An aircraft with hybrid thermal/electrical propulsion includes a turbomachine; a first electrical source; a second electrical source equipped with an electrical energy storage device; a non-propulsion electrical distribution network; a low-voltage electrical distribution network; and a propulsion electrical distribution network. The three electrical distribution networks are electrically supplied by the first and second electrical sources and electrically interconnected by static converters.
ELECTRIC ARCHITECTURE FOR HYBRID PROPULSION
2021-11-11
Patent
Electronic Resource
English
AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION
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