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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。
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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:US06733236B2
公开(公告)日:2004-05-11
申请号:US10176889
申请日:2002-06-21
IPC分类号: F04D2944
CPC分类号: F02B33/44 , F01D9/06 , F02B37/00 , F04D25/04 , F05D2220/40 , F05D2250/231 , F05D2250/311 , F05D2250/314 , Y02T10/144
摘要: A compressor in a turbocharger has a compressor impeller in an inflow passage and an outflow region downstream of the compressor-impeller outlet edge. The outflow region is assigned a connecting passage, a stabilizing chamber and an outflow passage, the connecting passage being arranged with a lateral offset with respect to a longitudinal center axis of the stabilizing chamber.
摘要翻译: 涡轮增压器中的压缩机具有在流入通道中的压缩机叶轮和压缩机 - 叶轮出口边缘下游的流出区域。 流出区域分配有连接通道,稳定室和流出通道,连接通道相对于稳定室的纵向中心轴线偏移地布置。
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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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公开(公告)号:US06260358B1
公开(公告)日:2001-07-17
申请号:US09551164
申请日:2000-04-17
IPC分类号: F02D2300
CPC分类号: F02D23/00 , F02B29/0406 , F02B37/02 , F02B37/22 , F02B37/24 , F02C6/12 , F02M26/05 , F02M26/10 , F02M26/23 , F02M26/43 , Y02T10/144
摘要: In a multi-cylinder internal combustion engine including an exhaust gas turbocharger to which at least two separate exhaust lines extend from different groups of cylinders of the engine, the exhaust lines have discharge openings arranged adjacent one another along a control surface area and a control slide member supported so as to be movable relative to the exhaust gas discharge openings includes wall portions movable with the slide member between a position in which the wall portions of the slide member are in alignment with stationary wall portions between the discharge openings for maintaining the exhaust gas flow passages separated from one another and a position in which the wall portions on the slide member are out of alignment with the stationary wall portions, wherein the exhaust gas lines are in communication with one another.
摘要翻译: 在包括排气涡轮增压器的多气缸内燃机中,至少两个独立的排气管线从发动机的不同气缸组延伸出来,排气管线具有沿着控制表面区域彼此相邻设置的排出口,以及控制滑块 被支撑成能够相对于排气排出口移动的构件包括可滑动构件在滑动构件的壁部与排出口之间的静止壁部对准的位置之间移动的壁部,用于维持排气 彼此分离的流动通道和滑动构件上的壁部分与固定壁部分不对准的位置,其中废气管线彼此连通。
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公开(公告)号:US06209324B1
公开(公告)日:2001-04-03
申请号:US09303435
申请日:1999-05-03
申请人: Helmut Daudel , Helmut Finger , Siegfried Sumser
发明人: Helmut Daudel , Helmut Finger , Siegfried Sumser
IPC分类号: F02B3344
CPC分类号: F02B29/0406 , F02B37/005 , F02B37/18 , F02B37/24 , F02M26/05 , F02M26/10 , F02M26/23 , F02M26/33 , F02M26/34 , Y02T10/144 , Y02T10/146
摘要: An exhaust turbocharger for an internal combustion engine has a main compressor for compressing the fresh air supplied to the engine, an additional compressor for compressing combustion gases to be recycled to the engine, and a turbine that can be driven by the exhaust gases from the engine and which serves to drive the main compressor and the additional compressor. The turbine has an adjustable geometry which facilitates optimization of engine operation regarding pollutant emissions, fuel consumption, and performance.
摘要翻译: 用于内燃机的排气涡轮增压器具有用于压缩供给发动机的新鲜空气的主压缩机,用于压缩要再循环到发动机的燃烧气体的附加压缩机,以及可由来自发动机的废气驱动的涡轮机 并且其用于驱动主压缩机和附加压缩机。 涡轮机具有可调节的几何形状,有助于优化发动机运行,以了解污染物排放,燃料消耗和性能。
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公开(公告)号:US06854272B2
公开(公告)日:2005-02-15
申请号:US10283682
申请日:2002-10-30
申请人: Helmut Finger , Lothar Lenke , Erwin Schmidt , Siegfried Sumser
发明人: Helmut Finger , Lothar Lenke , Erwin Schmidt , Siegfried Sumser
CPC分类号: F01D17/165 , F02C6/12
摘要: An exhaust gas turbocharger for an internal combustion engine, which has an exhaust gas turbine in the exhaust system and a compressor in the induction system, comprises a variable turbine geometry, associated with the turbine, for adjustably setting a radial inlet cross section for the flow to the turbine rotor. The variable turbine geometry is configured as a guide cascade ring, which has guide vanes distributed over the periphery and encompasses the turbine rotor. The minimum distance between two adjacent guide vanes obeys a specified relationship with respect to the diameter of the turbine rotor and the number of guide vanes of the guide cascade ring. In addition, a flow edge is provided on the radially inner surface of each guide vane.
