TURBOCHARGER COMPRESSOR IMPELLER WITH SERRATED LEADING EDGES

A turbocharger is disclosed. The turbocharger may comprise a turbine, and a compressor having a radial impeller. The radial impeller may include a body having a hub and a plurality of main blades extending from the hub. Each of the main blades may have a leading edge. The turbocharger may further co...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Lotz, Robert Dirk, Jenks, Gordon, Davis, Kenneth Lee, Watson, John Paul
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A turbocharger is disclosed. The turbocharger may comprise a turbine, and a compressor having a radial impeller. The radial impeller may include a body having a hub and a plurality of main blades extending from the hub. Each of the main blades may have a leading edge. The turbocharger may further comprise a plurality of serrations extending along the leading edge of each of the main blades, and a shaft interconnecting the compressor and the turbine. The body of the impeller may be formed by flank milling, and the serrations extending along the leading edges of the main blades may be formed by point milling.