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
24.06.2020
Patent
Elektronische Ressource
Französisch
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 |
Procédé d’alimentation électrique d’un réseau électrique et architecture électrique
Europäisches Patentamt | 2021
|PROCEDE ET ARCHITECTURE D'ALIMENTATION ELECTRIQUE DE RESEAU DOMESTIQUE EMBARQUE
Europäisches Patentamt | 2018
|PROCÉDÉ ET ARCHITECTURE D'ALIMENTATION ÉLECTRIQUE DE RÉSEAU DOMESTIQUE EMBARQUÉ
Europäisches Patentamt | 2018
|