COMPOUNDED TURBO POWER UNIT WITH BOOST COMBUSTOR
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United States of America Patent
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Issued Date -
May 9, 2024
app pub date -
Nov 4, 2022
filing date -
Nov 4, 2022
priority date (Note) -
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Abstract
An aircraft power system includes an internal combustion core engine where an inlet airflow is mixed with a fuel and ignited to generate shaft power and a primary gas flow, a boost combustor where a portion of the primary gas flow from the core engine is combined with fuel and ignited to generate a boosted gas flow, and a drive turbine that includes a drive output shaft wherein the boosted gas flow is expanded to generate shaft power.
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