ELECTRICAL CONVERSION AND DISTRIBUTION SYSTEM FOR AN AIRCRAFT

The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising a synchronous starter-generator (ENG S/G) intended to be coupled to an aircraft engine, a rectifier (R) capable of transforming alternating voltage into direct voltage, an auxiliary synch...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DE WERGIFOSSE, Eric, CASIMIR, Roland, GIORGIS, Vincent
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GENERATION SYSTEMS FOR STORING ELECTRIC ENERGY
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