摘要翻译: 一种用于内燃机的排气涡轮增压器,其在排气系统中具有排气涡轮机和在该感应系统中的压缩机,包括与该涡轮相关联的可变涡轮几何形状,用于可调节地设定该流量的径向入口横截面 到涡轮转子。 可变涡轮机几何形状被构造为引导级联环,引导级联环具有分布在周边上并包围涡轮转子的导向叶片。 两个相邻的导向叶片之间的最小距离相对于涡轮机转子的直径和引导级联环的导向叶片的数量达到规定的关系。 此外,在每个导叶的径向内表面上设置流动边缘。
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公开(公告)号:US5943864A
公开(公告)日:1999-08-31
申请号:US851242
申请日:1997-05-05
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。
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公开(公告)号:US07428813B2
公开(公告)日:2008-09-30
申请号:US11150700
申请日:2005-06-11
申请人: Helmut Finger , Erwin Schmidt , Siegfried Sumser
发明人: Helmut Finger , Erwin Schmidt , Siegfried Sumser
IPC分类号: F02D23/00 , F02B33/44 , F02M25/07 , F16K11/085
CPC分类号: F02B37/183 , F02B29/0406 , F02B37/02 , F02B37/025 , F02B37/24 , F02D9/06 , F02D9/16 , F02M26/05 , F02M26/10 , F02M26/23 , F02M26/43 , F16K11/076 , Y02T10/144 , Y10T137/86871
摘要: In an internal combustion engine having an exhaust gas turbocharger with an exhaust gas inlet structure including two exhaust gas flow passages in communication with two exhaust ducts via a rotary cylinder valve for controlling the exhaust gas flow, the valve includes two inlet openings for directing the flow to the inlet flow passages of the turbine and a recess which when disposed over the exhaust gas flow passages permits exhaust gas to flow from one to the other of the exhaust gas ducts, the interior of the valve being in communication with a bypass line for bypassing the turbine.
摘要翻译: 在具有废气涡轮增压器的内燃机中,所述排气涡轮增压器具有排气入口结构,所述排气入口结构包括通过用于控制废气流量的旋转气缸阀与两个排气管连通的两个废气流动通道,所述阀包括用于引导流动的两个入口 到涡轮机的入口流动通道和凹陷,当设置在废气流动通道上方时,排气能够从废气管道中的一个流到另一个,阀的内部与用于旁路的旁路管路连通 涡轮机。
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公开(公告)号:US20050229597A1
公开(公告)日:2005-10-20
申请号:US11150700
申请日:2005-06-11
申请人: Helmut Finger , Erwin Schmidt , Siegfried Sumser
发明人: Helmut Finger , Erwin Schmidt , Siegfried Sumser
IPC分类号: F02B37/02 , F02B37/18 , F02B37/24 , F02D9/06 , F02D9/16 , F02M25/07 , F16K11/076 , F02B47/08
CPC分类号: F02B37/183 , F02B29/0406 , F02B37/02 , F02B37/025 , F02B37/24 , F02D9/06 , F02D9/16 , F02M26/05 , F02M26/10 , F02M26/23 , F02M26/43 , F16K11/076 , Y02T10/144 , Y10T137/86871
摘要: In an internal combustion engine having an exhaust gas turbocharger with an exhaust gas inlet structure including two exhaust gas flow passages in communication with two exhaust ducts via a rotary cylinder valve for controlling the exhaust gas flow, the valve includes two inlet openings for directing the flow to the inlet flow passages of the turbine and a recess which when disposed over the exhaust gas flow passages permits exhaust gas to flow from one to the other of the exhaust gas ducts, the interior of the valve being in communication with a bypass line for bypassing the turbine.
摘要翻译: 在具有废气涡轮增压器的内燃机中,所述排气涡轮增压器具有排气入口结构,所述排气入口结构包括通过用于控制废气流量的旋转气缸阀与两个排气管连通的两个废气流动通道,所述阀包括用于引导流动的两个入口 到涡轮机的入口流动通道和凹陷,当设置在废气流动通道上方时,排气能够从废气管道中的一个流到另一个,阀的内部与用于旁路的旁路管路连通 涡轮机。
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