| 摘要 |
The device (22) has an articulating arm (24) comprising two sections (30, 32) that are articulated with one another to swivel relative to each other around a clevis pin, where one of the sections is designed as a rod. A guiding unit (26) guides an electric cable (20) along the articulating arm and comprises a spiral coil (50) that is directed along a coil axis for winding the cable around the spiral coil. The spiral coil comprises a spacer element (60) to maintain successive windings of the cable around the coil axis at a distance from each other along the coil axis. An independent claim is also included for an aircraft. |
