Regulating core air bled from a turbine engine core flowpath
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United States of America
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Dec 31, 2024
Grant Date -
N/A
app pub date -
Dec 29, 2023
filing date -
Dec 29, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
An assembly is provided for a turbine engine. This assembly includes an engine core extending along an axis. The engine core includes a first compressor section, a second compressor section, a flowpath, a bleed port, an inner passage, an outer passage and a flow diverter. The flowpath extends longitudinally through the first compressor section and the second compressor section. The bleed port fluidly couples the flowpath to the inner passage and the outer passage in parallel. The bleed port is located longitudinally along the flowpath between the first compressor section and the second compressor section. The flow diverter is located at an inlet into the bleed port from the flowpath. The flow diverter is configured to move between a first position and a second position.
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