ELECTRICAL SUPPLY CIRCUIT IN AN AIRCRAFT FOR ELECTRICAL EQUIPMENT, INCLUDING A DE-ICING CIRCUIT

The circuit has a power distribution system (17) for supplying power to electrical equipment i.e. nacelle load (5b), arranged in an engine (23) i.e. gas turbine engine, of an aircraft e.g. airplane, or in a surrounding of the engine. A power generator (27) is integrated to the engine, and is directl...

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Bibliographische Detailangaben
Hauptverfasser:	STUTZ, ANTOINE JEAN-BAPTISTE, BOUDYAF, RACHID
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The circuit has a power distribution system (17) for supplying power to electrical equipment i.e. nacelle load (5b), arranged in an engine (23) i.e. gas turbine engine, of an aircraft e.g. airplane, or in a surrounding of the engine. A power generator (27) is integrated to the engine, and is directly connected to another electrical equipment i.e. nacelle anti-icing system (5a), for supplying alternating current (AC) voltage to the anti-icing system. A permanent magnet generator is mechanically coupled with the power generator.