FIELD: electrical engineering.
SUBSTANCE: proposed is a method of supplying electricity to an electrical consumer (2) of an aircraft, wherein the method comprises the following stages: electrical energy is supplied to an electrical consumer (2) from a main source (1) generating electricity; an instantaneous parameter characterizing the main source (1) is measured; level of use of the main source (1) is determined based on the measured instantaneous parameter; voltage of the main source (1) is regulated depending on the level of use; voltage at the output of the main source (1) is measured; the measured voltage or level of use is compared with a predetermined threshold value (Vh); and electric power is supplied to the electric consumer (2) from an auxiliary source (3) storing electric power when the measured voltage is less than a predetermined threshold value to supply additional electric power to the electric consumer (2).
EFFECT: technical result is in optimized consumption of electricity supplied by hybrid sources in real time with limited complexity of implementation of such solution.
8 cl, 2 dwg
