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.
CONNECTING ARRANGEMENT AND METHOD FOR PROVIDING SUCH CONNECTING ARRANGEMENT
VERBINDUNGSANORDNUNG UND VERFAHREN ZUM HERSTELLEN EINER SOLCHEN VERBINDUNGSANORDNUNG
AGENCEMENT DE CONNEXION ET PROCÉDÉ POUR ÉTABLIR UN TEL AGENCEMENT DE CONNEXION
2018-05-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2023
|European Patent Office | 2024
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