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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CONNECTING ARRANGEMENT AND METHOD FOR PROVIDING SUCH CONNECTING ARRANGEMENT


    Weitere Titelangaben:

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


    Beteiligte:
    SCHOMAKER RALF (Autor:in) / KNICKREHM BJOERN (Autor:in)

    Erscheinungsdatum :

    02.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




    Connecting arrangement

    HAEGELE KLAUS / HEISE WILFRIED / SALKIC ASMIR et al. | Europäisches Patentamt | 2017

    Freier Zugriff


    Vehicle ceiling connecting arrangement

    CREET ROBERT / MJÖRNESTÅL NICLAS / LARSSON HANS et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    VEHICLE CEILING CONNECTING ARRANGEMENT

    CREET ROBERT / MJÖRNESTÅL NICLAS / LARSSON HANS et al. | Europäisches Patentamt | 2019

    Freier Zugriff