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1. 发明授权

US06883314B2 Cooling of engine combustion air 有权
标题翻译：发动机燃烧空气冷却
公开(公告)号：US06883314B2
公开(公告)日：2005-04-26
申请号：US10210273
申请日：2002-08-01
申请人： James J. Callas , Gerald N. Coleman , James J. Faletti , David A. Pierpont , James R. Weber
发明人： James J. Callas , Gerald N. Coleman , James J. Faletti , David A. Pierpont , James R. Weber
IPC分类号： F02B3/06 , F02B29/04 , F02B37/013 , F02B33/44
CPC分类号： F02B37/013 , F02B3/06 , F02B29/0412 , F02B37/004 , Y02T10/142 , Y02T10/144 , Y02T10/146
摘要： Combustion air for use in an engine is normally compressed by a compressor which adds heat during the process of increasing the density of the combustion air. To decrease the heat content of the combustion air, an aftercooler is used. When compressing combustion air to a higher density, the combustion air is compressed by a first compressor section to a first preestablished pressure and temperature and by a second compressor section to a second preestablished pressure and temperature. To decrease the heat content of the highly compressed dense combustion air, a first aftercooler having an air to liquid configuration is used and a second aftercooler having an air to air configuration is used.
摘要翻译：用于发动机的燃烧空气通常由在增加燃烧空气的密度的过程中增加热量的压缩机压缩。为了降低燃烧空气的热量，使用后冷却器。当将燃烧空气压缩到更高的密度时，燃烧空气被第一压缩机部分压缩到第一预先建立的压力和温度，并且通过第二压缩机部分被压缩到第二预先建立的压力和温度。为了降低高度压缩的致密燃烧空气的热含量，使用具有空气至液体构造的第一后冷器，并且使用具有空气 - 空气构造的第二后冷器。

2. 发明授权

US06484499B2 Twin variable nozzle turbine exhaust gas recirculation system 有权
标题翻译：双变量喷嘴涡轮排气再循环系统
公开(公告)号：US06484499B2
公开(公告)日：2002-11-26
申请号：US09755356
申请日：2001-01-05
申请人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
发明人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
IPC分类号： F02B3344
CPC分类号： F02D23/02 , F01N13/107 , F02B3/06 , F02B29/0412 , F02B37/004 , F02B37/013 , F02B37/18 , F02B37/24 , F02M26/08 , F02M26/23 , F02M26/43 , F02M26/44 , Y02T10/144
摘要： An internal combustion engine, particularly suitable for a vehicle, is provided with a plurality of combustion cylinders, at least a first exhaust manifold and a second exhaust manifold and at least one intake manifold. Each exhaust manifold is coupled with a plurality of the combustion cylinders. Each intake manifold is coupled with a plurality of the combustion cylinders. A first turbocharger includes a first turbine having at least one inlet and an outlet, and a first compressor having an inlet and an outlet. Then at least one first turbine inlet has a controllable, variable intake nozzle fluidly coupled with the first exhaust manifold. A second turbocharger includes a second turbine having an inlet and an outlet, and a second compressor having an inlet and an outlet. The second turbine inlet has a controllable, variable intake nozzle fluidly coupled with the second exhaust manifold. The first compressor outlet is fluidly coupled with the second compressor inlet. The engine has improved performance, is compact in design and is economical in operation.
摘要翻译：特别适用于车辆的内燃机设置有多个燃烧缸，至少第一排气歧管和第二排气歧管以及至少一个进气歧管。每个排气歧管与多个燃烧气缸联接。每个进气歧管与多个燃烧气缸联接。第一涡轮增压器包括具有至少一个入口和出口的第一涡轮机和具有入口和出口的第一压缩机。然后，至少一个第一涡轮机入口具有与第一排气歧管流体耦合的可控制的可变进气喷嘴。第二涡轮增压器包括具有入口和出口的第二涡轮机和具有入口和出口的第二压缩机。第二涡轮机入口具有与第二排气歧管流体耦合的可控制的可变进气喷嘴。第一压缩机出口与第二压缩机入口流体耦合。发动机性能提高，设计紧凑，操作经济。

