发明名称 |
Turbocharger with axial discontinuity |
摘要 |
<p>A turbocharger turbine containing a separate insert affixed within the housing. The insert is of a stamped metal configuration, and forms at least a portion of inlet passageway outer wall. An axial discontinuity is machined into the inlet passageway outer wall, the axial discontinuity being characterized by a size and location to direct airflow away from the blade-gap zone over at least part of the range of flow conditions. The inlet passageway may be either larger or smaller upstream of the axial discontinuity.</p> |
申请公布号 |
EP2292908(A2) |
申请公布日期 |
2011.03.09 |
申请号 |
EP20100168797 |
申请日期 |
2010.07.07 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
ESPASA, OLIVIER;TISSERANT, DENIS;SEVERIN, EMMANUEL;SAUSSE, LORRAIN;ABEL, FRANCIS;BARTHELET, PIERRE |
分类号 |
F02C6/12;F01D5/04;F04D29/16 |
主分类号 |
F02C6/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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