A PULSE-SEPARATED AXIAL TURBINE STAGE WITH RADIAL-AXIAL INLET GUIDE VANES

A turbocharger with at least one axial turbine stage. Separate circumferential sections of the turbine are fed by separate exhaust system runners. The turbine is designed to harness pulse energy. Corresponding engine having cylinders comprising such a turbocharger. L'invention concerne un turbo...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	KROEGER, Georg, SILLER, Ulrich, BIESINGER, Thomas, KARSTADT, Sascha
Format:	Patent
Sprache:	eng ; fre
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A turbocharger with at least one axial turbine stage. Separate circumferential sections of the turbine are fed by separate exhaust system runners. The turbine is designed to harness pulse energy. Corresponding engine having cylinders comprising such a turbocharger. L'invention concerne un turbocompresseur comprenant au moins un étage de turbine axiale. Des sections circonférentielles séparées de la turbine sont alimentées par des conduits séparés de systèmes d'échappement. La turbine est conçue pour exploiter l'énergie d'impulsion. L'invention concerne également un moteur correspondant ayant des cylindres comprenant un tel turbocompresseur.