FIELD: electrical engineering.
SUBSTANCE: invention relates to electric engineering area, and can be used to control the electric power supply network of aircraft. Method and a system for supplying electrical energy to an aircraft that is equipped with a plurality of loads to be powered (C1-C4), and power supply system comprising a plurality of power sources (S1, S2, S3) and an on-board energy management module (MG). Energy management module (MG) is electrically connected to said power sources (S1, S2, S3) and to said loads to be powered (C1-C4). Energy management module (MG) controls the power supply to at least one of said loads (C1-C4) using at least two different power sources in parallel (S1, S2, S3) in the event of increased energy requirements, said load (C1-C4) initially being powered by single energy source (S1, S2, S3).
EFFECT: technical result constitutes lower power consumption, increase in efficiency.
10 cl, 2 dwg
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Authors
Dates
2018-03-23—Published
2014-01-20—Filed