AIRCRAFT ELECTRICAL ARCHITECTURE Russian patent published in 2025 - IPC B64D31/00 H02J4/00 H02M9/00 B64D41/00 

FIELD: electricity.

SUBSTANCE: invention relates to improvement of aircraft electrical architecture. Aircraft electrical architecture comprises a plurality of primary generators (GEN1, GEN2), each of which is connected to the aircraft traction engine, a plurality of primary electrical networks (AC1, AC2, Essential AC), each of which is connected to a primary generator in normal operation, a single-component secondary electrical network (RES) operating in a certain voltage range, electric power accumulation device (BAT-HVDC) connected directly to the secondary network, two electric power converters (CP1, CP2), wherein CP1 is designed to supply power to the BAT-HVDC device in normal operation, and CP2, located between RES and AC2, provides transfer of energy in normal operation from the secondary electrical network to the second of the primary electrical networks, wherein BAT-HVDC and CP2 are configured to supply AC2 with power equal to at least half the rated power of one of the primary generators (GEN1, GEN2).

EFFECT: possibility of receiving energy from any devices, possibility of temporary storage of energy, including due to excess power, supply of electric energy to the primary network during consumption peaks.

12 cl, 4 dwg