Turbocharger and guide gate therefor and stopper of the guide gate

A turbocharger (1) with variable turbine geometry (VTG), having a blade bearing ring (6), which has a multiplicity of guide blades (7), and which has a stop (25) at least for adjusting the minimum throughflow through the nozzle cross sections formed by the guide blades (7), wherein the stop (25) has...

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Bibliographische Detailangaben
Hauptverfasser:	RAMB THOMAS, HEIDINGSFELDER LEIF
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL ENGINE PLANTS IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES 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:	A turbocharger (1) with variable turbine geometry (VTG), having a blade bearing ring (6), which has a multiplicity of guide blades (7), and which has a stop (25) at least for adjusting the minimum throughflow through the nozzle cross sections formed by the guide blades (7), wherein the stop (25) has a fixing peg (32) on which a deformable, arched adjusting section (26) is arranged. Since the stop is formed as a deformable component which can be fixed in the guide grate, it is possible after the assembly of the guide grate to rework said stop in a simple manner in order to precisely set the required stop position, since said stop is not integrally connected to the guide grate.