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. 公开了种具有至少个轴流式涡轮机级的涡轮增压器。涡轮机的分离的周向区段...

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Bibliographische Detailangaben
Hauptverfasser:	BIESINGER THOMAS, SILLER ULRICH, KROEGER GEORG, KARSTADT SASCHA
Format:	Patent
Sprache:	chi ; 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 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. 公开了种具有至少个轴流式涡轮机级的涡轮增压器。涡轮机的分离的周向区段由分离的排气系统流道实现供给。涡轮机是设计成对脉冲能量加以利用。