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    Compressor, in particular for an internal combustion engine
    2.
    发明授权
    Compressor, in particular for an internal combustion engine 失效
    压缩机，特别是内燃机

    公开(公告)号：US06726441B2

    公开(公告)日：2004-04-27

    申请号：US10068554

    申请日：2002-02-06

    申请人： Siegfried Sumser ,  Peter Fledersbacher ,  Wolfgang Erdmann ,  Helmut Finger ,  Friedrich Wirbeleit

    发明人： Siegfried Sumser ,  Peter Fledersbacher ,  Wolfgang Erdmann ,  Helmut Finger ,  Friedrich Wirbeleit

    IPC分类号： F04D2966

    CPC分类号： F01D1/12 ,  F04D29/4213 ,  F04D29/685 ,  F05D2220/40

    摘要： In an air compressor, particularly for an internal combustion engine, which has a compressor housing with a flow duct structure and a recirculation arrangement including a bypass structure for recirculation some of the air entering the compressor wheel, a recirculating ring is arranged in the bypass flow structure around the compressor wheel and the ring has a plurality of flow passages distributed uniformly around its circumference with inflow orifices at the radial inner end in communication with the compressor flow duct and outflow orifice at the radial outer end in communication with a by-pass flow space.

    摘要翻译： 在空气压缩机中，特别是用于内燃机，其具有具有流动管道结构的压缩机壳体和包括用于使进入压缩机叶轮的一些空气再循环的旁路结构的再循环装置，循环环设置在旁路流中 压缩机叶轮和环周围的结构具有多个在其圆周上均匀分布的流动通道，在径向内端处的流入孔与压缩机流动管道和径向外端处的流出孔连通，与旁通流 空间。

    Exhaust gas turbine of a turbocharger for an internal combustion engine
    3.
    发明授权
    Exhaust gas turbine of a turbocharger for an internal combustion engine 有权
    用于内燃机的涡轮增压器的废气涡轮

    公开(公告)号：US06314736B1

    公开(公告)日：2001-11-13

    申请号：US09558834

    申请日：2000-04-26

    申请人： Helmut Daudel ,  Wolfgang Erdmann ,  Peter Fledersbacher ,  Carsten Funke ,  Paul Löffler ,  Siegfried Sumser

    发明人： Helmut Daudel ,  Wolfgang Erdmann ,  Peter Fledersbacher ,  Carsten Funke ,  Paul Löffler ,  Siegfried Sumser

    IPC分类号： F02D2300

    CPC分类号： F01D17/16 ,  F01D11/00 ,  F01D17/165

    摘要： An exhaust gas turbine portion of a vehicle engine turbocharger is provided with at least one variable guide-blade cascade with guide blades in a nozzle opening to the turbocharger rotor for effectively changing the cross section of the exhaust flow to the rotor wherein the angle of the guide blades is selectively settable by an adjusting device. The width dimension of the gap between the ends of the guide-blade cascade and the casing wall defining the nozzle is adjustable between a substantially zero gap dimension and a maximum gap dimension.

    摘要翻译： 车辆发动机涡轮增压器的废气涡轮机部分设置有至少一个与导向叶片级联的可变导向叶片，该导向叶片在与涡轮增压器转子相关的喷嘴开口中，用于有效地改变排气流到转子的横截面，其中， 导向叶片可由调节装置选择性地设定。 引导叶片级联的端部与限定喷嘴的壳体壁之间的间隙的宽度尺寸可在基本上零间隙尺寸和最大间隙尺寸之间调节。

    Exhaust-gas turbocharger for an internal combustion engine
    4.
    发明申请
    Exhaust-gas turbocharger for an internal combustion engine 失效
    用于内燃机的排气涡轮增压器

    公开(公告)号：US20050056015A1

    公开(公告)日：2005-03-17

    申请号：US10946375

    申请日：2004-09-21

    申请人： Peter Fledersbacher ,  Siegfried Sumser ,  Helmut Finger ,  Wolfgang Erdmann

    发明人： Peter Fledersbacher ,  Siegfried Sumser ,  Helmut Finger ,  Wolfgang Erdmann

    IPC分类号： F02B37/02 ,  F01D9/02 ,  F01D17/14 ,  F01D17/16 ,  F01D25/24 ,  F02B37/22 ,  F02B39/00 ,  F02D23/00

    CPC分类号： F01D17/143 ,  F01D9/026 ,  F01D17/167 ,  F01N13/107 ,  F02B37/025 ,  F02B37/22 ,  F05D2220/40 ,  Y02T10/144

    摘要： An exhaust-gas turbocharger in an internal combustion engine having a compressor in the induction tract and an exhaust-gas turbine in the exhaust-gas line wherein the exhaust-gas turbine has at least two spiral ducts which in each case open into a radial flow inlet passage. Arranged in the radial flow inlet passage is a guide cascade ring which is disposed between two axially delimiting walls. One of the walls is designed to be axially displaceable and adapted to accommodate the vanes of the guide cascade ring. The wall is displaceable axially outward to such an extent that the vanes of the radial guide cascade ring are no longer in contact with the wall and there is a direct, unobstructed flow path to an outflow duct in the exhaust-gas turbine.

