FIELD: control and diagnostic equipment.
SUBSTANCE: invention relates to monitoring and diagnostic equipment and can be used for ground monitoring of state of aviation gas turbine engines within aircraft, as well as helicopter engines, unmanned aerial vehicles. Device is equipped with hardware access key and carrier-block versions of on-board control and diagnostic software connected to inputs of operational control unit, as well as by adapter of bus – loader, its input connected through hardware-software interface with operational control unit, while operational control unit via hardware-software interface and output of bus-adapter unit through connector are able to connect to system digital bus of control and registration units of engine parameters.
EFFECT: expand of device functionality and increase in reliability of diagnosis.
1 cl, 1 dwg
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Authors
Dates
2018-05-11—Published
2017-08-31—Filed