FIELD: transport.
SUBSTANCE: invention relates to device for electronic digital control system FADEC comprising, at least, one avionics component 300, one engine interface 310, and, at least, one engine controller 315 arranged inside or nearby aircraft engine 320. At least, one said engine interface 310 allows data exchange between said avionics component 300 and engine controller 315. Engine interface 320 represents a universal hardware and may be connected to various engine controllers 315 to be installed onboard aircraft. Said engine interface is characteristic of one type of aircraft engine. Proposed device allows distributing the functions executed in FADEC systems between avionics components and FADEC system and simplification FADEC systems and their software.
EFFECT: centralised data exchange.
18 cl, 4 dwg
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