-
公开(公告)号：US20080152484A1
公开(公告)日：2008-06-26
申请号：US12001078
申请日：2007-12-08
CPC分类号： F02C6/12 , F01D17/143 , F02C9/18
摘要： In an exhaust-gas turbine of an exhaust-gas turbo-charger including a turbine wheel which is rotatably supported in a housing and to which exhaust gas can be supplied via an inlet channel and discharged out of the exhaust-gas turbine via an outlet duct, wherein a guide vane structure and an axial slide which interacts with the latter, are disposed in the turbine inlet at the transition from the inlet channel to the turbine wheel, the guide vane structure is fixedly mounted with respect to the housing and the axial slide is arranged at the turbine outlet side and is movably supported on an outlet duct contour sleeve and provided with an axial opening for accommodating the guide vane structure, and the contour sleeve includes openings which conduct exhaust gas from the inlet channel directly to the outlet duct and which are arranged so that they are covered by the axial slide when the axial slide is moved out of its open position, the guide vane structure extending axially over the contour sleeve openings so as to impart a swirl to the exhaust gas being discharged via the contour sleeve openings when the slide member is in an open position.
摘要翻译： 在排气涡轮增压器的废气涡轮机中，该排气涡轮增压器包括可旋转地支撑在壳体中的涡轮机叶轮，并且可以经由入口通道向其供给废气，并经由出口管道排出废气涡轮机 ，其中在从所述入口通道到所述涡轮机叶轮的过渡处，在所述涡轮机入口处设置有与所述涡轮机入口相互作用的导向叶片结构和轴向滑动件，所述导向叶片结构相对于所述壳体和所述轴向滑块 布置在涡轮出口侧并且可移动地支撑在出口管道轮廓套筒上并且设置有用于容纳引导叶片结构的轴向开口，并且轮廓套筒包括将排气从入口通道直接引导到出口管道的开口， 它们被布置成使得当轴向滑动件从其打开位置移出时它们被轴向滑动件覆盖，导向叶片结构在轴线上延伸超过轮廓 ur套筒开口，以便当滑动构件处于打开位置时，经由轮廓套筒开口排出的废气产生漩涡。
-
公开(公告)号：US20050056016A1
公开(公告)日：2005-03-17
申请号：US10949959
申请日：2004-09-24
IPC分类号： F02B37/00 , F01D17/16 , F02B37/24 , F02D23/00 , F02D41/00 , F02M25/07 , F04D27/02 , F04D29/46 , F02B33/44
CPC分类号： F04D29/462 , F01D17/165 , F02B29/0406 , F02B37/24 , F02D41/0007 , F02M26/05 , F02M26/10 , F02M26/23 , F04D29/4213 , F05D2250/51 , Y02T10/144
摘要： In a variable exhaust gas turbocharger for an internal combustion engine having an exhaust gas turbine and a compressor with a variable vane structure wherein the exhaust gas turbocharger comprises a housing and a compressor wheel which is connected to an exhaust gas turbine wheel via a shaft, the compressor has a radial inflow flow passage in which a variable vane structure or throttle device is arranged upstream of the compressor wheel and another vane structure is arranged in the radial flow passage downstream of the compressor wheel in the direction of flow.
摘要翻译： 在具有废气涡轮机的内燃机的可变废气涡轮增压器和具有可变叶片结构的压缩机中，其中排气涡轮增压器包括壳体和通过轴连接到废气涡轮机叶轮的压缩机叶轮， 压缩机具有径向流入流动通道，其中可变叶片结构或节流装置布置在压缩机叶轮的上游，并且另一个叶片结构布置在沿着流动方向的压缩机叶轮下游的径向流动通道中。
-
43.发明授权Exhaust gas turbocharger for an internal combustion engine and a method for operating an exhaust gas turbocharger 失效用于内燃机的废气涡轮增压器和用于操作排气涡轮增压器的方法公开(公告)号：US06481205B2
公开(公告)日：2002-11-19
申请号：US09974713
申请日：2001-10-10
IPC分类号： F02B3344
CPC分类号： F02C6/12 , F01D15/10 , F02B37/025 , F02B37/10 , F02B39/10 , F04D17/025 , F04D25/024 , F04D25/0606 , F04D25/066 , F05D2220/40 , Y02T10/144
摘要： In an exhaust gas turbocharger for an internal combustion engine having an air intake duct and an exhaust duct and wherein the turbocharger includes a compressor arranged in the air intake duct and a turbine arranged in the exhaust duct and a shaft carrying the turbine wheel and the compressor impeller, an electric motor is provided which includes a rotor provided with an air mover disposed in the inlet area of the compressor and being controllable for rotation independently of the rotation of the turbine.
摘要翻译： 在具有进气管道和排气管道的内燃机的排气涡轮增压器中，所述涡轮增压器包括布置在所述进气管道中的压缩机和布置在所述排气管道中的涡轮机，以及承载所述涡轮机叶轮和所述压缩机的轴 叶轮，提供一种电动机，其包括设置有设置在压缩机的入口区域中的鼓风机的转子，并且可独立于涡轮机的旋转而被控制。
-
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。
-
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。
-
46.发明授权公开(公告)号：US07513114B2
公开(公告)日：2009-04-07
申请号：US11645123
申请日：2006-12-22
申请人： Siegfried Sumser , Wolfram Schmid , Helmut Finger
发明人： Siegfried Sumser , Wolfram Schmid , Helmut Finger
CPC分类号： F02B37/02 , F02B37/025 , F02B37/22 , Y02T10/144
摘要： In an exhaust gas turbocharger for a reciprocating internal combustion engine comprising an exhaust gas turbine in the exhaust line and a compressor in the inlet line of the engine, the exhaust gas turbine has two exhaust gas flow passages, by way of which exhaust gas is fed to the turbine rotor, the ratio of the turbine rotor diameter to the compressor wheel diameter being set by a function, which is dependent on the displacement volume of the internal combustion engine.
