FIELD: aircrafts.
SUBSTANCE: invention relates to instrumentation and can be used on aircraft (AC) for processing, storing, displaying and transmitting flight information to ground control points. The system contains an AC data registration subsystem, an information retrieval unit, a unit for accumulating and processing diagnostic information of the state of AC elements and assemblies, a unit for diagnosing the physical state of a pilot, a unit for preparing flight information for transmission to ground control points, a device for measuring rotor blades inconsistency, a device for dynamic balancing of the main rotor, a device for indicating flow stall on the rotor blades and a device for monitoring the approach to the "vortex ring" mode and a warning subsystem for the "helicopter pick-up" mode.
EFFECT: improving the safety and reliability of the system's operation as part of aircraft, especially helicopters.
1 cl, 1 dwg
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Authors
Dates
2021-12-21—Published
2021-06-11—Filed