Scalable freight loading system, especially for an aircraft
The invention relates to a scalable freight loading system, especially for an aircraft, said system comprising drive means (L 1 -L 9 , R 1 -R 9 ), covering sensors, bolts, proximity switches (PL 1 -PL 9 , PR 1 -PR 9 ), and a central control device (CCB). According to the invention, the loading surface is divided into sectors (S 1 , S 2 , S 3 ); a local control unit (SCB 1 , SCB 2 , SCB 3 ) is associated with each sector; the drive means, covering sensors, and proximity switches of a sector are connected to IO ports of the local control unit; and the local control units are connected to the central control unit by means of a bus system (CAN-Bus).
1. A scalable freight loading system, comprising:
power drive units, covering sensors, locking bars, proximity switches and a central control unit, a loading surface includes sectors, local control units each having I/O ports, wherein one of the local control units is assigned to one respective sector; wherein of the local control units, the power drive units, the covering sensors and the proximity switches of a sector are solely connected to the I/O ports of the local control unit for the respective sector; and the local control units are connected via a bus system to the central control unit.
2. The freight loading system according to claim 1 , wherein the local control units include a means for storing the statuses of all the sectors.
3. The freight loading system according to claim 1 , wherein the power drive units comprise floor conveyors.
4. The freight loading system according to claim 1 , wherein the bus system comprises a CAN bus.
5. A method for operating a scalable freight loading system according to claim 1 , wherein the local control units use the bus system in order to transmit the status of the power drive units, the covering sensors and the proximity switches.
6. The method according to claim 5 , wherein the respective local control unit transmits the sector status at the start-up of the freight loading system and/or in the event of a change in the sector status.
7. The method according to claim 5 , wherein the sector status is transmitted has a standardized status object of the CAN bus.
8. The method according to claim 5 , wherein the power drive unit which is not covered by a freight item is activated if it is arranged behind another power drive unit covered by the freight item, as seen in transporting direction.
9. The method according to claim 5 , further comprising:
determining when the locking bar is raised; and
further comprising the step of not activating the power drive unit for the locking bar that is raised.