FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises aircraft general equipment (3), control station (2) with control means connected to data exchange system (4) incorporating first and second doubly reserved communication channels (5) and (6), respectively. These are composed by first and second cached channels (7) and (8), and second primary and second secondary data exchange channels (9, 10). First and second computer-concentrator units (11) and (12), first and second units (13) and (15) of DC supply protection and switching units, first and second AC supply protection and switching units (14, 16), first and second signal converters (17) and (18) are connected to the latter.
EFFECT: reliability and perfected control.
4 cl, 1 dwg
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Authors
Dates
2014-10-10—Published
2013-04-30—Filed