发明名称 |
Sector-Divided Turbine Assembly With Axial Piston Variable-Geometry Mechanism |
摘要 |
A turbine ( 40 ) for a turbocharger ( 10 ) has a turbine housing ( 41 ) defining a generally annular chamber ( 43 ) surrounding a turbine wheel ( 44 ), the chamber receiving exhaust gas for driving the turbine wheel. The chamber has dividing walls ( 46 ) that divide the chamber into a plurality of angular sectors ( 43 a, 43 b), each fed with exhaust gas separately from the other sector(s). ( 52,53 ) located radially inwardly of the sectors for guiding flow into the turbine wheel include at least dividing vanes ( 52 ) that form extensions of the dividing walls ( 46 ) so as to extend the sector-division of the exhaust gas flow path all the way to the trailing edges of the dividing vanes. An axially slidable piston ( 48 ) is disposed radially inwardly of the sectors, and radially overlaps with the dividing vanes ( 52 ). The vanes either are mounted on fixed structure and are received in slots ( 49 ) in the piston, or are mounted on the piston and received in slots in fixed structure.
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申请公布号 |
US2008038110(A1) |
申请公布日期 |
2008.02.14 |
申请号 |
US20030576663 |
申请日期 |
2003.10.24 |
申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
ROBERTS QUENTIN;BERNARDINI LUCIANO;LOMBARD ALAIN;PETITJEAN DOMINIQUE;LOTTERMAN JEFF |
分类号 |
F01D9/02;F01D17/14;F01D17/16 |
主分类号 |
F01D9/02 |
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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