Centrifugal compressor with bleed flow splitter for a gas turbine engine

An impeller includes a plurality of vanes formed around a hub, each of the plurality of vanes defines an offset between a leading edge and a trailing edge.

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Bibliographische Detailangaben
Hauptverfasser: SANTELER KEITH A, WAGNER JOEL H, MAGGE SHANKAR S
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:An impeller includes a plurality of vanes formed around a hub, each of the plurality of vanes defines an offset between a leading edge and a trailing edge.