Turbocharger with a high diffusion turbine wheel

A turbocharger including a turbine wheel having a hub-to-tip ratio of no more than 60% and blades with a high turning angle, a turbine housing forming an inwardly spiraling primary-scroll passageway that significantly converges to produce highly accelerated airflow into the turbine at high circumfer...

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Bibliographic Details
Main Authors Elliott, Thomas J, Kares, Vaclav
Format Patent
LanguageEnglish
French
German
Published 21.12.2016
Subjects
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Summary:A turbocharger including a turbine wheel having a hub-to-tip ratio of no more than 60% and blades with a high turning angle, a turbine housing forming an inwardly spiraling primary-scroll passageway that significantly converges to produce highly accelerated airflow into the turbine at high circumferential angles, and a two-sided parallel compressor. The compressor and turbine each produce substantially no axial force, allowing the use of minimal axial thrust bearings.
Bibliography:Application Number: EP20110160541