WIRELESS ELECTRONIC SYSTEM OF CONTROL AND DIAGNOSTICS OF AIRCRAFT GAS TURBINE ENGINE Russian patent published in 2017 - IPC F02C9/28 

FIELD: engines and pumps.

SUBSTANCE: system is equipped with an energy radiator, a set of energy receivers, an input device, an interference analyzer, a band-elimination filter, a subtracter, a storage, where the digital control unit is connected to the storage, the data receiving and scheduling radio module is connected to the subtractor, the outputs of a set of wireless smart sensors of the aircraft engine performance are connected via radio channels to the input of the input device, which is connected to the inputs of the interference analyzer and the band-elimination filter, the output of the interference analyzer is connected to the second input of the band-elimination filter, the output of which is connected to the input of the substracter, the output of which is connected to the input of the data receiving and scheduling radio module, and the second input of the subtracter is connected to the storage output, the input of which is connected to one of the outputs of the digital control unit, the other output of which is connected to the energy radiator which is through a radio channel is associated with a set of energy receivers, the outputs of which are connected to the inputs of a set of wireless smart sensors of aircraft engine performance.

EFFECT: increase of reliability and noise immunity of the electronic monitoring and diagnostic system, increase in the overhaul life of the system components.

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