ELECTRICAL POWER SUPPLY SYSTEM AND METHOD FOR AN AIRCRAFT

The invention relates to a system and a method for supplying electric power to an aircraft. This system comprises an electrical network comprising main generators (G) for supplying electrical distribution channels and a homopolar generator (30) for creating an artificial neutral.

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Bibliographische Detailangaben
Hauptverfasser:	PRISSE, LUCIEN, PAUVERT, VINCENT, AUBERT, BRICE, ALEJO, DOMINIQUE
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GENERATION PARACHUTES PERFORMING OPERATIONS REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION SYSTEMS FOR STORING ELECTRIC ENERGY TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention relates to a system and a method for supplying electric power to an aircraft. This system comprises an electrical network comprising main generators (G) for supplying electrical distribution channels and a homopolar generator (30) for creating an artificial neutral.