GAS TURBINE ENGINE WITH POWER DENSITY RANGE
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United States of America Patent
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Issued Date -
Dec 22, 2022
app pub date -
Apr 27, 2022
filing date -
Apr 27, 2022
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Abstract
A gas turbine engine includes a propulsor section including a propulsor, a compressor section including a low pressure compressor and a high pressure compressor, a geared architecture, a turbine section including a low pressure turbine and a high pressure turbine, and a power density of greater than or equal to 4.75 and less than or equal to 5.5 lbf/in3, wherein the power density is a ratio of a thrust provided by the engine to a volume of the turbine section.
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