3. 发明授权

US06321537B1 Exhaust gas recirculation system in an internal combustion engine 有权
标题翻译：内燃机废气再循环系统
公开(公告)号：US06321537B1
公开(公告)日：2001-11-27
申请号：US09706481
申请日：2000-11-03
申请人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
发明人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
IPC分类号： F02B3344
CPC分类号： F01N13/107 , F02B29/0406 , F02B37/001 , F02B37/013 , F02B37/183 , F02M26/08 , F02M26/10 , F02M26/23 , F02M26/42 , F02M26/69 , F02M26/71 , F02M26/73 , Y02T10/144
摘要： An exhaust gas recirculation system, particularly suitable for use in an internal combustion engine, is provided with a plurality of combustion cylinders, at least one exhaust manifold, and at least one intake manifold. Each exhaust manifold is coupled with a plurality of the combustion cylinders, and each intake manifold is coupled with a plurality of combustion cylinders. A first turbocharger includes a first turbine having at least one inlet and an outlet, and a first compressor having an inlet and an outlet. The at least one first turbine inlet is fluidly coupled with a corresponding exhaust manifold. A second turbocharger includes a second turbine having at least one inlet and an outlet, and a second compressor having an inlet and an outlet. The at least one second turbine inlet is fluidly coupled with a corresponding exhaust manifold. A valve assembly includes an inlet, a first outlet and a second outlet. The valve inlet is fluidly coupled with a corresponding first turbine inlet, the valve first outlet is fluidly coupled with the second turbine inlet, and the valve second outlet is fluidly coupled with at least one intake manifold.
摘要翻译：特别适用于内燃机的排气再循环系统设置有多个燃烧气缸，至少一个排气歧管和至少一个进气歧管。每个排气歧管与多个燃烧气缸联接，并且每个进气歧管与多个燃烧气缸联接。第一涡轮增压器包括具有至少一个入口和出口的第一涡轮机和具有入口和出口的第一压缩机。所述至少一个第一涡轮机入口与相应的排气歧管流体联接。第二涡轮增压器包括具有至少一个入口和出口的第二涡轮机和具有入口和出口的第二压缩机。至少一个第二涡轮机入口与相应的排气歧管流体连接。阀组件包括入口，第一出口和第二出口。阀入口与对应的第一涡轮机入口流体联接，阀第一出口与第二涡轮机入口流体联接，阀第二出口与至少一个进气歧管流体连接。

4. 发明授权

US06484500B1 Two turbocharger engine emission control system 有权
标题翻译：两个涡轮增压器发动机排放控制系统
公开(公告)号：US06484500B1
公开(公告)日：2002-11-26
申请号：US09939968
申请日：2001-08-27
申请人： Gerald N. Coleman , Dennis D. Feucht , James J. Faletti , David A. Pierpont
发明人： Gerald N. Coleman , Dennis D. Feucht , James J. Faletti , David A. Pierpont
IPC分类号： F02B3344
CPC分类号： F02B37/22 , F01N13/107 , F02B29/0406 , F02B37/004 , F02B37/013 , F02B37/025 , F02B37/12 , F02B37/18 , F02M26/08 , F02M26/23 , F02M26/43 , F02M26/44 , F02M26/71 , Y02T10/144
摘要： An internal combustion engine comprises a first exhaust manifold, a second exhaust manifold, a first turbocharger having a first turbine and a first compressor, and a second turbocharger having a second turbine and a second compressor. A second gas inlet port of the second turbine is connected in fluid communication with a second exhaust manifold to receive at least a portion of second combustion gases. A second gas outlet port of the second turbine and the first exhaust manifold are in fluid communication with a first gas inlet port of the first turbine. A valve is connected in fluid communication with the second exhaust manifold to receive a remainder of exhaust gases not included in the at least a portion of the second combustion gases supplied to the second turbine. The valve is connected in fluid communication with a mixer to deliver at least a portion of the remainder of exhaust gases to the mixer for mixing with compressed air in the mixer.
摘要翻译：内燃机包括第一排气歧管，第二排气歧管，具有第一涡轮机和第一压缩机的第一涡轮增压器和具有第二涡轮机和第二压缩机的第二涡轮增压器。第二涡轮机的第二气体入口与第二排气歧管流体连通地连接以接收至少一部分第二燃烧气体。第二涡轮机和第一排气歧管的第二气体出口与第一涡轮机的第一气体入口端口流体连通。阀与第二排气歧管流体连通地连接，以接收不包括在供应到第二涡轮的第二燃烧气体的至少一部分中的余下的废气。阀与混合器流体连通地连接以将剩余的废气的至少一部分输送到混合器以与混合器中的压缩空气混合。

