Aircraft engine having two radially offset turbines
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United States of America Patent
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Oct 15, 2024
Grant Date -
Sep 19, 2024
app pub date -
Mar 16, 2023
filing date -
Mar 16, 2023
priority date (Note) -
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Abstract
An aircraft engine, has: a high-pressure spool having a high-pressure turbine drivingly engaged to a high-pressure compressor; and a low-pressure spool having: a first low-pressure turbine downstream of the high-pressure turbine; and a second low-pressure turbine downstream of the first low-pressure turbine, one or more of the first low-pressure turbine and the second low-pressure turbine drivingly engaged to a rotatable load, the first low-pressure turbine and the second low-pressure turbine radially offset from one another relative to a central axis of the aircraft engine.
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