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A method for operating a power plant to facilitate reducing emissions, wherein the power plant includes a gas turbine engine assembly and a carbon dioxide (CO2) separator. The method includes increasing an operating pressure of exhaust gas discharged from the gas turbine engine assembly, separating

A method for operating a power plant to facilitate reducing emissions, wherein the power plant includes a gas turbine engine assembly and a carbon dioxide (CO2) separator. The method includes increasing an operating pressure of exhaust gas discharged from the gas turbine engine assembly, separating substantially all the CO2 entrained within the gas turbine engine utilizing the CO2separator to produce a CO2 lean airstream, reducing the operating temperature of the CO2lean airstream, and utilizing the cooled CO2lean airstream to facilitate reducing an operating temperature of air entering the gas turbine engine assembly.

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1. A method for reducing emissions in a power plant including a gas turbine engine assembly and a carbon dioxide (CO2) separator, said method comprising: increasing an operating pressure of an exhaust stream discharged from the gas turbine engine assembly;reducing an operating temperature of the exh

1. A method for reducing emissions in a power plant including a gas turbine engine assembly and a carbon dioxide (CO2) separator, said method comprising: increasing an operating pressure of an exhaust stream discharged from the gas turbine engine assembly;reducing an operating temperature of the exhaust stream;substantially reducing a concentration of CO2 entrained within the exhaust stream utilizing the CO2 separator to produce a CO2 lean exhaust stream;reducing the operating temperature of the CO2 lean exhaust stream;channeling the cooled CO2 lean exhaust stream through a first flow path of a heat exchanger to reduce an operating temperature of a flow of ambient air channeled through a second flow path of the heat exchanger prior to entering the gas turbine engine assembly wherein the first and second flow paths are coupled in thermal communication and isolated in flow communication with respect to each other;substantially removing moisture entrained in the gas turbine engine inlet airflow utilizing a desiccant air drying system; andchanneling the relatively dry air discharged from the desiccant air drying system through a heat exchanger. 2. A method in accordance with claim 1, further comprising: reducing the moisture content within the CO2 lean exhaust stream utilizing a desiccant air drying system; andchanneling the airflow discharged from the desiccant air drying system into an expander to facilitate reducing the operating temperature of the CO2 lean airstream. 3. A method in accordance with claim 1, further comprising: channeling the exhaust stream discharged from the CO2 separator through an expander to facilitate reducing the operating temperature of the CO2 lean exhaust stream;channeling a first portion of the exhaust stream discharged from the expander directly into the gas turbine engine inlet to reduce the temperature of the gas turbine engine inlet air; andchanneling a second portion of the exhaust stream discharged from the expander to a heat exchanger to remove heat energy from the exhaust stream channeled into the compressor. 4. A method in accordance with claim 1, further comprising: dividing the CO2 lean exhaust stream into a first portion and a second portion; andmixing the first portion of the CO2 lean exhaust stream with the air entering the gas turbine engine assembly to facilitate reducing nitrous oxide emissions generated by the gas turbine engine assembly. 5. A method in accordance with claim 4, further comprising: mixing the first portion of the CO2 lean exhaust stream with the air entering the gas turbine engine assembly to produce a fog that includes a plurality of water droplets; andchanneling the fog into the gas turbine engine assembly to facilitate reducing the operational temperature of the airflow supplied to the gas turbine engine assembly and to reduce the work required in the compression process and increase the overall efficiency of the gas turbine engine assembly. 6. A method in accordance with claim 4, further comprising channeling the second portion of the CO2 lean exhaust stream through a heat exchanger to facilitate reducing the operating temperature of the exhaust stream and to facilitate moisture condensation and its removal from the exhaust stream. 7. A power plant, comprising: a gas turbine engine assembly;a compressor configured to increase an operating pressure of an exhaust stream;a heat recovery steam generator configured to receive said exhaust stream and reducing the operating temperature of the exhaust stream;a carbon dioxide (CO2) separator in flow communication with said gas turbine engine assembly, said CO2 separator configured to substantially remove the CO2 from said gas turbine engine exhaust stream to produce a CO2 lean exhaust stream;an expander configured to reduce an operating temperature of the CO2 lean exhaust stream; anda heat exchanger configured to receive said exhaust stream discharged from said expander and utilizing said cooled CO2 lean exhaust stream to reduce an operating temperature of the gas turbine engine inlet airflow. 8. A power plant in accordance with claim 7, wherein said CO2 separator is configured to receive substantially all of the exhaust stream discharged from said gas turbine engine assembly. 9. A power plant in accordance with claim 7, further comprising an intercooler configured to receive the exhaust stream discharged from said compressor and reduce an operating temperature of the exhaust stream. 10. A power plant in accordance with claim 7, further comprising a first desiccant air drying system configured to substantially remove moisture from a gas turbine engine inlet airflow. 11. A power plant in accordance with claim 7, further comprising a second desiccant air drying system configured to reduce the moisture content within the CO2 lean exhaust stream discharged from said CO2 separator. 12. A power plant in accordance with claim 7, further comprising a low-pressure compressor that is coupled to said expander, said expander configured to drive said low-pressure compressor. 13. A power plant in accordance with claim 12, further comprising a prime mover coupled to said expander, said prime mover configured to supplement said expander to drive said low-pressure compressor. 14. A power plant in accordance with claim 13, wherein said prime mover comprises at least one of a gas turbine engine, a reciprocating engine, and an electric motor. 15. A power plant in accordance with claim 7, further comprising an intercooler configured to generate heat energy that is utilized in the CO2 separation process. 16. A power plant in accordance with claim 7, further comprising a heat recover steam generator configured to generate heat energy that is utilized in the CO2 separation process. 17. A power plant in accordance with claim 7, wherein said carbon dioxide (CO2) separator is further configured to recirculate the CO2 lean exhaust stream to the gas turbine engine inlet to facilitate reducing nitrous oxide emissions in the gas turbine engine. 18. A power plant in accordance with claim 7, wherein said carbon dioxide (CO2) separator comprises an amine solution to separate CO2 from the gas turbine engine exhaust stream. 19. A power plant in accordance with claim 7, wherein said carbon dioxide (CO2) separator comprises a plurality of membranes to separate CO2 from the gas turbine engine exhaust stream.