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Gas Turbine Regenerator
Looking for support calculation of how we can calculate the required exhaust flow of flue gas to raise the compressor exist temp prior enter to the combustion.

we have nine GT Hitachi frame 7E each, two GT couple with HRSG. However, only one GT can connected to ONE HRSG while other GT is either working as simple cycle or on stand by mode. From energy conservation point of view we are looking for fuel consumption reduction and we to install the regenerator in the GT. Now if any one has the idea of regenerator calculation and how much fuel gas can be reduced, it will be support us.