| 摘要 |
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. |
