CPC F01K 11/02 (2013.01) [F01K 7/223 (2013.01); F01K 15/02 (2013.01); F05D 2220/72 (2013.01)] | 16 Claims |
1. A turbine engine assembly comprising:
a core engine generating an exhaust gas flow, the core engine including a compressor where inlet airflow is compressed and communicated to a combustor where the compressed airflow is mixed with fuel and ignited to generate the exhaust gas flow that is expanded through the turbine section;
a condenser where water is extracted from the exhaust gas flow;
an evaporator disposed within an exhaust gas flow path where heat is input into the water extracted by the condenser without superheat to generate a first steam flow;
a steam turbine where the first steam flow is expanded and cooled; and
a superheater disposed within the exhaust gas flow path where additional heat is input into the first steam flow exhausted from the steam turbine to generate a second steam flow, wherein the second steam flow is injected into a core flow path of the core engine wherein the exhaust gas flow is communicated through the superheater before being communicated through the evaporator.
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