Electrical power distribution system and method with active load control

1. A method of sharing an electrical load in an electrical power distribution system, the method comprising:

providing a first AC power source, a second AC power source, a first DC bus, and a second DC bus;

connecting the first AC power source to the first DC bus via a first AC to DC rectifier;

connecting the second AC power source to the first DC bus via a second AC to DC rectifier;

connecting the second AC power source to the second DC bus via the second AC to DC rectifier;

extracting DC power simultaneously from the first and the second DC buses to satisfy a total DC load requirement;

monitoring an amount of DC power extracted from first and the second DC buses;

determining a desired proportion of the total DC load requirement that is to be provided by each of the DC buses;

changing a proportion of the total DC load provided from the first DC bus by changing an AC voltage output of the first AC power source relative to an AC voltage output of the second AC power source, to correspondingly change DC voltage on the first DC bus relative to DC voltage on the second DC bus and thereby partially shift power extraction between the first and second AC power sources.

2. The method of claim 1 , further comprising the step of:

applying a reverse bias on a diode of the second AC to DC rectifiers, thereby restricting DC voltage output to the second DC bus from the first AC to DC rectifier.

3. The method of claim 1 , further comprising the steps of:

acquiring the DC voltage output of the first DC bus; and

regulating the AC voltage output of the first AC power unit relative to the AC voltage output of the second AC power sources via a first regulation control unit and a second regulation control.

4. The method of claim 1 , wherein the step of providing the first power source and the second power source comprises:

driving a first AC generator with a first spool of a first aircraft engine; and

driving a second AC generator with one of;

a second aircraft engine,

an auxiliary power unit, and

a second spool of the first aircraft engine.

5. An electrical power distribution system, comprising:

a first AC power source;

a first regulation control unit for controlling AC voltage output of the first AC power source;

a second AC power source;

a second regulation control unit for controlling AC voltage output of the first AC power source;

a first DC bus;

a second DC bus;

a first AC to DC rectifier, the first AC power source being connected to the first DC bus via the first AC to DC rectifier;

a second AC to DC rectifier, the second AC power source being connected to the first DC bus via the second AC to DC rectifier;

the second AC power source being connected to the second DC bus via the second AC to DC rectifier; and

an electrical load management control unit interconnected to provide desired output-voltage commands to the first and the second regulation control units;

the electrical load management control unit interconnected to the first and second DC buses to determine DC voltages on the first and second DC buses;

the electrical load management control unit varying DC voltage on the first and second DC buses by varying AC output voltage of the first and second AC power sources with commands to the first and second regulation control units;

the electrical load management control unit providing a desired allocation of a total DC load to the first and second DC buses by varying the DC voltage on the first and second DC buses.