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A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbin

A power generation system includes: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A control valve system controls flow of the excess air flow from the first gas turbine system to the second gas turbine system. A cooling fluid injector may be coupled to the excess air flow path for injecting a cooling fluid such as water or steam into the excess air flow.

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1. A power generation system, comprising: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first

1. A power generation system, comprising: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of at least one of the first combustor and the first turbine component, creating an excess air flow;a second gas turbine system including a second turbine component, a second compressor and a second combustor to which air from the second compressor and fuel are supplied, the second combustor arranged to supply hot combustion gases to the second turbine component;a control valve system controlling flow of the excess air flow from the first gas turbine system to the second gas turbine system along an excess air flow path, wherein the control valve system includes a first control valve controlling a first portion of the excess air flow to a discharge of the second compressor, a second control valve controlling a second portion of the excess air flow to the second combustor, and a third control valve controlling a third portion of the flow of the excess air flow to the turbine nozzle cooling inlets of the second turbine component; anda cooling fluid injector coupled to the excess air flow path for injecting a cooling fluid into the excess air flow. 2. The power generation system of claim 1, further comprising at least one sensor for measuring a flow rate of at least a portion of the excess air flow, each sensor operably coupled to the control valve system. 3. The power generation system of claim 1, wherein an exhaust of each of the first turbine system and the second turbine system are supplied to at least one steam generator for powering a steam turbine system. 4. The power generation system of claim 1, wherein the cooling fluid injector injects water as the cooling fluid. 5. The power generation system of claim 1, wherein the cooling fluid injector injects steam as the cooling fluid. 6. A power generation system, comprising: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of at least one of the first combustor and the first turbine component, creating an excess air flow;a second gas turbine system including a second turbine component, a second compressor and a second combustor to which air from the second compressor and fuel are supplied, the second combustor arranged to supply hot combustion gases to the second turbine component;a control valve system controlling flow of the excess air flow to at least one of a discharge of the second compressor, the second combustor and a turbine nozzle cooling inlet of the second turbine component along an excess air flow path; anda cooling fluid injector coupled to the excess air flow path for injecting a cooling fluid into the excess air flow,wherein the control valve system includes a first control valve controlling a first portion of the excess air flow to the discharge of the second compressor, a second control valve controlling a second portion of the excess air flow to the second combustor, and a third control valve controlling a third portion of the flow of the excess air flow to the turbine nozzle cooling inlets of the second turbine component, andwherein an exhaust of each of the first turbine system and the second turbine system are supplied to at least one steam generator for powering a steam turbine system. 7. The power generation system of claim 6, wherein the cooling fluid injector injects water as the cooling fluid. 8. The power generation system of claim 6, wherein the cooling fluid injector injects steam as the cooling fluid. 9. A method for providing and controlling an excess flow of air in a power generation system, comprising: extracting an excess air flow from a first integral compressor of a first gas turbine system including a first turbine component, the first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first integral compressor having a flow capacity greater than an intake capacity of at least one of the first combustor and the first turbine component;directing the excess air flow to a second gas turbine system including a second turbine component, a second compressor and a second combustor to which air from the second compressor and fuel are supplied, the second combustor arranged to supply hot combustion gases to the second turbine component;controlling, using a control valve system, flow of the excess air flow from the first gas turbine system to the second gas turbine system along an excess air flow path, wherein the control valve system includes a first control valve controlling a first portion of the excess air flow to a discharge of the second compressor, a second control valve controlling a second portion of the excess air flow to the second combustor, and a third control valve controlling a third portion of the flow of the excess air flow to the turbine nozzle cooling inlets of the second turbine component; andinjecting a cooling fluid into the excess air flow path. 10. The method of claim 9, wherein the injecting includes injecting one of water and steam as the cooling fluid.