公开(公告)号：US06546728B2

公开(公告)日：2003-04-15

申请号：US09910005

申请日：2001-07-23

申请人： Erwin Schmidt ,  Siegfried Sumser

发明人： Erwin Schmidt ,  Siegfried Sumser

IPC分类号： F02D2300

CPC分类号： F02B37/24 ,  F01D17/12 ,  F01D17/165 ,  F02B29/0406 ,  F02C6/12 ,  F02D9/06 ,  F02M26/05 ,  F02M26/10 ,  F02M26/23 ,  Y02T10/144

摘要： An exhaust-gas turbocharger for an internal combustion engine has a turbine having a variable turbine geometry for the variable setting of the effective flow inlet cross section to the turbine wheel. The exhaust-gas turbocharger has a compressor which is connected to the turbine via a shaft. The variable turbine geometry can be adjusted by means of a regulating device between a closed position and an open position. To compensate for wear, a stop limiting an end position of the variable turbine geometry is provided, and the position of this stop can be set in a variable manner.

公开(公告)号：US06539716B2

公开(公告)日：2003-04-01

申请号：US09974708

申请日：2001-10-10

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

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

IPC分类号： F02B3344

CPC分类号： F02B41/10 ,  F02B29/0406 ,  F02B37/005 ,  F02B37/24 ,  F02M26/08 ,  F02M26/10 ,  F02M26/23 ,  Y02T10/144 ,  Y02T10/163

摘要： In an internal combustion engine including an exhaust gas turbocharger and a compound power turbine connected to the crankshaft of the engine and an exhaust gas recirculation system extending between the engine exhaust duct upstream of the exhaust gas turbine and the intake duct downstream of the compressor of the exhaust gas turbocharger, the exhaust gas turbine and the compound power turbine have a size relationship determined by the power absorption capability &phgr; of each turbine such that: φ = m . ⁢ T p wherein: {dot over (m)} is the exhaust gas mass flow rate through the turbine, T is the exhaust gas temperature at the turbine inlet, and p is the exhaust gas pressure at the turbine outlet and the maximal compound power turbine absorption capability exceeds the maximal absorption capability of the exhaust gas turbine.

摘要翻译： 在包括排气涡轮增压器和连接到发动机的曲轴的复合动力涡轮机的内燃机和在排气涡轮机上游的发动机排气管道和在压缩机的下游的进气管道之间延伸的废气再循环系统 废气涡轮增压器，废气涡轮机和复合动力涡轮机具有由每个涡轮机的功率吸收能力phi确定的尺寸关系，使得：其中：{dot over（m是通过涡轮机的废气质量流量，T是 涡轮机入口处的废气温度，和p是涡轮出口处的排气压力，最大复合动力涡轮机吸收能力超过排气涡轮机的最大吸收能力。

公开(公告)号：US06378305B1

公开(公告)日：2002-04-30

申请号：US09588787

申请日：2000-06-06

申请人： Siegfried Sumser ,  Werner Rumez

发明人： Siegfried Sumser ,  Werner Rumez

IPC分类号： F02D2300

CPC分类号： F02B37/24 ,  F02C6/12 ,  F02D9/06 ,  F02M26/05 ,  Y02T10/144

摘要： An internal combustion engine having an exhaust-gas turbocharger is provided. The exhaust-gas turbocharger includes a variable turbine geometry that allows for a greater range of use. The exhaust-gas turbocharger is used as a throttling device to dimension the combustion-air quantity delivered to the engine. The variable turbine geometry can be adjusted in such a way that the direction of rotation of the rotor of the exhaust-gas turbocharger is reversed. The intake pressure in the air inlet of the internal combustion engine is set as a function of the direction of rotation of the rotor.

