The invention relates to an aircraft electrical power supply network architecture, comprising at least one compressor motor (116a, 116b) for the aircraft's air conditioning plant and at least two electrical generators (112a, 112b) of the aircraft. The architecture is characterized in that each compressor motor (116a, 116b) comprises at least two independent coils (126a, 128a, 126b, 128b), and a first of said coils (126a, 126b) of each compressor motor (116a, 16b) is linked, via a first power supply line, to one of the electrical generators (112a, 112b) and a second of said coils (128a, 128b) of each compressor motor (116a, 116b) is linked, via a second power supply line, to an electrical generator (112a, 112b) different from the electrical generator to which the first coil (126a, 126b) is linked.
ARCHITECTURE DE RÉSEAU D'ALIMENTATION ÉLECTRIQUE
POWER SUPPLY NETWORK ARCHITECTURE
ENERGIEVERSORGUNGSNETZARCHITEKTUR
2020-06-24
Patent
Electronic Resource
French
IPC: | H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern |
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