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A gas turbine, in particular an aircraft engine and to a method for generating electrical energy in a gas turbine is provided. The gas turbine comprises at least on engine core (18), in which a shaft (19) produces a shaft output. The turbine is equipped with means that generate electrical energy bot

A gas turbine, in particular an aircraft engine and to a method for generating electrical energy in a gas turbine is provided. The gas turbine comprises at least on engine core (18), in which a shaft (19) produces a shaft output. The turbine is equipped with means that generate electrical energy both from the shaft output produced by the engine core (18) and from the compressed air that is dissipated by the engine core (18).

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What is claimed is: 1. A gas turbine, comprising: a core engine including a high pressure compressor and a shaft connected thereto for driving said high pressure compressor; an electrical power generator connected to the shaft generating electrical power from the shaft, the electrical power generat

What is claimed is: 1. A gas turbine, comprising: a core engine including a high pressure compressor and a shaft connected thereto for driving said high pressure compressor; an electrical power generator connected to the shaft generating electrical power from the shaft, the electrical power generator further including an air turbine receiving compressed air drawn from the high pressure compressor to generate electrical power, the electrical power generator including a first generator and a first coupling apparatus, the first coupling apparatus coupling the first generator to the shaft so that the first generator is capable of generating electrical power from the mechanical shaft power drawn from the core engine via the shaft, the electrical power generator further including a second generator and a second coupling apparatus coupled to the second generator, the second coupling apparatus being arranged and configured such that the second coupling apparatus is capable of removably coupling the second generator to the air turbine in a first operating state and is capable of removably coupling the second generator to the shaft in a second operating state so that the second generator is capable of generating electrical power from the mechanical power generated by the air turbine or alternatively the mechanical shaft power drawn from the core engine via the shaft, the first coupling apparatus being arranged and configured such that the first coupling apparatus is capable of coupling the first generator to the shaft when the second generator is coupled to the air turbine via the second coupling apparatus. 2. The gas turbine as recited in claim 1, wherein the second operating state is a high load range of the core engine and the electrical power generator generates electrical power in the high load range of the core engine exclusively from mechanical shaft power drawn from the core engine via the shaft. 3. The gas turbine as recited in claim 1, wherein the first operating state is a lower load range of the core engine and the electrical power generator generates electrical power in the lower load range of the core engine from the mechanical shaft power drawn from the core engine via the shaft and from pneumatic energy contained in the compressed air. 4. The gas turbine as recited in claim 1, further comprising a controller, wherein the controller, as a function of the load range of the core engine, automatically controls the second coupling apparatus such that the second coupling apparatus couples and uncouples the second generator from the air turbine. 5. The gas turbine as recited in claim 1, wherein the first coupling apparatus includes a first gear and the first generator is connected to the shaft via the first gear. 6. The gas turbine as recited in claim 5, wherein the second coupling apparatus includes a second gear and the second generator is connected to the air turbine via the second gear. 7. The gas turbine as recited in claim 6 wherein the second coupling apparatus further includes a freewheel assigned to the second gear which cooperates with the air turbine. 8. The gas turbine as recited in claim 7, wherein the second coupling apparatus further includes a controllable clutch and the first and second generators are connectable to one another via the controllable clutch in the second operating state the second operating state being an upper load range of the core engine, the first and second generators being driven in the upper load range of the core engine exclusively by the shaft. 9. The gas turbine as recited in claim 8, wherein the first and second gears are connected to one another via the controllable clutch and the freewheel decouples the air turbine. 10. The gas turbine as recited in claim 8 wherein the first operating state is a lower load range of the core engine and the first and second generators are decoupled in the lower load range of the core engine, the first generator being driven exclusively by the shaft and the second generator being driven exclusively by the air turbine. 11. The gas turbine as recited in claim 10, wherein the controllable clutch decouples the first and second generators by decoupling the first and second gears from one another, and the freewheel couples the air turbine with the second generator via the second gear. 12. The gas turbine as recited in claim 1, wherein the electrical power generator is connected to the shaft via a gear, the electrical power generator generating electrical power from the mechanical shaft power drawn from the core engine via the shaft. 13. The gas turbine as recited in claim 1 wherein the first operating state is a lower load range of the core engine and the first and second generators are decoupled in the lower load range of the core engine, the first generator being driven exclusively by the shaft and the second generator being driven exclusively by the air turbine. 14. The gas turbine recited in claim 1 wherein the first coupling apparatus and the second coupling apparatus are arranged and configured such that in the second operating state the second coupling apparatus couples the second generator to the shaft via the first coupling apparatus. 15. A gas turbine, comprising: a core engine including a high pressure compressor and a shaft connected thereto for driving said high pressure compressor; an electrical power generator connected to the shaft generating electrical power from the shaft, the electrical power generator further including an air turbine receiving compressed air drawn from the high pressure compressor to generate electrical power, the electrical power generator including a first generator and a first coupling apparatus, the first coupling apparatus coupling the first generator to the shaft, the first generator generating electrical power from the mechanical shaft power drawn from the core engine via the shaft in a lower load range and a higher load range, the electrical power generator further including a second generator and a second coupling apparatus coupled to the second generator, the second coupling apparatus being arranged and configured such that the second coupling apparatus is capable of removably coupling the second generator to the air turbine in the lower load range and is capable of removably coupling the second generator to the shaft in the higher load range so that the second generator is capable of generating electrical power from the mechanical power generated by the air turbine in the lower load range and from the mechanical shaft power drawn from the core engine via the shaft in the higher load range. 16. A gas turbine, comprising: a core engine including a high pressure compressor and a shaft connected thereto for driving said high pressure compressor; an electrical power generator connected to the shaft generating electrical power from the shaft, the electrical power generator further including an air turbine receiving compressed air drawn from the high pressure compressor to generate electrical power, the electrical power generator including a first generator and a first coupling apparatus, the first coupling apparatus coupling the first generator to the shaft, the first generator generating electrical power from the mechanical shaft power drawn from the core engine via the shaft, the electrical power generator further including a second generator and a second coupling apparatus coupled to the second generator, the second coupling apparatus being arranged and configured such that the second coupling apparatus is capable of removably coupling the second generator to the air turbine so that the second generator is capable of generating electrical power from the mechanical power generated by the air turbine; and a controller, the controller controlling the second coupling apparatus such that the second coupling apparatus couples and uncouples the second generator from the air turbine so that an operating characteristic curve of the gas turbine maintains a predetermined surge limit margin.