摘要翻译： 提供具有排气涡轮增压器的内燃机。 废气涡轮增压器包括允许更大范围使用的可变涡轮几何形状。 排气涡轮增压器用作节流装置，用于确定输送到发动机的燃烧空气量。 可变涡轮机的几何形状可以使废气涡轮增压器的转子的旋转方向相反。 内燃机的进气口中的进气压力被设定为转子旋转方向的函数。

公开(公告)号：US06256991B1

公开(公告)日：2001-07-10

申请号：US09446526

申请日：1999-12-27

申请人： Erwin Schmidt ,  Siegfried Sumser

发明人： Erwin Schmidt ,  Siegfried Sumser

IPC分类号： F02D2300

CPC分类号： F02B37/24 ,  F02D9/06 ,  F02D41/0005 ,  F02D41/0007 ,  F05B2200/11 ,  Y02T10/144 ,  Y02T10/42

摘要： In a turbocharger system for internal combustion engines, the internal combustion engine has at least one combustion chamber with a variable volume and a swept volume determined by the sum of the differential volumes between the smallest and largest volumes of the combustion chambers of the internal combustion engine. The turbocharger system associated to the internal combustion engine has at least one turbine arranged in the exhaust gas pipe of the internal combustion engine and provided with a flow channel which opens via an annular jet-shaped region onto a turbine wheel. A guiding apparatus arranged in the opening region of the flow channel has a variable guiding grid with adjustable guiding blades which make it possible to obtain free flow sections of different sizes and which acts as a throttle during braking in an adjustable manner, depending on the operational parameters of the internal combustion engine, for determining the narrowest flow section in the exhaust gas pipe that leads to the turbine. The system is characterized in that at maximum braking power the relation between the free flow section A in the exhaust gas pipe that leads to the turbine, the inlet diameter D of the turbine wheel and the swept volume VH of the internal combustion engine is described by the equation (I) when the braking power supplied by the internal combustion engine during braking is at its maximum, the turbo-braking factor (TBF) being smaller than 0.0005 (5%). The internal combustion engine and the turbocharger are matched so as to supply maximum braking power with low thermal stress.

摘要翻译： 在用于内燃机的涡轮增压器系统中，内燃机具有至少一个具有可变体积的燃烧室和由内燃机的燃烧室的最小和最大容积之间的不同体积之和的总和确定的扫掠容积 。 与内燃机相关联的涡轮增压器系统具有布置在内燃机的排气管中的至少一个涡轮机，并且设置有经由环形喷射区域在涡轮机轮上打开的流动通道。 布置在流动通道的开口区域中的引导装置具有带可调引导叶片的可变引导格栅，其可以获得不同尺寸的自由流动部分，并且可以以可调整的方式在制动期间用作节流阀，这取决于操作 用于确定通向涡轮机的排气管中最窄的流动部分的内燃机的参数。 该系统的特征在于，在最大制动力下，通向涡轮机的废气管道中的自由流动部分A与涡轮机叶轮的入口直径D和内燃机的扫掠体积V H之间的关系由 在制动时由内燃机供给的制动功率处于其最大值时，涡轮制动系数（TBF）小于0.0005（5％）的公式（I）。 内燃机和涡轮增压器匹配，以提供具有低热应力的最大制动功率。

公开(公告)号：US06224333B1

公开(公告)日：2001-05-01

申请号：US09248272

申请日：1999-02-11

申请人： Paul Loeffler ,  Erwin Schmidt ,  Siegfried Sumser

发明人： Paul Loeffler ,  Erwin Schmidt ,  Siegfried Sumser

IPC分类号： F01D1716

CPC分类号： F01D17/167 ,  F01D17/143 ,  F02B37/24 ,  Y10T29/49318 ,  Y10T29/4932

摘要： An exhaust gas turbocharger for an internal-combustion engine has a turbine wheel which is arranged in a housing of the exhaust gas turbocharger and to which exhaust gas can be fed by way of a flow duct constructed in the housing. A variable baffle is provided for adjusting the flow cross-section of the flow duct. In order to equip the exhaust gas turbocharger with a braking function at low manufacturing and mounting expenditures, the baffle is movably accommodated in a matrix which is detachably held on the housing. The baffle and the matrix form an exchangeable braking module.

