INTER-TURBINE BURNER IN RECUPERATION CYCLE ENGINE
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United States of America Patent
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Issued Date -
Jan 23, 2025
app pub date -
Oct 3, 2024
filing date -
Oct 3, 2024
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Abstract
A turbine engine assembly an inter-turbine burner that is disposed between at least two of a plurality of turbine stages where an additional amount of fuel is mixed with an exhaust gas flow to generate a reheated gas flow. A condenser extracts water from the reheated gas flow and an evaporator system generates a steam flow from at least a portion of water that is extracted by the condenser for injection into the core airflow.
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