Regulating core air bled from a turbine engine core flowpath
AssigneeRtx Corporation
InventorsDaniel B. Kupratis, Mark F. Zelesky, Michael G. McCaffrey
Life of this patent
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AssigneeRtx Corporation
InventorsDaniel B. Kupratis, Mark F. Zelesky, Michael G. McCaffrey
Estimating the term…
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.
An assembly for a turbine engine, comprising:
An assembly for a turbine engine, comprising:
An assembly for a turbine engine, comprising:
Dependencies are inferred from the claim text.