Bus system for an aircraft

Details Bus system for an aircraft Bus system for an aircraft

H - Electricity

04

L

H04L 12/40 (2006.01) H04L 12/413 (2006.01) H04L 29/02 (2006.01)

Patent

CA 2490561

The present invention relates to a bus system for transmitting a data packet between multiple devices in an aircraft, which is based on the CAN data bus system, but has an expanded identification field, in which a fixed region is designed for identification of the manifold aircraft systems, through which each aircraft system may be addressed uniquely. According to an exemplary embodiment, the data packet may be sent with different priorities, through which "important" data packets have priority on the transmission medium.

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