5. 发明授权

US06418721B1 Two turbocharger exhaust gas re-circulation system having a first stage variable nozzle turbine 失效
标题翻译：两个具有第一级可变喷嘴涡轮的涡轮增压器排气再循环系统
公开(公告)号：US06418721B1
公开(公告)日：2002-07-16
申请号：US09755632
申请日：2001-01-05
申请人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
发明人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
IPC分类号： F02B3344
CPC分类号： F02B37/001 , F01N13/107 , F02B37/004 , F02B37/013 , F02B37/18 , F02B37/22 , F02B37/24 , F02M26/05 , F02M26/08 , F02M26/23 , F02M26/42 , F02M26/71 , Y02T10/144
摘要： An internal combustion engine, particularly suitable for a motor vehicle, is provided with a plurality of combustion cylinders, at least a first exhaust manifold and a second exhaust manifold and at least one intake manifold. Each exhaust manifold is coupled with a plurality of the combustion cylinders. Each intake manifold is coupled with a plurality of the combustion cylinders. A first turbocharger includes a first turbine having at least one inlet and an outlet, and a first compressor having an inlet and an outlet. The at least one first turbine inlet is fluidly coupled with the first exhaust manifold and includes a controllable, variable intake nozzle. A second turbocharger includes a second turbine having an inlet and an outlet, and a second compressor having an inlet and an outlet. The second turbine inlet is fluidly coupled with the second exhaust manifold. The first compressor outlet is fluidly coupled with the second compressor inlet. The engine has improved performance and efficiency, with an efficient and compact turbocharger arrangement.
摘要翻译：特别适用于机动车辆的内燃机设置有多个燃烧缸，至少第一排气歧管和第二排气歧管以及至少一个进气歧管。每个排气歧管与多个燃烧气缸联接。每个进气歧管与多个燃烧气缸联接。第一涡轮增压器包括具有至少一个入口和出口的第一涡轮机和具有入口和出口的第一压缩机。所述至少一个第一涡轮机入口与所述第一排气歧管流体耦合并且包括可控的可变进气喷嘴。第二涡轮增压器包括具有入口和出口的第二涡轮机和具有入口和出口的第二压缩机。第二涡轮机入口与第二排气歧管流体耦合。第一压缩机出口与第二压缩机入口流体耦合。发动机具有改进的性能和效率，具有高效紧凑的涡轮增压器装置。

6. 发明授权

US06412279B1 Twin turbine exhaust gas re-circulation system having a second stage variable nozzle turbine 失效
标题翻译：具有第二级可变喷嘴涡轮机的双涡轮排气再循环系统
公开(公告)号：US06412279B1
公开(公告)日：2002-07-02
申请号：US09742700
申请日：2000-12-20
申请人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
发明人： Gerald N. Coleman , James J. Faletti , Dennis D. Feucht , David A. Pierpont
IPC分类号： F02B3344
CPC分类号： F02D41/0007 , F02B29/0406 , F02B37/001 , F02B37/013 , F02B37/025 , F02B37/24 , F02D41/0065 , F02M26/08 , F02M26/23 , F02M26/43 , Y02T10/144
摘要： An internal combustion engine, particularly suitable for a motor vehicle, is provided with a plurality of combustion cylinders, at least a first exhaust manifold and a second exhaust manifold and at least one intake manifold. Each exhaust manifold is coupled with a plurality of the combustion cylinders. Each intake manifold is coupled with a plurality of the combustion cylinders. A first turbocharger includes a first turbine having at least one inlet and an outlet, and a first compressor having an inlet and an outlet. The at least one first turbine inlet is fluidly coupled with the first exhaust manifold. A second turbocharger includes a second turbine having an inlet and an outlet, and a second compressor having an inlet and an outlet. The second turbine inlet is fluidly coupled with the second exhaust manifold and includes a controllable, variable intake nozzle. The first compressor outlet is fluidly coupled with the second compressor inlet. The engine has good fuel consumption characteristics and EGR flow rate control.
摘要翻译：特别适用于机动车辆的内燃机设置有多个燃烧缸，至少第一排气歧管和第二排气歧管以及至少一个进气歧管。每个排气歧管与多个燃烧气缸联接。每个进气歧管与多个燃烧气缸联接。第一涡轮增压器包括具有至少一个入口和出口的第一涡轮机和具有入口和出口的第一压缩机。所述至少一个第一涡轮机入口与所述第一排气歧管流体耦合。第二涡轮增压器包括具有入口和出口的第二涡轮机和具有入口和出口的第二压缩机。第二涡轮机入口与第二排气歧管流体连接并且包括可控的可变进气喷嘴。第一压缩机出口与第二压缩机入口流体耦合。发动机具有良好的燃油消耗特性和EGR流量控制。

