CPC F02C 9/40 (2013.01) [F02C 3/06 (2013.01); F02C 7/22 (2013.01)] | 16 Claims |
14. A method of intercooling a core airflow of a turbine engine comprising:
communicating a portion of a water flow to an intercooling system disposed within a compressor section of the turbine engine;
cooling the core airflow with the portion of the water flow by placing the core airflow and the portion of the water flow into thermal communication in the intercooling system resulting in a heated water flow;
communicating h heated water flow from the intercooling system to an evaporator aft of a combustor of the turbine engine to generate a steam flow; and
injecting the steam flow into the combustor.
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