A starting/generating system for an aircraft turbine engine, the starting/generating system comprising at least one brushless drive motor/generator, at least one control module and at least one power module, the power module being configured to supply/receive electric power from the brushless drive motor/generator, the control module being connected to the brushless drive motor/generator by a control cable in order to control its operation, in which system the power module is configured to be mounted in the housing of the non-pressurized zone so as to be located adjacent to the brushless drive motor/generator and the control module is configured to be mounted in a pressurized zone of the aircraft, the control module being connected to the power module by a two-way communication cable in order to control its operation.
SYSTEME ET PROCEDE DE DEMARRAGE/GENERATION POUR TURBOMACHINE D'AERONEF
STARTING/GENERATING SYSTEM AND METHOD FOR AN AIRCRAFT TURBINE ENGINE
ANLASS-/ERZEUGUNGSSYSTEM UND -VERFAHREN FÜR EIN FLUGZEUGTURBINENTRIEBWERK
2021-06-09
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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