GAS TURBINE ENGINE WITH POWER TURBINE DRIVEN BOOST COMPRESSOR
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United States of America Patent
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Issued Date -
Jul 30, 2020
app pub date -
Jan 24, 2019
filing date -
Jan 24, 2019
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Abstract
A gas turbine engine has an output shaft, a power turbine drivingly engaged to the output shaft, a boost compressor drivingly engaged by the power turbine; and a boost compressor bleed air circuit having an inlet fluidly connected to the boost compressor and an outlet fluidly connected to the power turbine.
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