turbine system 12 can be parked at a higher load as indicated by point u201c b u201d in fig8 with a higher exhaust temperature at the higher exhaust temperature the no x and co emissions in the exhaust gas stream 32 are lower the temperature of the exhaust gas stream 32 of the gas turbine system 12 can be controlled using the bypass air ba to provide an inlet temperature of about 700 u00b0 f at the hrsg system 14 this results in lower start up no x and co emissions and also helps to increase the power output of the gas turbine system 12 during start up comparing point a and point b in fig8 for example it can easily be seen that the gas turbine system 12 can be operated point b at a higher temperature and higher load than a conventional gas turbine system point a while still providing an inlet temperature of about 700 u00b0 f at the hrsg system 14 during normal operation a portion of the flow of air generated by the fan 60 may be used to supercharge the compressor component 18 of the gas turbine system 12 thereby boosting the power output of the gas turbine system 12 further the.