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.
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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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. |
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