| 摘要 |
The present invention relates to an internal link for aircraft having at least a first pylon which is intended for a load and provided with signal cabling, intended for e.g. countermeasure pods, and power supply, and at least a second pylon which is intended for a load and provided with power supply, but which has no corresponding signal cabling. Signals to the load of the second pylon are sent via the signal cabling to first signal conversion equipment in connection with the first pylon and are sent through an antenna to second signal conversion equipment in connection with the second pylon where it is converted into the signal that existed in the signal cabling. |