    摘要翻译： 一种在内燃机中的排气涡轮增压器，其具有在所述排气管线中的压缩机和所述排气管线中的废气涡轮机，其中所述排气涡轮机具有至少两个螺旋管道，每个所述螺旋管道在每种情况下都敞开成径向流动 入口通道。 在径向流入口通道中布置有引导级联环，其布置在两个轴向限定的壁之间。 一个壁被设计成可轴向移动并适于容纳引导级联环的叶片。 该壁可以轴向向外移动到这样的程度，使得径向引导级联环的叶片不再与壁接触，并且存在与排气涡轮机中的流出管道直接无阻碍的流动路径。

    Exhaust-gas turbocharger for an internal combustion engine
    5.
    发明授权
    Exhaust-gas turbocharger for an internal combustion engine 失效
    用于内燃机的排气涡轮增压器

    公开(公告)号：US07047739B2

    公开(公告)日：2006-05-23

    申请号：US10946375

    申请日：2004-09-21

    申请人： Peter Fledersbacher ,  Siegfried Sumser ,  Helmut Finger ,  Wolfgang Erdmann

    发明人： Peter Fledersbacher ,  Siegfried Sumser ,  Helmut Finger ,  Wolfgang Erdmann

    IPC分类号： F02D23/00 ,  F02B37/12 ,  F01D17/14 ,  F01D17/16 ,  F01D9/02

    CPC分类号： F01D17/143 ,  F01D9/026 ,  F01D17/167 ,  F01N13/107 ,  F02B37/025 ,  F02B37/22 ,  F05D2220/40 ,  Y02T10/144

    摘要： An exhaust-gas turbocharger in an internal combustion engine having a compressor in the induction tract and an exhaust-gas turbine in the exhaust-gas line wherein the exhaust-gas turbine has at least two spiral ducts which in each case open into a radial flow inlet passage. Arranged in the radial flow inlet passage is a guide cascade ring which is disposed between two axially delimiting walls. One of the walls is designed to be axially displaceable and adapted to accommodate the vanes of the guide cascade ring. The wall is displaceable axially outward to such an extent that the vanes of the radial guide cascade ring are no longer in contact with the wall and there is a direct, unobstructed flow path to an outflow duct in the exhaust-gas turbine.

    摘要翻译： 一种在内燃机中的排气涡轮增压器，其具有在所述排气管线中的压缩机和所述排气管线中的废气涡轮机，其中所述排气涡轮机具有至少两个螺旋管道，每个所述螺旋管道在每种情况下都敞开成径向流动 入口通道。 在径向流入口通道中布置有引导级联环，其布置在两个轴向限定的壁之间。 一个壁被设计成可轴向移动并适于容纳引导级联环的叶片。 该壁可以轴向向外移动到这样的程度，使得径向引导级联环的叶片不再与壁接触，并且存在与排气涡轮机中的流出管道直接无阻碍的流动路径。

    Engine-braking arrangement for an internal combustion engine with an exhaust-gas turbocharger
    8.
    发明授权
    Engine-braking arrangement for an internal combustion engine with an exhaust-gas turbocharger 有权
    具有排气涡轮增压器的内燃机的发动机制动装置

    公开(公告)号：US06223534B1

    公开(公告)日：2001-05-01

    申请号：US09370194

    申请日：1999-08-09

    申请人： Wolfgang Erdmann ,  Carsten Funke ,  Jürgen Lenz ,  Paul Löffler ,  Erwin Schmidt ,  Siegfried Sumser

    发明人： Wolfgang Erdmann ,  Carsten Funke ,  Jürgen Lenz ,  Paul Löffler ,  Erwin Schmidt ,  Siegfried Sumser

    IPC分类号： F02D2300

    CPC分类号： F02B37/025 ,  F02D9/06 ,  F02D9/16 ,  Y02T10/144

    摘要： In an engine braking arrangement for an internal combustion engine with an exhaust gas turbocharger including a turbine arranged in the engine exhaust duct and a compressor driven by the turbine and arranged in the engine intake duct, a brake valve disposed in the exhaust duct upstream of the turbine and a pressure relief line extending from the exhaust duct upstream of the turbine rotor to an area downstream of the turbine and including a stop valve, the stop valve is a rotationally adjustable rotary valve operable by an actuating device depending on the intake pressure in the intake duct.

