| 摘要 |
An electrical connector for providing electrical communication between a fixed structure of an aircraft and a movable component mechanically connected to the fixed structure, wherein the electrical connector is arranged to be mechanically connected to the fixed structure at a first end of the connector and is arranged to be mechanically connected to the movable component at a second end of the connector, the electrical connector comprising a first telescopic element, at least a portion of which is electrically conductive and which is arranged to provide a first current path between the fixed structure and the movable component. |
