Electrical network of an aircraft

1. An electrical network of an aircraft comprising:

several main generators,

several high voltage direct current HVDC networks, each one powered by one of the generators in normal operation,

several low voltage direct current LVDC networks, each one powered by one of the high voltage direct current HVDC networks,

several converters to transfer energy from one of the high voltage direct current HVDC networks to one of the low voltage direct current LVDC networks, the different converters being independent and isolated from each other, each converter being dedicated to one of the high voltage HVDC networks and to the low voltage direct current LVDC network,

a load designed to be powered in normal operation by the main generators and in backup operation by one of the low voltage direct current LVDC networks, the backup operation being put into place when at least one of the high voltage HVDC networks is no longer powered by the associated main generator in normal operation,

in which the converters are reversible and in backup operation the load is powered in parallel by several of the high voltage direct current HVDC networks whose energy comes from the low voltage direct current LVDC networks.

2. The electrical network according to claim 1 , in which the load is an auxiliary generator APU.

3. The electrical network according to claim 1 , in which the converters each have a nonzero apparent output impedance defined so as to allow several converters being placed in parallel without common control means for the different converters.

4. The electrical network according to claim 3 , in which the apparent output impedance has an increase in value beyond a predefined current strength provided by the particular converter.

5. The electrical network according to claim 1 , in which each of the converters is configured to limit the current strength which it is able to provide to a maximum value.

6. The electrical network according to claim 1 , further comprising, between each of the high voltage direct current HVDC networks and the load, a secondary distribution comprising a plurality of contactors and enabling either isolating or connecting of the load and the high voltage direct current HVDC network in question and in which the load can be powered in parallel by several of the different high voltage direct current HVDC networks through the secondary distribution.

7. The electrical network according to claim 6 , further comprising a control module for the secondary distribution configured to enable the closing of the contactors if the main generators are not providing power to the high voltage direct current HVDC networks.

8. The electrical network according to claim 1 , in which the first load utilizes a plurality of converters in parallel and the network further comprises:

a plurality of second loads utilizing the converters independently of each other and designed to be powered separately by the high voltage direct current HVDC networks,

means of managing the priority between the first load and the second loads.

9. The electrical network according to claim 8 , in which the second loads are EBAC braking systems designed to brake the wheels of a landing gear of the airplane.

10. The electrical network according to claim 9 , furthermore further comprising:

a plurality of batteries, each one connected to one of the low voltage direct current LVDC networks,

means of managing the load of the batteries making it possible to preserve a minimum charge sufficient to power the electric brakes.

11. The electrical network according to claim 1 , further comprising:

an avionics system able to be connected in backup operation to one of the low voltage direct current LVDC networks,

at least one battery able to be dedicated to the avionics system.