7. 发明授权

US06640542B2 Bypass venturi assembly with single shaft actuator for an exhaust gas recirculation system 失效
公开(公告)号：US06640542B2
公开(公告)日：2003-11-04
申请号：US10028634
申请日：2001-12-20
申请人： Gerald N. Coleman , Dennis D. Feucht , Michael P. Harmon , David A. Pierpont , Matthew D. Rampenthal
发明人： Gerald N. Coleman , Dennis D. Feucht , Michael P. Harmon , David A. Pierpont , Matthew D. Rampenthal
IPC分类号： F02B3344
CPC分类号： F02B33/44 , F02B37/00 , Y02T10/144 , Y10T137/87692
摘要： An internal combustion engine, particularly suitable for use in a work machine, is provided with a combustion air supply and an exhaust manifold. A bypass venturi assembly includes a housing having an outlet, a combustion air inlet and an exhaust gas inlet. A center piece is positioned within the housing and is in communication with the combustion air inlet. The center piece defines a combustion air bypass section therein. A combustion air bypass valve is positioned in association with the combustion air bypass section. An exhaust gas valve is positioned in association with the exhaust gas inlet. A single shaft is coupled with and carries each of the combustion air bypass valve and the exhaust gas valve.

8. 发明授权

US06439212B1 Bypass venturi assembly and elbow with turning vane for an exhaust gas recirculation system 失效
标题翻译：旁路文氏管组件和弯头与转向叶片用于废气再循环系统
公开(公告)号：US06439212B1
公开(公告)日：2002-08-27
申请号：US10025368
申请日：2001-12-19
申请人： Gerald N. Coleman , Dennis D. Feucht , Michael P. Harmon , David A. Pierpont , Matthew D. Rampenthal
发明人： Gerald N. Coleman , Dennis D. Feucht , Michael P. Harmon , David A. Pierpont , Matthew D. Rampenthal
IPC分类号： F02B4708
CPC分类号： F02D9/104 , F02B37/00 , F02D2009/0276 , F02M26/05 , F02M26/10 , F02M26/19 , F02M26/54 , F02M35/10118 , F02M35/10222 , F02M35/10268 , F02M35/112
摘要： A bypass venturi assembly for recirculating exhaust gas in an internal combustion engine, Particularly suitable for use in an on-road vehicle, is provided with a housing having an outlet, a combustion air inlet and an exhaust gas inlet. A center piece is Positioned within the housing and is in communication with the combustion air inlet. The center piece defines a combustion air bypass section therein. A combustion air bypass valve is positioned in association with the combustion air bypass section. An exhaust gas valve is positioned in association with the exhaust gas inlet. An elbow is coupled with the outlet and defines a fluid flow path. The elbow includes a vane therein which is positioned in association with the flow path.
摘要翻译：用于在内燃机中再循环废气的旁路文氏管组件，特别适用于在道路车辆上设置有具有出口，燃烧空气入口和废气入口的壳体。中心件位于外壳内并与燃烧空气入口连通。中心件在其中限定燃烧空气旁通部分。燃烧空气旁通阀与燃烧空气旁路部分相关联地定位。排气阀与废气入口相关联地定位。肘部与出口联接并限定流体流动路径。弯头包括与流路相关联地定位的叶片。

