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公开(公告)号：US07121788B2
公开(公告)日：2006-10-17
申请号：US10524882
申请日：2003-08-09
申请人： Helmut Daudel , Helmut Finger , Peter Fledersbacher , Hans-Josef Hemer , Ralf Koch , Stephan Schenkel , Siegfried Sumser
发明人： Helmut Daudel , Helmut Finger , Peter Fledersbacher , Hans-Josef Hemer , Ralf Koch , Stephan Schenkel , Siegfried Sumser
CPC分类号： F01D17/165 , F05D2220/40 , F05D2250/311 , F05D2250/41
摘要： An exhaust gas turbocharger for an internal combustion engine comprises a turbine in the exhaust line and a compressor, which is driven by the turbine and which is located inside the intake tract of the internal combustion engine. The turbine comprises a flow duct having a radial flow entrance cross-section, and a flow ring is provided that delimits the flow entrance cross-section. An adjustable vane is placed in the radial flow entrance cross-section for variably adjusting this flow entrance cross-section. The flow ring inside the housing of the exhaust gas turbine can be axially displaced between a contact position toward the vane and a position that frees a gap toward the vane.
摘要翻译： 用于内燃机的排气涡轮增压器包括排气管中的涡轮机和由涡轮驱动并位于内燃机的进气道内部的压缩机。 涡轮机包括具有径向流入口横截面的流动管道，并且提供限定流入口横截面的流动环。 可调节的叶片放置在径向流入口横截面中，用于可变地调节该流入口横截面。 排气涡轮机的壳体内的流动环可以在朝向叶片的接触位置和将间隙释放到叶片上的位置之间轴向移动。
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公开(公告)号：US06739134B2
公开(公告)日：2004-05-25
申请号：US10311128
申请日：2003-04-11
申请人： Peter Fledersbacher , Siegfried Sumser , Paul Loeffler , Helmut Finger , Hans-Josef Hemer , Ralf Koch
发明人： Peter Fledersbacher , Siegfried Sumser , Paul Loeffler , Helmut Finger , Hans-Josef Hemer , Ralf Koch
IPC分类号： F02D2300
CPC分类号： F01D17/165 , F02B37/025 , F02B37/24 , F05D2220/30 , F05D2220/40 , Y02T10/144
摘要： An exhaust-gas turbocharger for an internal combustion engine has a turbine in the exhaust-gas tract and a compressor, driven by the turbine, in the intake tract, the turbine having a flow channel with a radial flow-inlet cross-section and a semi-axial flow-inlet cross-section, and a flow ring being provided which limits the two flow-inlet cross-sections. The turbine is furnished with variable turbine geometry for the changeable adjustment of the flow-inlet cross-section. To improve efficiency, the position of the flow ring in the housing of the exhaust-gas turbocharger is variably adjustable.
摘要翻译： 用于内燃机的废气涡轮增压器具有排气管道中的涡轮机和由涡轮机驱动的进气道中的压缩机，涡轮机具有具有径向流入口横截面的流动通道和 半轴流入口横截面，以及限定两个流入口横截面的流动环。 涡轮机配备有可变的涡轮机几何形状，用于流入口横截面的可变调节。 为了提高效率，排气涡轮增压器的壳体中的流动环的位置是可变的。
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公开(公告)号：US20050268610A1
公开(公告)日：2005-12-08
申请号：US10524882
申请日：2003-08-09
申请人： Helmut Daudel , Helmut Finger , Peter Fledersbacher , Hans-Josef Hemer , Ralf Koch , Stephan Schenkel , Siegfried Sumser
发明人： Helmut Daudel , Helmut Finger , Peter Fledersbacher , Hans-Josef Hemer , Ralf Koch , Stephan Schenkel , Siegfried Sumser
CPC分类号： F01D17/165 , F05D2220/40 , F05D2250/311 , F05D2250/41
摘要： An exhaust gas turbocharger for an internal combustion engine comprises a turbine in the exhaust line and a compressor, which is driven by the turbine and which is located inside the intake tract of the internal combustion engine. The turbine comprises a flow duct having a radial flow entrance cross-section, and a flow ring is provided that delimits the flow entrance cross-section. An adjustable vane is placed in the radial flow entrance cross-section for variably adjusting this flow entrance cross-section. The flow ring inside the housing of the exhaust gas turbine can be axially displaced between a contact position toward the vane and a position that frees a gap toward the vane.
摘要翻译： 用于内燃机的排气涡轮增压器包括排气管中的涡轮机和由涡轮驱动并位于内燃机的进气道内部的压缩机。 涡轮机包括具有径向流入口横截面的流动管道，并且设置限定流入口横截面的流动环。 可调节的叶片放置在径向流入口横截面中，用于可变地调节该流入口横截面。 排气涡轮机的壳体内的流动环可以在朝向叶片的接触位置和将间隙释放到叶片上的位置之间轴向移动。
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4.发明授权公开(公告)号：US07021057B2
公开(公告)日：2006-04-04
申请号：US10401278
申请日：2003-03-27
CPC分类号： F01D17/165 , F02B37/025 , F02C6/12 , Y02T10/144
摘要： In an exhaust gas turbocharger for an internal combustion engine comprising a radial flow exhaust gas turbine and a compressor, which is connected to the turbine via a shaft, the turbine having a radial inflow duct and a radial inlet flow passage, which leads to the turbine wheel and in which a variable geometry vane structure for changing the cross-section of the radial inlet flow passage is supported between two support walls fixed to the turbine casing, one of the support walls projects into the inflow duct, in such a manner that the rear side of this support wall is spaced from the inner wall of the inflow duct wall so that the exhaust gas within the inflow duct is in contact also with the rear side of this support wall.
