FIELD: electrical equipment of flying vehicles. SUBSTANCE: system includes transducers of rotational speeds of propeller and stator of electric generator, control units and fault detection units. Stator is divided into two parts: one part consists of permanent magnets of inductor poles; this part is freely revolving and may be fixed by means of braking clutch; second part is secured immovably and is provided with winding for check of faults in resistive thermal elements and electric generator windings. EFFECT: reduced mass of system. 1 dwg
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