9. 发明授权

US06659092B2 Bypass assembly with annular bypass venturi for an exhaust gas recirculation system 失效
公开(公告)号：US06659092B2
公开(公告)日：2003-12-09
申请号：US10028633
申请日：2001-12-20
申请人： Gerald N. Coleman , Dennis D. Feucht , Michael P. Harmon , David A. Pierpont , Matthew D. Rampenthal
发明人： Gerald N. Coleman , Dennis D. Feucht , Michael P. Harmon , David A. Pierpont , Matthew D. Rampenthal
IPC分类号： F02M2507
CPC分类号： F02M26/51 , F02M26/19 , F02M26/21 , F02M26/70
摘要： A bypass venturi assembly for recirculating exhaust gas in an internal combustion engine, and particularly suitable for use in a vehicle, is provided with a housing having an outlet, a combustion air inlet and an exhaust gas inlet. A center piece is positioned within the housing and in communication with the combustion air inlet. The center piece defines a combustion air bypass section therein. An annular venturi nozzle positioned between the housing and the center piece is in communication with the combustion air inlet and defines a combustion air venturi section. The venturi nozzle is in communication with the exhaust gas inlet and defines an exhaust gas venturi section. A combustion air bypass valve is positioned in association with the combustion air bypass section. An exhaust gas valve is positioned in association with the exhaust gas inlet. The venturi nozzle is separate from the housing and allows a nozzle with a particular configuration to be utilized, depending upon the application.

10. 发明授权

US06609373B2 Exhaust gas recirculation system with variable geometry turbine and bypass venturi assembly 有权
标题翻译：具有可变几何涡轮机和旁路文丘里管组件的废气再循环系统
公开(公告)号：US06609373B2
公开(公告)日：2003-08-26
申请号：US10025655
申请日：2001-12-19
申请人： Gerald N. Coleman , David A. Pierpont , Dennis D. Feucht , Matthew D. Rampenthal , Michael P. Harmon
发明人： Gerald N. Coleman , David A. Pierpont , Dennis D. Feucht , Matthew D. Rampenthal , Michael P. Harmon
IPC分类号： F02B3344
CPC分类号： F02B33/44 , F02B37/24 , F02D2009/0276 , F02M26/05 , F02M26/10 , F02M26/21 , F02M26/51 , F02M26/70 , Y02T10/144
摘要： An internal combustion engine, particularly suitable for use in a work machine, is provided with an exhaust manifold, a turbocharger, and a bypass venturi assembly. The turbocharger includes a turbine and a compressor, with the turbine having a variable geometry inlet coupled with the exhaust manifold, and the compressor having an outlet. The bypass venturi assembly includes a housing having an outlet, a combustion air inlet and an exhaust gas inlet. The combustion air inlet is coupled with the compressor outlet. The exhaust gas inlet is coupled with the exhaust manifold. A center piece is positioned within the housing and is in communication with the combustion air inlet. The center piece defines a combustion air bypass section therein. A combustion air bypass valve is positioned in association with the combustion air bypass section. The exhaust gas valve is positioned in association with the exhaust gas inlet. The variable geometry inlet of the turbine allows the pressure ratio of the compressed combustion air to be varied, thereby improving the mixing efficiency of the exhaust gas with the combustion air.
摘要翻译：特别适用于作业机械的内燃机设置有排气歧管，涡轮增压器和旁路文氏管组件。涡轮增压器包括涡轮机和压缩机，涡轮机具有与排气歧管连接的可变几何入口，并且压缩机具有出口。旁路文氏管组件包括具有出口，燃烧空气入口和废气入口的壳体。燃烧空气入口与压缩机出口连接。排气入口与排气歧管连接。中心件位于壳体内并与燃烧空气入口连通。中心件在其中限定燃烧空气旁通部分。燃烧空气旁通阀与燃烧空气旁路部分相关联地定位。排气阀与排气入口相关联地定位。涡轮机的可变几何形状入口允许压缩的燃烧空气的压力比改变，从而提高废气与燃烧空气的混合效率。

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