Electrical supply system for an aircraft with a legacy AC network and a bipolar DC network
An electrical supply system for an aircraft includes a generator having a neutral point, an AC network, a bipolar DC network, and a neutral point clamped converter. The neutral point is connected to ground, in at least one operating mode. The converter has an AC side with AC connectors couplable with at least one phase of the generator. The converter also has a DC side with a first DC connector, a second DC connector and a neutral DC connector. The AC side of the converter is coupled with the generator, the DC side is coupled with the bipolar DC network, and the neutral DC connector is connected to ground. The convertor provides a DC voltage on the DC side upon receiving an AC voltage on the AC side, and provides an AC voltage on the AC side upon receiving a DC voltage on the DC side.
1. An electrical supply system for an aircraft, comprising:
a generator having a plurality of phases and a neutral point;
an AC network;
a bi polar DC network; and
a neutral point clamped converter;
wherein the generator provides an AC voltage;
wherein the neutral point of the generator is connected to ground, in at least one mode of operation;
wherein the converter comprises an AC side having a plurality of AC connectors, each of which is couplable with at least one phase of the generator, and comprises a DC side having a first DC connector, a second DC connector and a neutral DC connector;
wherein the AC side of the converter is coupled with the generator, the DC side is coupled with the bipolar DC network, and the neutral DC connector is connected to ground; and
wherein the convertor provides a DC voltage on the DC side upon receiving an AC voltage on the AC side, and provides an AC voltage on the AC side upon receiving a DC voltage on the DC side,
further comprising a first switch and a second switch, wherein the first switch is arranged directly between the generator and the converter to selectively interrupt a connection of the generator and the converter, independent of a position of the second switch, and wherein the second switch is arranged directly between the generator and the AC network to selectively interrupt a connection of the generator to the AC network, independent of a position of the first switch, and
a third switch, wherein the third switch is arranged between a first branch point between the first switch and the AC side of the converter and a second branch point between the second switch and the AC network to selectively provide a connection of the AC network to the AC side of the converter.
2. The electrical supply system of claim 1 , wherein the converter is a multilevel neutral point clamped converter.
3. The electrical supply system of claim 1 ,
further comprising a first filter arranged between the generator and the AC side of the converter, wherein the first filter is configured to receive an unmodified AC current from the generator and to influence the AC voltage delivered from the AC side or to the AC side of the converter to reach a predetermined voltage/power quality.
4. The electrical supply system of claim 3 , further comprising a second filter arranged between the AC network and the generator, wherein the second filter is configured to receive an unmodified AC current from the generator and to influence the AC voltage delivered into the AC network to reach a predetermined voltage/power quality.
5. The electrical supply system of claim 1 , further comprising an additional power supply device to provide a DC voltage to the bipolar DC network.
6. The electrical supply system of claim 1 , wherein the converter is a three-level neutral point clamped converter.
7. The electrical supply system of claim 1 , wherein the converter is a two-level converter.
8. An aircraft comprising an electrical supply system, the electrical supply system comprising:
a generator having a plurality of phases and a neutral point;
an AC network;
a bi polar DC network; and
a neutral point clamped converter;
wherein the generator provides an AC voltage;
wherein the neutral point of the generator is connected to ground, in at least one mode of operation;
wherein the converter comprises an AC side having a plurality of AC connectors, each of which is couplable with at least one phase of the generator, and comprises a DC side having a first DC connector, a second DC connector and a neutral DC connector;
wherein the AC side of the converter is coupled with the generator, the DC side is coupled with the bipolar DC network, and the neutral DC connector is connected to ground; and
wherein the convertor provides a DC voltage on the DC side upon receiving an AC voltage on the AC side, and provides an AC voltage on the AC side upon receiving a DC voltage on the DC side,
further comprising a first switch and a second switch, wherein the first switch is arranged directly between the generator and the converter to selectively interrupt a connection of the generator and the converter, independent of a position of the second switch, and wherein the second switch is arranged directly between the generator and the AC network to selectively interrupt a connection of the generator to the AC network, independent of a position of the first switch, and
a third switch, wherein the third switch is arranged between a first branch point between the first switch and the AC side of the converter and a second branch point between the second switch and the AC network to selectively provide a connection of the AC network to the AC side of the converter.