Electrical network of an aircraft and method of operation of the electrical network

An electrical network of an aircraft and a method of operation comprises: an AC bus, a DC bus, a rectifier providing a DC voltage to the DC bus with the help of the AC bus, a plurality of bidirectional converters comprising two linkup points, each bidirectional converter being linked up at its first...

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Bibliographische Detailangaben
1. Verfasser:	Tardy Alain
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS PRODUCING MECHANICAL POWER SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING VEHICLES IN GENERAL VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR WEAPONS WIND MOTORS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	An electrical network of an aircraft and a method of operation comprises: an AC bus, a DC bus, a rectifier providing a DC voltage to the DC bus with the help of the AC bus, a plurality of bidirectional converters comprising two linkup points, each bidirectional converter being linked up at its first linkup point to the DC bus and being able to be linked up at its second linkup point to a load of the aircraft so as to power it, the network being able to be linked up to at least two generators each capable of delivering the AC voltage to the AC bus by the rectifier. At least one link links up at least one of the generators to the second linkup point of at least one of the bidirectional converters. The network can change generator with no cutoff and with no particular synchronization of the generators.