Compressor in particular for turbocharger

A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the fl...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	ROACH, PAUL DR
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the flow direction (F) and which includes a cut back region (19). The cut back region is locally inclined to the flow direction (F) by an angle ± of not more than 65 degrees.