A connecting arrangement for joining at least two components to form a structural assembly, near a wing of an aircraft, wherein at least one component is formed from a fiber composite plastic and at least one further component is formed from either a metal or a fiber composite plastic. A bushing is secured in a hole through the components. The bushing includes a first end with a collar which faces towards a lower face of the structural assembly and a second end. A zone of an upper face of the structural assembly radially surrounds the second end and includes a depression. A connecting element is installed in the bushing. This provides a smooth, aerodynamically beneficial configuration of the upper face, which can be coated, and which ensures a reliable electrical contact between the connecting element and a conductive surface of the first component.


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    Title :

    CONNECTING ARRANGEMENT AND METHOD FOR PROVIDING SUCH CONNECTING ARRANGEMENT


    Additional title:

    VERBINDUNGSANORDNUNG UND VERFAHREN ZUM HERSTELLEN EINER SOLCHEN VERBINDUNGSANORDNUNG
    AGENCEMENT DE CONNEXION ET PROCÉDÉ POUR ÉTABLIR UN TEL AGENCEMENT DE CONNEXION


    Contributors:

    Publication date :

    2018-05-02


    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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