发明名称 |
Sistema turbo compressor para motor de combustão interna compreendendo duas unidades turbo serialmente localizadas com seus eixos geométricos de rotação essencialemte concêntricos |
摘要 |
<p>A turbocharger system for an internal combustion engine having at least one exhaust line for evacuating exhaust gases from the combustion chamber of the engine and at least one inlet line for supplying air to the combustion chamber. A high-pressure turbine interacts with a high-pressure compressor forming a high-pressure turbo unit with a common rotation axis. A low-pressure turbine interacts with a low-pressure compressor forming a low-pressure turbo unit with a common rotation axis. The high-pressure turbo unit and the low-pressure turbo unit are serially placed with the rotation axes essentially concentric and with the high-pressure turbine and the low-pressure turbine placed adjacent to each other and coupled together by an intermediate piece configured as a flow duct. The low-pressure turbo unit ( 22 ) is attached to one part of the internal combustion engine, while the high-pressure turbo unit is attached to another part of the engine.</p> |
申请公布号 |
BRPI0410005(B1) |
申请公布日期 |
2015.05.26 |
申请号 |
BR2004PI10005 |
申请日期 |
2004.05.11 |
申请人 |
VOLVO LASTVAGNAR AB |
发明人 |
GOBERT;ULRICH;SUNDIN;LARS;ISING;MAGNUS;GRUNDITZ;DANIEL;ANDERSSON;PER;GISELMO;KENT;KRAUSCHE;SEBASTIAN |
分类号 |
F02B37/013;F02B29/04 |
主分类号 |
F02B37/013 |
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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