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：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。

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：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：US5943864A

公开(公告)日：1999-08-31

申请号：US851242

申请日：1997-05-05

申请人： Siegfried Sumser ,  Erwin Schmidt ,  Helmut Finger ,  Hong Son Truong

发明人： Siegfried Sumser ,  Erwin Schmidt ,  Helmut Finger ,  Hong Son Truong

IPC分类号： F01D17/14 ,  F02B37/18 ,  F02M25/07

CPC分类号： F02B37/183 ,  F01D17/148 ,  F02B37/025 ,  F02B29/0406 ,  F02M26/05 ,  F02M26/09 ,  F02M26/37 ,  F02M26/40 ,  F05D2220/40 ,  Y02T10/144

摘要： In an exhaust gas turbocharger for an internal combustion engine with a turbine casing including a turbine inlet structure with two flow passages separated by a partition, a turbine control valve is arranged in the partition and is in communication with a turbine bypass flow passage, which is disposed in the partition and extends to the turbine outlet for discharging exhaust gases from at least one of the two turbine inlet flow passages to the turbine outlet under the control of the turbine bypass valve.

摘要翻译： 在具有涡轮机壳体的涡轮机壳体的排气涡轮增压器中，所述涡轮机壳体包括具有由隔板隔开的两个流动通道的涡轮机入口结构，涡轮机控制阀设置在分隔件中，并与涡轮机旁通流路连通， 设置在隔板中并延伸到涡轮机出口，用于在涡轮旁通阀的控制下将废气从两个涡轮机入口流动通道中的至少一个排出到涡轮机出口。

公开(公告)号：US5910000A

公开(公告)日：1999-06-08

申请号：US962900

申请日：1997-11-03

申请人： Marco Schade ,  Erwin Schmidt ,  Siegfried Sumser

发明人： Marco Schade ,  Erwin Schmidt ,  Siegfried Sumser

IPC分类号： F01D17/14 ,  F01D17/16 ,  F01D1/08

CPC分类号： F01D17/167 ,  F01D17/141

摘要： In an exhaust gas turbocharger turbine for an internal combustion engine with a turbine housing having an annular flow path, a control sleeve axially movably supported in an annular space formed in the turbine housing adjacent the annular flow path and having at its front end a flow guide structure with vanes for guiding the exhaust gas flow when the flow guide structure is disposed in the annular flow path, a ring is disposed at the front end of the control sleeve in front of the flow guide structure such that the annular space is covered and sealed when the control sleeve is fully retracted into the annular space whereby flow losses are substantially reduced.

摘要翻译： 在具有涡轮壳体具有环形流动通道的内燃机的排气涡轮增压器涡轮机中，控制套筒可轴向移动地支撑在邻近环形流动通道形成在涡轮机壳体中的环形空间中，并且在其前端处具有流动导向件 具有用于当流动引导结构设置在环形流动路径中时用于引导排气流动的叶片的结构，在流动引导结构前面的控制套筒的前端设置有环，使得环形空间被覆盖和密封 当控制套筒完全缩回到环形空间中时，流量损失显着减小。