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5.发明申请公开(公告)号：US20050091978A1
公开(公告)日：2005-05-05
申请号：US10988406
申请日：2004-11-10
IPC分类号： F01D17/16 , F02B37/04 , F02B37/24 , F02B39/10 , F02C6/12 , F02M25/07 , F04D25/02 , F04D25/04 , F02B33/44
CPC分类号： F02B39/10 , F01D17/16 , F02B29/0406 , F02B37/025 , F02B37/04 , F02B37/24 , F02C6/12 , F02M26/05 , F02M26/10 , F02M26/28 , F04D25/022 , F04D25/04 , Y02T10/144
摘要： In a variable exhaust gas turbocharger for an internal combustion engine including an exhaust gas turbocharger to which exhaust gas is supplied from the engine to provide a torque for driving the turbocharger, an additional device is provided which includes an electrical or mechanical drive for supplying an additional torque to the exhaust gas turbocharger in order to maintain the exhaust gas turbocharger at a certain speed at which it is capable of generating a desired inlet air pressure for the charge air supplied to the internal combustion engine.
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公开(公告)号：US06467454B1
公开(公告)日：2002-10-22
申请号：US09597495
申请日：2000-06-21
IPC分类号： F02B3100
CPC分类号： F02B31/085 , F02B17/005 , F02B29/0412 , F02B37/00 , F02B2275/16 , F02B2275/48 , Y02T10/123 , Y02T10/125 , Y02T10/144 , Y02T10/146
摘要： For a spark ignited internal combustion engine having at least two inlet valves per cylinder each with a separate inlet passage and with a fuel injection device which injects fuel directly into the cylinder. An air charger for generating an air charge into one of the inlet passages and a connecting duct extending between the two inlet passages with a selectively opened and closed regulating device therein to apportion the flow of charge air through the separate inlet passages.
摘要翻译： 对于具有每个气缸的至少两个入口阀的火花点火内燃机，每个具有单独的入口通道和具有将燃料直接喷射到气缸中的燃料喷射装置。 一种空气充电器，用于将空气充入一个入口通道和一个在两个入口通道之间延伸的连接管道，其中选择性地打开和关闭调节装置，以分配通过分开的入口通道的增压空气流。
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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。
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公开(公告)号：US20070180825A1
公开(公告)日：2007-08-09
申请号：US11704707
申请日：2007-02-09
CPC分类号： F02B37/24 , F01D17/165 , F02B29/0437 , F02M26/05 , F02M26/28 , F05D2220/40 , F05D2250/41 , F05D2260/30 , Y02T10/144 , Y02T10/146
摘要： In an exhaust gas turbocharger for an internal combustion engine including an exhaust gas turbine in the exhaust line and a compressor in the intake tract of the internal combustion engine, and the exhaust gas turbine includes a gas inlet passage with a variable guide vane structure supported on one side of a support ring arranged in the inlet flow passage to the turbine wheel, the support ring is mounted in a floating manner such that the side thereof, which faces away form the guide vanes is exposed to the gas pressure in the inlet flow passage in order to bias the support ring toward the opposite inlet flow passage wall and spacer sleeves with expansion properties similar to those of the guide vanes are provided between the support ring and the opposite flow passage wall for delimiting the clearance between the guide vanes and the opposite flow passage wall.
摘要翻译： 在一种用于内燃机的排气涡轮增压器中，该排气涡轮增压器包括排气管中的废气涡轮机和内燃机的进气道中的压缩机，并且该排气涡轮机包括一个气体入口通道， 支撑环的一侧布置在到涡轮机叶轮的入口流动通道中，支撑环以浮动方式安装，使得其背离导叶的侧面暴露于入口流动通道中的气体压力 为了将支撑环偏压到相对的入口流动通道壁，并且具有类似于导向叶片的膨胀特性的间隔套筒设置在支撑环和相对的流动通道壁之间，用于限定导向叶片和相对的导向叶片之间的间隙 流道壁。
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公开(公告)号：US20070044470A1
公开(公告)日：2007-03-01
申请号：US11518545
申请日：2006-09-08
申请人： Siegfried Sumser , Peter Fledersbacher , Helmut Finger , Paul Loffler , Manfred Stute , Klaus Rossler
发明人： Siegfried Sumser , Peter Fledersbacher , Helmut Finger , Paul Loffler , Manfred Stute , Klaus Rossler
CPC分类号： F02B39/10 , F02B29/0406 , F02B37/04 , F02B37/16 , F02B37/183 , F02B37/24 , F02M26/08 , F02M26/23 , F04D25/0606 , F04D25/0653 , F04D27/0253 , F04D29/681 , F05D2220/40 , Y02T10/144
摘要： In an internal combustion engine and a method of operating the engine which comprises a compressor having an impeller disposed in a housing including a main inlet duct in which the impeller is supported and an additional inlet duct joining the main inlet duct in the area of the compressor impeller, and valving means for controlling the gas supply to the inlet ducts and an electric motor connected to the compressor impeller for rotation therewith so that the compressor is operable by the electric motor and by the pressure drop in the air intake line of the engine, a flywheel is coupled to the impeller for storing rotational energy when the impeller is driven by the intake gas and returning the energy to the impeller when the pressure drop collapses upon a sudden increase in the demand for engine power.
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公开(公告)号：US20050056015A1
公开(公告)日：2005-03-17
申请号：US10946375
申请日：2004-09-21
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。
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