FIELD: transport.
SUBSTANCE: invention relates to power engineering. Control system for aircraft driven by at least one engine installed in nacelle. Proposed system comprises: absolutely independent electronic control unit of jet engine operating conditions designed to control the conditions of at least one electrical device of the nacelle and to control said device directly. Note here that nacelle electric supply unit arranged outside aforesaid independent electronic control unit and designed to control the conditions of at least one electrical device of the nacelle. Invention covers also aircraft with above described control system.
EFFECT: decreased weight and sizes of said control system, lower servicing costs.
10 cl, 2 dwg
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