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A method of operating a turbine engine system and a turbine engine system are provided. The method comprises supplying a flow of oxygen to a combustion chamber defined within a plurality of turbines coupled serially together within the turbine engine system, supplying a flow of hydrocarbonaccous fue

A method of operating a turbine engine system and a turbine engine system are provided. The method comprises supplying a flow of oxygen to a combustion chamber defined within a plurality of turbines coupled serially together within the turbine engine system, supplying a flow of hydrocarbonaccous fuel to the combustion chambers of each of the plurality of turbines in the turbine engine system, and supplying a working fluid to an inlet of a first turbine engine coupled within the turbine engine system, wherein the working fluid is substantially nitrogen-free and wherein each of the turbines coupled within the turbine engine system is operable with the resulting fuel-oxygen-working fluid mixture.

대표청구항 ▼

1. A gas turbine engine system comprising: at least a first gas turbine engine, a second gas turbine engine, and a last gas turbine engine of a plurality of substantially identical gas turbine engines coupled together in serial flow communication wherein each gas turbine engine downstream of said fi

1. A gas turbine engine system comprising: at least a first gas turbine engine, a second gas turbine engine, and a last gas turbine engine of a plurality of substantially identical gas turbine engines coupled together in serial flow communication wherein each gas turbine engine downstream of said first gas turbine engine receives all of a substantially nitrogen-free exhaust from the gas turbine engine directly upstream and wherein each gas turbine engine upstream of said last gas turbine engine discharges a respective substantially nitrogen-free exhaust to the gas turbine engine directly downstream, each of said gas turbine engines comprises at least one compressor, at least one combustion chamber and at least a low pressure turbine and a high pressure turbine downstream from said combustion chamber, each said combustion chamber is coupled in flow communication to a source of hydrocarbonaceous fuel and to a source of oxygen, a working fluid of each said gas turbine engine being substantially nitrogen-free; andan exhaust gas conditioning system coupled between a discharge outlet of the last of said gas turbine engines coupled together in said system and an inlet of the first of said gas turbine engines coupled together in said system, said exhaust gas conditioning system configured to remove heat and water vapor from exhaust gases only from said last gas turbine engine to generate a flow of conditioned exhaust gas and to direct the flow of conditioned exhaust gas to said first gas turbine engine as a gas turbine engine working fluid, wherein said exhaust gas conditioning system is the only exhaust gas conditioning system coupled to the plurality of substantially identical gas turbine engines. 2. A gas turbine engine system in accordance with claim 1 further comprising a sequestration chamber coupled downstream from said exhaust gas conditioning system for storing at least a portion of exhaust discharged from said gas turbine engine system. 3. A gas turbine engine system in accordance with claim 2 wherein said sequestration chamber comprises a sub-surface storage chamber. 4. A gas turbine engine system in accordance with claim 2 wherein said exhaust gas conditioning system comprises at least one of a heat exchanger and an air separation unit coupled in flow communication between said last gas turbine engine and said sequestration chamber, and between said first gas turbine inlet and said last turbine engine discharge outlet. 5. A gas turbine engine system in accordance with claim 4 wherein each of said plurality of gas turbine engines is operable with a stream of carbon dioxide supplied from said exhaust gas conditioning system for use as a working fluid. 6. A gas turbine engine system in accordance with claim 1 wherein said exhaust gas conditioning system facilitates improving an operating efficiency of each of said plurality of gas turbine engines. 7. A gas turbine engine system in accordance with claim 1 wherein said exhaust gas conditioning system facilitates reducing nitrous oxide emissions generated from said gas turbine engine system. 8. A power generation system comprising: a first gas turbine engine comprising an inlet and a discharge outlet; anda second gas turbine engine substantially identical to said first gas turbine engine, said second gas turbine engine comprising an inlet and a discharge outlet, said second gas turbine engine inlet coupled to said first gas turbine engine discharge outlet for receiving all of a substantially nitrogen-free flow of exhaust gases discharged therefrom for use as a working fluid in said second gas turbine engine;a third gas turbine engine substantially identical to said first and second gas turbine engines, said third gas turbine engine comprising an inlet and a discharge outlet, said third gas turbine engine inlet coupled to said second gas turbine engine discharge outlet for receiving all of a substantially nitrogen-free flow of exhaust gases discharged therefrom for use as a working fluid in said third gas turbine engine,each of said first, second, and third gas turbine engines comprises at least one compressor, at least one combustion chamber and at least a low pressure turbine and a high pressure turbine downstream from said at least one combustion chamber, each of said at least one combustion chambers is coupled in flow communication to a source of hydrocarbonaceous fuel and to a source of oxygen; andan exhaust gas conditioning system coupled between said third gas turbine discharge outlet and said first gas turbine engine inlet, said exhaust gas conditioning system receives all of the exhaust discharged from said third gas turbine engine. 9. A power generation system in accordance with claim 8 wherein each of said first, second, and third gas turbine engines is operable with a working fluid that is substantially nitrogen-free. 10. A power generation system in accordance with claim 8 further comprising a sequestration chamber for storing carbon dioxide, said sequestration chamber coupled to exhaust gas conditioning system for receiving a portion of exhaust discharged from said exhaust gas conditioning system. 11. A power generation system in accordance with claim 10 wherein said sequestration chamber is further coupled to each of said first, second, and third turbine gas engines for receiving a portion of working fluid bled from each of said first, second, and third turbine gas engines. 12. A power generation system in accordance with claim 10 wherein said sequestration chamber comprises a sub-surface chamber. 13. A power generation system in accordance with claim 8 wherein said exhaust gas conditioning system comprises at least one of a heat exchanger and an air separation unit.