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    TURBO COMPRESSOR SYSTEM FOR INTERNAL COMBUSTION ENGINE COMPRISING TWO SERIALLY PLACED TURBO UNITS WITH THEIR ROTATION AXES ESSENTIALLY CONCENTRIC
    9.
    发明申请
    TURBO COMPRESSOR SYSTEM FOR INTERNAL COMBUSTION ENGINE COMPRISING TWO SERIALLY PLACED TURBO UNITS WITH THEIR ROTATION AXES ESSENTIALLY CONCENTRIC 有权
    用于内燃机的涡轮压缩机系统，包括两个串联的涡轮机组，其旋转轴基本上集中

    公开(公告)号：US20060123786A1

    公开(公告)日：2006-06-15

    申请号：US11164236

    申请日：2005-11-15

    申请人： Ulrich Gobert ,  Lars Sundin ,  Magnus Ising ,  Daniel Grunditz ,  Per Andersson ,  Kent Giselmo ,  Sebastian Krausche

    发明人： Ulrich Gobert ,  Lars Sundin ,  Magnus Ising ,  Daniel Grunditz ,  Per Andersson ,  Kent Giselmo ,  Sebastian Krausche

    IPC分类号： F02B33/44

    CPC分类号： F02B37/013 ,  F01N13/107 ,  F02B29/04 ,  F02B37/004 ,  F02B37/025 ,  F05B2220/40 ,  F05B2250/311 ,  Y02T10/144

    摘要： A turbocharger system for an internal combustion engine (10) having at least one exhaust line (15, 16) for evacuating exhaust gases from the combustion chamber (11) of the engine and at least one inlet line (12) for supplying air to the combustion chamber. A high-pressure turbine (17) interacts with a high-pressure compressor (19) and hereupon forms a high-pressure turbo unit (18) with a common rotation axis. A low-pressure turbine (21) interacts with a low-pressure compressor (23) and hereupon forms a low-pressure turbo unit (22) with a common rotation axis, for extracting energy from the exhaust flow of the engine and pressurizing the inlet air of the engine. The low-pressure turbine (21) is of the axial type. 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 (17) and the low-pressure turbine (21) placed adjacent to each other and coupled together by an intermediate piece configured as a flow duct. This is arranged to allow a certain eccentricity between the two rotation axes. The low-pressure turbo unit (22) is attached to one part of the internal combustion engine (10), while the high-pressure turbo unit (18) is attached to another part of the engine (10).

    摘要翻译： 一种用于内燃机（10）的涡轮增压器系统，具有至少一个用于从发动机的燃烧室（11）排出废气的排气管线（15,16）和至少一个入口管线（12），用于向 燃烧室。 高压涡轮机（17）与高压压缩机（19）相互作用，于是形成具有公共旋转轴线的高压涡轮机单元（18）。 低压涡轮机（21）与低压压缩机（23）相互作用，由此形成具有共同旋转轴线的低压涡轮机组件（22），用于从发动机的排气流中提取能量并对入口 发动机的空气。 低压涡轮机（21）为轴向型。 高压涡轮单元和低压涡轮单元串联放置，旋转轴基本上是同心的，并且高压涡轮机（17）和低压涡轮机（21）彼此相邻放置并且通过 构成为流路的中间件。 这被设置为允许两个旋转轴之间的一定偏心。 低压涡轮单元（22）附接到内燃机（10）的一部分，而高压涡轮单元（18）附接到发动机（10）的另一部分。