A method for operating a gas turbine system, wherein the gas turbine system including a compressor for compression of inlet air, a combustor for combustion of a fuel gas with compressed inlet air to form an exhaust gas, a heat recovery steam generator for collecting a portion of the exhaust gas, a scrubber for scrubbing the fuel with a scrubbing fluid before it is fed into the combustor, a direct contact cooler for cooling the exhaust gas discharged from the heat recovery steam generator with a cooling fluid;
- the method comprising:
- introducing the scrubbing fluid discharged from the scrubber into the direct contact cooler,
- contacting the scrubbing fluid in the direct contact cooler with the exhaust gas discharged from the heat recovery steam generator in order to remove a portion of nitrogen oxide therefrom;
- and
- feeding the exhaust gas discharged from the direct contact cooler into the compressor.