Shaft and turbine wheel assembly for a turbocharger

An assembly (600) for a turbocharger (200) includes a shaft (620) with an axial extension and a shaft-side groove portion, the shaft-side groove portion defined at least in part by a radial height; a turbine wheel (660) with a counter bore and a turbine wheel-side groove portion, the turbine wheel-s...

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Bibliographische Detailangaben
Hauptverfasser:	DAVIES, PETER, VAZEILLE, NICOLAS, GENIN, EMERIC
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	An assembly (600) for a turbocharger (200) includes a shaft (620) with an axial extension and a shaft-side groove portion, the shaft-side groove portion defined at least in part by a radial height; a turbine wheel (660) with a counter bore and a turbine wheel-side groove portion, the turbine wheel-side groove portion defined at least in part by a radial height; and, upon receipt of the axial extension of the shaft by the counter bore of the turbine wheel, a groove formed by the shaft-side groove portion and the turbine wheel-side groove portion, the groove configured to seat a seal component. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.