THERMAL COMPRESSION REHEATING CYCLE
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United States of America Patent
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Issued Date -
Jul 18, 2024
app pub date -
Jan 16, 2023
filing date -
Jan 16, 2023
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Abstract
A disclosed turbine engine assembly includes a core engine assembly generating an exhaust gas flow and a thermal compressor where the exhaust gas flow from the core engine is received and compressed. The thermal compressor includes a converging duct that recompresses the exhaust gas flow that is mixed with fuel in a secondary combustor and ignited to generate a reheated gas flow.
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