| 摘要 |
The invention relates to a control and energy supply system for the drive units and control units for at least two, preferably adjacent, aircraft seats, whereby all system components are connected by means of a data bus, such that the control system of the one seat is informed of what is happening to the other seat. The adjuster motors of the seats are supplied with electricity by means of two distinct networks. System breakdowns caused by loose or disconnected connectors, broken cables, short circuits and faulty controllers are thus avoided by said redundancy concept. |
