FIELD: instrument making.
SUBSTANCE: airborne electronic system of aircraft includes at least two instruments provided with possibility of information exchange at least by means of one bidirectional synchronous communication electric bus in which information exchange between instruments is performed by means of optic bus having the possibility of being connected to electric interfaces of the above instruments. Optic bus of airborne electronic system includes at least one optic cable containing at least one optic fibre and containing the connector on each end; at that, the above connector contains conversion device of electric signals to optic signals and conversion devices of optic signals to electric signals.
EFFECT: enlarging functional capabilities.
13 cl, 5 dwg
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