| 摘要 |
The invention concerns a connecting arrangement (14) for joining together at least two components (10, 12) to form a structural assembly (16), in particular in the region of a wing of an aircraft, wherein at least one component (10) is formed from a fibre composite plastic and at least one further component (12) is formed from a metal, or at least two components (10) are formed from a fibre composite plastic. In accordance with the invention a bushing (22) is secured in a through hole (20) through the components (10, 12), and a first end (26) of the bushing (22) is provided with a collar (30), which faces towards a lower face (32) of the structural assembly (16), and a second end (28) of the bushing (22) and a zone (34) of an upper face (36) of the structural assembly (16) radially surrounding this end (28) have a depression (38), and a connecting element (50) is installed in the bushing (22). By this means there ensues, inter alia, a smooth, aerodynamically beneficial configuration of the upper face (36), which can be provided with a coating without any problems, and which ensures a reliable electrical contact between the connecting element (50) and a conductive surface entity (18) of the first component (10). Furthermore the invention concerns a method, in particular for the purpose of manufacturing such a connecting arrangement (14). |
