TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER

A turbine engine having a rotor rotatable about a rotational axis, a stator, a plurality of circumferentially spaced bleed air passages, and an inducer. The plurality of circumferentially spaced bleed air passages being located between an axially adjacent set of vanes of the stator and blades of the...

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Bibliographische Detailangaben
Hauptverfasser: Guijarro Valencia, Antonio, Johnson, Steven Douglas, Schimmels, Scott Alan
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A turbine engine having a rotor rotatable about a rotational axis, a stator, a plurality of circumferentially spaced bleed air passages, and an inducer. The plurality of circumferentially spaced bleed air passages being located between an axially adjacent set of vanes of the stator and blades of the rotor. The inducer including a nozzle passage fluidly coupling a nozzle inlet of the inducer to a nozzle outlet of the inducer.