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Systems and methods for controlling a gas turbine are disclosed. The gas turbine can include a compressor oversized in airflow capacity and one or variable blade rows to control the airflow into the compressor. The position of the variable blade rows can be controlled according to a nominal variable

Systems and methods for controlling a gas turbine are disclosed. The gas turbine can include a compressor oversized in airflow capacity and one or variable blade rows to control the airflow into the compressor. The position of the variable blade rows can be controlled according to a nominal variable blade row schedule that is defined to throttle down the variable blade rows to provide nominal flow into the compressor. The positions of the variable blade rows can be adjusted from the nominal positions set forth in the variable blade row schedule pursuant to a request to operate the gas turbine system in either a controlled output mode or in a frequency compensation mode.

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1. A gas turbine system, comprising: a compressor oversized in airflow capacity configured to supply compressed air for use during combustion in the gas turbine;one or more variable blade rows configured to control the airflow rate into said compressor, said one or more variable blade rows being mov

1. A gas turbine system, comprising: a compressor oversized in airflow capacity configured to supply compressed air for use during combustion in the gas turbine;one or more variable blade rows configured to control the airflow rate into said compressor, said one or more variable blade rows being movable between a first position wherein said one or more variable blade rows provide a maximum airflow rate into said compressor and a second position wherein said one or more variable blade rows provide a decreased airflow rate into said compressor;a controller configured to operate the gas turbine system in a nominal mode, a controlled output mode, and a frequency compensation mode, the controller configured to control the position of said one or more variable blade rows according to a nominal variable blade row position schedule when the gas turbine system is operated in the nominal mode, said nominal variable blade row position schedule specifying nominal positions for said one or more variable blade rows such that said one or more variable blade rows provide a nominal airflow rate into said compressor, the nominal airflow rate being less than the maximum airflow rate;wherein pursuant to an operator request, said gas turbine system is operable in either the controlled output mode or the frequency compensation mode, said controller configured to adjust the position of the one or more variable blade rows from the nominal positions specified in the nominal variable blade row schedule to operate said gas turbine system in the controlled output mode or in the frequency compensation mode, wherein when said gas turbine is operated in the controlled output mode, said controller is configured to adjust the position of said one or more variable blade rows to increase or decrease airflow into said compressor to achieve a power output requested by an operator. 2. The gas turbine system of claim 1, wherein said compressor is oversized in airflow capacity such that said compressor can provide an increased airflow rate at a design point ambient temperature that is greater than the design point airflow rate at the design point ambient temperature. 3. The gas turbine system of claim 2, wherein said compressor is oversized in airflow capacity such that the increased airflow rate at about 59° F. is approximately 5% to 25% greater than the design point airflow rate at about 59° F. 4. The gas turbine system of claim 1, wherein when said gas turbine system is operated in the controlled output mode, said controller is configured to adjust the position of said one or more variable blade rows to increase airflow into the compressor to compensate for airflow loss in said compressor due to increased ambient temperature. 5. The gas turbine system of claim 1, wherein when said gas turbine system is operated in said frequency compensation mode, said controller is configured to monitor the frequency of an electricity grid and adjust the position of said one or more variable blade rows based at least in part on the frequency of the electricity grid. 6. The gas turbine system of claim 5, wherein said controller is configured to: adjust the position of said one or more variable blade rows to provide increased airflow into said compressor when the frequency of the electricity grid is less than a first threshold;adjust the position said one or more variable blade rows to provide decreased airflow into said compressor when the frequency of the electricity grid is greater than a second threshold; andmaintain the position of said one or more variable blade rows when the frequency of the electricity grid is greater than or approximately equal to the first threshold and less than or approximately equal to the second threshold. 7. A gas turbine system, the gas turbine system comprising: a compressor oversized in airflow capacity configured to supply compressed air for use in combustion in the gas turbine;one or more variable blade rows for controlling the airflow into said compressor; and a controller configured to operate the gas turbine system in a nominal mode, a controlled output mode and in a frequency compensation mode, the controller configured to control the position of said one or variable blade rows according to a nominal variable blade row schedule when the gas turbine system is operated in the nominal mode, said controller being further configured to adjust the position of said one or more variable blade rows from the nominal positions set forth in the nominal variable blade row schedule in response to a request to operate the gas turbine in the controlled output mode or the frequency compensation mode;wherein when said gas turbine system is operated in the controlled output mode, said controller is configured to adjust the position of said one or more variable blade rows to increase or decrease airflow into said compressor to achieve a power output requested by an operator; wherein when said gas turbine system is operated in said frequency compensation mode, said controller is configured to monitor the frequency of an electricity grid and adjust the position of said one or more variable blade rows based at least in part on the frequency of the electricity grid. 8. The gas turbine system of claim 7, wherein said nominal variable blade row position schedule specifies nominal positions for said one or more variable blade rows such that said one or more variable blade rows provide a nominal airflow rate into said compressor, the nominal airflow rate being less than a maximum airflow rate into said compressor. 9. The gas turbine system of claim 7, wherein said compressor is oversized in airflow capacity such that said compressor can provide an increased airflow rate at the design point ambient temperature that is greater than the design point airflow rate at the design point ambient temperature. 10. The gas turbine system of claim 9, wherein said compressor is oversized in airflow capacity such that the increased airflow rate at about 59° F. is approximately 5% to 25% greater than the design point airflow rate at about 59° F. 11. The gas turbine system of claim 7, wherein when said gas turbine is operated in said controlled output mode, said controller is configured to adjust the position of said one or more variable blade rows to increase airflow into said compressor to compensate for airflow loss in said compressor due to increased ambient temperature. 12. The gas turbine system of claim 10, wherein when said gas turbine is operating in said frequency compensation mode, said controller is configured to: adjust the position of said one or more variable blade rows to provide increased airflow into said compressor when the frequency of the electricity grid is less than a first threshold;adjust the position said one or more variable blade rows to provide decreased airflow into said compressor when the frequency of the electricity grid is greater than a second threshold; andmaintain the position of said one or more variable blade rows when the frequency of the electricity grid is greater than or approximately equal to the first threshold and less than or approximately equal to the second threshold.