TRANSPORT ELEMENT SUPPORT ASSEMBLY


    Additional title:

    TRANSPORTELEMENTSTÜTZANORDNUNG
    ENSEMBLE DE SUPPORT D'ÉLÉMENT DE TRANSPORT



    Publication date :

    2022-04-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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