FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft engine power plant systems. Aircraft with hybrid power supply consists of the following assemblies: external structure (fuselage, wings, etc), electrical equipment 34, internal combustion engine to develop thrust, engine power supply means as well as: multiple forward light power-to-electric power converters 24 arranged at the part of external structure outer surface, means 32 for comparison of electric power generated by transducers 24, excess electric power takeoff means 36, means 38 to supply extra power thrust by excess extra electric power, is available.
EFFECT: higher power output, fuel savings, increased flight range.
6 cl, 3 dwg
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