发明名称 |
Centrifugal compressor for exhaust gas turbocharger of internal combustion engine of motor vehicle, has impeller blade with trailing edge partially arranged in plane, which with axial direction has angle different from zero degree angle |
摘要 |
<p>The centrifugal compressor (10) has a compressor wheel (12) rotating around a rotational axis (18) and an impeller blade (21) that inflows air to be compacted during operation of the centrifugal compressor in an axial direction by the compressor wheel and deflects air in a radial direction. A trailing edge (25) of the impeller blade is partially arranged in a plane, which with the axial direction has an angle different from zero degree angle. The trailing edge extends to an inlet (33) of an axial diffuser (24). A cover contour is formed by extension of a hub body (19) of the compressor wheel.</p> |
申请公布号 |
DE102012019632(A1) |
申请公布日期 |
2013.03.28 |
申请号 |
DE20121019632 |
申请日期 |
2012.10.06 |
申请人 |
DAIMLER AG |
发明人 |
SUMSER, SIEGFRIED;STILLER, MICHAEL |
分类号 |
F04D29/30 |
主分类号 |
F04D29/30 |
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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