FIELD: engines and pumps.
SUBSTANCE: system is equipped with a set of wireless smart sensors of aircraft engine parametres, wireless control lever, wireless control and indication panel, radio module of information receiving and monitoring, information complexation assembly, computation unit of reference parametre value of aircraft engine, information state and substitution analyser, information transmission ratio module; at that, outputs of the set of wireless smart sensors of aircraft engine parametres, wireless control lever and wireless control and indication panel are connected via radio channels to inputs of radio module of information receiving and monitoring, which is connected to information complexation assembly, the output of which is connected to input of information state and substitution analyser, and the other output of information complexation assembly through computation unit of reference parametre values of aircraft engine is connected to the other input of information state and substitution analyser connected to digital control unit the output of which is connected to information transmission radio module connected via radio channel to wireless control and indication panel.
EFFECT: improving reliability of electronic control system, decreasing number and weight of cables and electrical connections, simplifying piping of gas turbine aircraft engine and decreasing costs for its maintenance.
2 dwg
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