FIELD: electrical engineering.
SUBSTANCE: invention relates to the field of electrical engineering, in particular, to aircraft. The described result is achieved by the aircraft containing one gas turbine engine, at least one first electricity source, at least one second electricity source equipped with means of electricity storage, a non-traction electrical distribution network, and a low-voltage electrical distribution network, while additionally containing a traction electrical distribution network, wherein all three distribution networks are powered by the first and second electricity sources and are mutually electrically connected via static converters.
EFFECT: ensured supply or selection of controlled power using one or multiple electric machines on high and low-pressure shafts.
15 cl, 1 dwg
