Energy supply system for supplying energy to aircraft systems
View Patent ↗An energy supply system for an aircraft comprises at least one fuel cell and at least one energy storage device, wherein the fuel cell, of which there is at least one, is coupled to the energy storage device, of which there is at least one, such that the energy storage device can be charged by means of the fuel cell.
1. An energy supply system for energy supply of at least one consumer in an aircraft, the energy supply system comprising:
at least one fuel cell;
at least one electrical energy storage device; and
at least one gas turbine serving as an auxiliary power unit for providing electrical power to consumers in the aircraft,
wherein the at least one fuel cell is coupled to the at least one electrical energy storage device such that the at least one electrical energy storage device can be charged by the fuel cell,
wherein the at least one electrical energy storage device is arranged as a buffer storage device between the at least one fuel cell and the at least one consumer, and
wherein the electrical energy storage device is configured to provide electrical power to the gas turbine in a start-up phase of the gas turbine.
2. The energy supply system of claim 1 ,
wherein said at least one electrical energy storage device is a plurality of electrical energy storage devices and said at least one fuel cell is a plurality of fuel cells.
3. The energy supply system of claim 1 ,
wherein the at least one electrical energy storage device is a capacitor.
4. The energy supply system of claim 1 ,
wherein the energy supply system is a passive system.
5. The energy supply system of claim 1 , further comprising:
at least one inverted rectifier or at least one rectifier.
6. The energy supply system of claim 5 ,
wherein the at least one inverted rectifier or the at least one rectifier convert electrical energy provided by the at least one fuel cell or of the at least one electrical energy storage device.
7. The energy supply system of claim 6 ,
wherein the conversion relates to voltage or to frequency.
8. The energy supply system of claim 1 , further comprising:
a control unit,
wherein the control unit controls the at least one electrical energy storage device to buffer demand peaks of electrical loads generated by the consumers.
9. The energy supply system of claim 1 ,
wherein the energy supply system is configured to charge the electrical energy storage device by an electrical energy recovery system from at least one of an electrical consumer load and an aircraft's on-board network.
10. A method comprising:
using an energy supply system for energy supply of at least one consumer in an aircraft, the energy supply system comprising
at least one fuel cell;
at least one electrical energy storage device;
at least one gas turbine serving as an auxiliary power unit for providing electrical power to consumers in the aircraft;
wherein the at least one fuel cell is coupled to the at least one electrical energy storage device such that the at least one electrical energy storage device can be charged by the fuel cell, and
wherein the at least one electrical energy storage device is arranged as a buffer storage device between the at least one fuel cell and the at least one consumer, and
wherein the electrical energy storage device is configured to provide electrical power the gas turbine in a start-up phase of the gas turbine.
11. A method for operating an energy supply system in an aircraft, the method comprising:
providing electrical energy by a fuel cell;
storing the provided electrical energy in an intermediate storage device;
providing electrical energy from the intermediate storage device to a gas turbine serving as an auxiliary power unit for providing electrical power to consumers in the aircraft during a start-up phase of the gas turbine.