发明名称 Axial turbine wheel
摘要 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.
申请公布号 EP2378099(B1) 申请公布日期 2016.06.15
申请号 EP20110161576 申请日期 2011.04.07
申请人 HONEYWELL INTERNATIONAL INC. 发明人 KARES, VACLAV;LOTTERMAN, JEFFREY A.
分类号 F02C6/12;F01D5/02;F01D5/14 主分类号 F02C6/12
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