    摘要翻译： 在具有排气涡轮增压器的内燃机的发动机制动装置中，所述排气涡轮增压器包括布置在所述发动机排气管道中的涡轮机和由所述涡轮机驱动并设置在所述发动机进气管道中的压缩机，设置在所述排气管道上游的制动阀 涡轮机和从涡轮转子上游的排气管道延伸到涡轮机下游的区域并包括截止阀的压力释放管线，该截止阀是可旋转地调节的旋转阀，其可由致动装置操作，这取决于在 进气管。

    Exhaust gas turbocharger turbine
    9.
    发明授权
    Exhaust gas turbocharger turbine 失效
    废气涡轮增压器涡轮机

    公开(公告)号：US06443696B1

    公开(公告)日：2002-09-03

    申请号：US09673329

    申请日：2000-10-12

    申请人： Wolfgang Erdmann ,  Carsten Funke ,  Thomas Hardt ,  Paul Löffler ,  Erwin Schmidt ,  Siegfried Sumser

    发明人： Wolfgang Erdmann ,  Carsten Funke ,  Thomas Hardt ,  Paul Löffler ,  Erwin Schmidt ,  Siegfried Sumser

    IPC分类号： F01D1716

    CPC分类号： F01D17/143 ,  F01D17/165 ,  F02B37/025 ,  F02B37/22 ,  F02C6/12 ,  F02D9/06

    摘要： An exhaust-gas turbocharger turbine of an internal combustion engine is provided with a spiral guide passage arranged in a turbine housing, a turbine impeller, a flow gap be ween the guide passage and the turbine impeller, and guide blades forming a guide cascade. The guide cascade with the guide blades projects axially from a support, arranged so as to be displaceable in the axial direction in the turbine housing, in such a way that the guide blades, in normal operation, are mounted in recesses of a housing wall part of the turbine housing, the recesses, in the form of a female piece, forming a mating profile shape for the guide blades. In braking operation of the internal combustion engine, the guide blades project into the flow gap during an axial displacement of the support. The device with actuation for the braking operation can be fitted as a complete module into the turbine spiral.

    摘要翻译： 内燃机的排气涡轮增压器涡轮机设置有涡轮机壳体，涡轮叶轮，引导通道和涡轮机叶轮的流动间隙以及形成引导级联的引导叶片的螺旋引导通道。 与引导叶片的引导级联从支撑件轴向突出，布置成在涡轮机壳体中沿轴向移位，使得导向叶片在正常操作中安装在壳体壁部分的凹部中 涡轮机壳体的凹部，以阴形件的形式形成用于导向叶片的配合轮廓形状。 在内燃机的制动操作中，导向叶片在支撑件的轴向位移期间突出到流动间隙中。 具有用于制动操作的致动装置可以作为完整模块装配到涡轮螺旋中。

    Radial-flow exhaust-gas turbocharger turbine
    10.
    发明授权
    Radial-flow exhaust-gas turbocharger turbine 有权
    径向排气涡轮增压器涡轮

    公开(公告)号：US6050775A

    公开(公告)日：2000-04-18

    申请号：US199455

    申请日：1998-11-25

    申请人： Wolfgang Erdmann ,  Siegfried Sumser

    发明人： Wolfgang Erdmann ,  Siegfried Sumser

    IPC分类号： F01D17/16 ,  F01B25/02

    CPC分类号： F01D17/165 ,  F05D2220/40

    摘要： A radial-flow exhaust-gas turbocharger turbine is provided with a row of adjustable guide blades which are rotatable via adjusting shafts mounted in a casing. The guide blades are each provided with sealing discs on their longitudinal sides running at right angles to the adjusting-shaft axes. The diameter of the sealing discs is a multiple of the thickness of the guide blades. The sealing discs which are located on the side remote from the adjusting shafts form bearing points for the guide blades in the casing.

    摘要翻译： 径流排气涡轮增压器涡轮机设置有一排可调导向叶片，其可通过安装在壳体中的调节轴旋转。 导向叶片在其与调节轴轴线成直角的纵向侧上设有密封盘。 密封盘的直径是导向叶片厚度的倍数。 位于远离调节轴的一侧的密封盘形成用于壳体中的引导叶片的支承点。