摘要翻译： 用于内燃机的废气涡轮增压器具有设置在排气涡轮增压器的壳体中的涡轮机叶轮，并且可以通过构造在壳体中的流动管道将废气进给到该涡轮机叶轮。 提供了可变挡板来调节流动管道的流动横截面。 为了在低制造和安装支出下为排气涡轮增压器配备制动功能，挡板可移动地容纳在可拆卸地保持在壳体上的矩阵中。 挡板和矩阵形成可更换的制动模块。

公开(公告)号：US06220032B1

公开(公告)日：2001-04-24

申请号：US09406847

申请日：1999-09-29

申请人： Erwin Schmidt ,  Siegfried Sumser

发明人： Erwin Schmidt ,  Siegfried Sumser

IPC分类号： F02D2300

CPC分类号： F02D9/06

摘要： In an engine braking operation for a supercharged internal-combustion engine which has an exhaust gas turbocharger having a turbine with a variable turbine geometry, the turbine geometry is adjusted between a ram position to reduce the effective turbine cross-section and an opening position to open the effective turbine cross-section. In order to influence the action of the engine brake simply, such that a braking is adapted to different situations, the variable turbine geometry is adjusted between a definable hard braking adjustment and a definable soft braking adjustment. The hard braking adjustment is situated between the ram position and a drive starting position assigned to the fired drive operating mode. The soft braking adjustment is situated between the drive starting position and the opening position. The hard braking adjustment is selected so that the engine braking power is higher than in the soft braking adjustment.

摘要翻译： 在具有具有可变涡轮机几何形状的涡轮机的排气涡轮增压器的增压内燃机的发动机制动操作中，涡轮几何形状在压头位置之间调整以减小有效的涡轮横截面和打开位置以打开 有效的涡轮横截面。 为了简单地影响发动机制动器的作用，使得制动适应于不同的情况，可变涡轮机几何形状在可定义的硬制动调节和可定义的软制动调节之间进行调节。 硬制动调节位于推动位置和分配给燃烧驱动器操作模式的驱动器起始位置之间。 软制动调节位于驱动开始位置和打开位置之间。 选择硬制动调整，使得发动机制动功率高于软制动调整中的制动功率。

公开(公告)号：US06216459B1

公开(公告)日：2001-04-17

申请号：US09459243

申请日：1999-12-10

申请人： Helmut Daudel ,  Helmut Finger ,  Erwin Schmidt ,  Siegfried Sumser

发明人： Helmut Daudel ,  Helmut Finger ,  Erwin Schmidt ,  Siegfried Sumser

IPC分类号： F02M2507

CPC分类号： F02B37/025 ,  F02B37/007 ,  F02B37/18 ,  F02B37/183 ,  F02C3/32 ,  F02C3/34 ,  F02C6/12 ,  F02D9/06 ,  F02M26/05 ,  F02M26/10 ,  F02M26/25 ,  F02M26/34 ,  F02M26/38 ,  F02M26/42 ,  Y02T10/144

摘要： In an exhaust gas re-circulation arrangement for a supercharged internal combustion engine including an exhaust gas turbocharger with an exhaust gas turbine and a compressor, first and second exhaust pipes extending from the engine separately to the exhaust gas turbine, a charge air duct extending from the compressor to the engine and an exhaust gas recirculation line extending from one of the exhaust pipes upstream of the exhaust gas turbine to the charge air duct downstream of the compressor, the exhaust gas turbine has two turbine inlet flow passages, which provide for different flow volumes and to each of which one of the exhaust pipes is connected and a control arrangement is provided for controlling the exhaust gas flow through the turbine inlet flow passages so as to control the pressure in the exhaust gas re-circulation line to be higher than in the charge air intake duct.

摘要翻译： 在包括具有废气涡轮机的排气涡轮增压器和压缩机的增压内燃机的废气再循环装置中，从发动机分别向排气涡轮机延伸的第一和第二排气管， 发动机的压缩机和从排气涡轮机上游的排气管之一延伸到压缩机下游的增压空气管道的废气再循环管线，排气涡轮机具有两个涡轮机入口流动通道，其提供不同的流量 排放管中的一个连接到排气管中，并且设置有控制装置，用于控制通过涡轮机入口流动通道的废气流，从而将废气再循环管线中的压力控制在高于 增压进气管。

