The invention relates to a cooling assembly (15) including: a conduit (16) including a side wall (17) and a fan (20) comprising: a rotating electric machine (32) a power supply module (35) including: three distinct single-phase self-transformers (79a, 79b, 79c) and magnetically decoupled, each self-transformer (79a, 79b, 79c) surrounding the side wall (17) of the conduit (16).
ENSEMBLE DE REFROIDISSEMENT POUR AERONEF
2016-09-08
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern |
CIRCUIT DE REFROIDISSEMENT POUR AERONEF ET PROCEDE DE PROTECTION DU CIRCUIT DE REFROIDISSEMENT
Europäisches Patentamt | 2023
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