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。

公开(公告)号：US06050093A

公开(公告)日：2000-04-18

申请号：US74101

申请日：1998-05-07

申请人： Helmut Daudel ,  Siegfried Sumser

发明人： Helmut Daudel ,  Siegfried Sumser

IPC分类号： F02B37/24 ,  F02D41/00 ,  F02D23/00

CPC分类号： F02D41/0007 ,  F02B37/24 ,  F02D2041/1433 ,  Y02T10/144

摘要： In a method and apparatus for controlling a supercharged internal combustion engine including an exhaust gas turbocharger having variable turbine inlet vanes, an engine control unit includes an engine performance graph with control parameters for a multitude of engine operating points compressor performance graph is also recorded in the engine performance which represents for various exhaust gas turbocharger speeds a particular relationship between mass flow through the compressor and total pressure ratio. A multitude of engine operating curves for constant turbine guide vane positions and constant engine speeds for various engine loads and engine operating modes are also recorded and retrieved by the engine control unit for controlling the engine depending on desired engine load and engine speed for adjusting the turbine inlet vanes.

摘要翻译： 在用于控制包括具有可变涡轮机入口叶片的排气涡轮增压器的增压内燃机的方法和装置中，发动机控制单元包括具有用于多个发动机工作点的控制参数的发动机性能曲线图，压缩机性能图也记录在 代表各种废气涡轮增压器的发动机性能加速了通过压缩机的质量流量与总压力比之间的特定关系。 用于各种发动机负载和发动机操作模式的恒定涡轮引导叶片位置和恒定发动机速度的多个发动机操作曲线也由发动机控制单元记录和回收，用于根据期望的发动机负载和用于调节涡轮机的发动机转速来控制发动机 入口叶片。

公开(公告)号：US6020652A

公开(公告)日：2000-02-01

申请号：US161473

申请日：1998-09-28

申请人： Helmut Daudel ,  Peter Renninger ,  Siegfried Sumser

发明人： Helmut Daudel ,  Peter Renninger ,  Siegfried Sumser

IPC分类号： F02B37/24 ,  F02B41/10 ,  F02D9/06 ,  B60L11/02 ,  B61C9/38

CPC分类号： F02B37/24 ,  F02B41/10 ,  F02D9/06 ,  Y02T10/144 ,  Y02T10/163

摘要： In the engine braking operation of supercharged internal combustion engines, the braking power is generated by backing-up the exhaust gas before it enters an exhaust gas turbine of an exhaust gas turbocharger from an actuator in the exhaust gas duct. In order to make it possible to control the braking power within the operating limits of the exhaust gas turbocharger, the actual value and a maximum value of the turbine inlet pressure within the operating limits of the exhaust gas turbo supercharger are inferred from a performance graph of the internal combustion engine, which performance graph includes an electronically stored compressor performance graph of the supercharged air compressor which represents the relationship between mass throughput and total pressure ratio of the compressor and in which a plurality of engine operating lines for certain actuator positions and certain engine speeds as well as for a constant turbine inlet pressure are recorded. The maximum value arises as a function of the engine speed from a characteristic rotational speed line stored in the performance graph. Corresponding to the desired braking power, a nominal value which, together with the actual value of the turbine inlet pressure, serves in the control circuit as an inlet parameter for an engine controller for a comparison of nominal and actual values, is determined proportionally from the maximum value.

摘要翻译： 在增压内燃机的发动机制动操作中，通过在废气管道中的致动器进入废气涡轮增压器的废气涡轮机之前将排气备份，来产生制动功率。 为了能够在排气涡轮增压器的运行极限内控制制动功率，可以从排气涡轮增压器的运行极限内的涡轮机入口压力的实际值和最大值根据 内燃机，该性能图包括增压空气压缩机的电子存储的压缩机性能曲线图，其表示压缩机的质量吞吐量和总压力比之间的关系，并且其中用于某些致动器位置的多个发动机操作线和某些发动机 记录速度以及恒定的涡轮机入口压力。 根据存储在性能图中的特征转速线，发动机转速的函数产生最大值。 对应于期望的制动功率，将额定值与涡轮进口压力的实际值一起用于控制电路中，作为用于比较标称值和实际值的发动机控制器的入口参数，从 最大值。