摘要翻译： 在用于往复式内燃机的废气涡轮增压器中，其包括排气管线中的排气涡轮机和发动机的入口管路中的压缩机，排气涡轮机具有两个废气流动通道，通过该排气流路 涡轮转子直径与压缩机叶轮直径的比率由根据内燃机的排量的功能来设定。
-
公开(公告)号：US08186943B2
公开(公告)日：2012-05-29
申请号：US12001078
申请日：2007-12-08
IPC分类号： F01B25/02
CPC分类号： F02C6/12 , F01D17/143 , F02C9/18
摘要： In an exhaust-gas turbine of an exhaust-gas turbo-charger including a turbine wheel which is rotatably supported in a housing and to which exhaust gas can be supplied via an inlet channel and discharged out of the exhaust-gas turbine via an outlet duct, wherein a guide vane structure and an axial slide which interacts with the latter, are disposed in the turbine inlet at the transition from the inlet channel to the turbine wheel, the guide vane structure is fixedly mounted with respect to the housing and the axial slide is arranged at the turbine outlet side and is movably supported on an outlet duct contour sleeve and provided with an axial opening for accommodating the guide vane structure, and the contour sleeve includes openings which conduct exhaust gas from the inlet channel directly to the outlet duct and which are arranged so that they are covered by the axial slide when the axial slide is moved out of its open position, the guide vane structure extending axially over the contour sleeve openings so as to impart a swirl to the exhaust gas being discharged via the contour sleeve openings when the slide member is in an open position.
摘要翻译： 在排气涡轮增压器的废气涡轮机中，该排气涡轮增压器包括可旋转地支撑在壳体中的涡轮机叶轮，并且可以经由入口通道向其供给废气，并经由出口管道排出废气涡轮机 ，其中在从所述入口通道到所述涡轮机叶轮的过渡处，在所述涡轮机入口处设置有与所述涡轮机入口相互作用的导向叶片结构和轴向滑动件，所述导向叶片结构相对于所述壳体和所述轴向滑块 布置在涡轮出口侧并且可移动地支撑在出口管道轮廓套筒上并且设置有用于容纳引导叶片结构的轴向开口，并且轮廓套筒包括将排气从入口通道直接引导到出口管道的开口， 它们被布置成使得当轴向滑动件从其打开位置移出时它们被轴向滑动件覆盖，导向叶片结构在轴线上延伸超过轮廓 ur套筒开口，以便当滑动构件处于打开位置时，经由轮廓套筒开口排出的废气产生漩涡。
-
公开(公告)号：US07870731B2
公开(公告)日：2011-01-18
申请号：US11978158
申请日：2007-10-27
CPC分类号： F02C6/12 , F01D5/022 , F01D17/143 , F02C3/073 , F04D29/284 , F04D29/4213
摘要： In an exhaust gas turbocharger for an internal combustion engine having a turbine wheel connected, by means of a shaft, to the compressor wheel of a compressor which includes a variable inlet geometry comprising a plunger and a sleeve-shaped partition for controlling an auxiliary duct leading radially to the compressor wheel, which is provided with compressor wheel blades to which air is supplied axially via an axial inlet passage and radially via a radial wheel inlet area, the compressor wheel includes a contoured ring provided at its outer circumferential surface with auxiliary blades disposed over, and aligned with, the compressor wheel blades in the radial and the axial wheel inlet region of the compressor wheel.
摘要翻译： 在用于内燃机的废气涡轮增压器中，其具有通过轴连接到压缩机的压缩机叶轮的涡轮机轮，所述压缩机叶轮包括可变入口几何形状，其包括柱塞和用于控制辅助管道的套筒形分隔件 压缩机叶轮设置有压缩机叶轮，空气经由轴向入口通道轴向供应，径向通过径向轮入口区域，压缩机叶轮包括设置在其外圆周表面处的轮廓环，辅助叶片设置 并且与压缩机叶轮的径向和轴向轮入口区域中的压缩机叶轮对准并对齐。
-
公开(公告)号：US20080092538A1
公开(公告)日：2008-04-24
申请号：US11978158
申请日：2007-10-27
IPC分类号： F02B33/44
CPC分类号： F02C6/12 , F01D5/022 , F01D17/143 , F02C3/073 , F04D29/284 , F04D29/4213
摘要： In an exhaust gas turbocharger for an internal combustion engine having a turbine wheel connected, by means of a shaft, to the compressor wheel of a compressor which includes a variable inlet geometry comprising a plunger and a sleeve-shaped partition for controlling an auxiliary duct leading radially to the compressor wheel, which is provided with compressor wheel blades to which air is supplied axially via an axial inlet passage and radially via a radial wheel inlet area, the compressor wheel includes a contoured ring provided at its outer circumferential surface with auxiliary blades disposed over, and aligned with, the compressor wheel blades in the radial and the axial wheel inlet region of the compressor wheel.
摘要翻译： 在用于内燃机的废气涡轮增压器中，其具有通过轴连接到压缩机的压缩机叶轮的涡轮机轮，所述压缩机叶轮包括可变入口几何形状，其包括柱塞和用于控制辅助管道的套筒形分隔件 压缩机叶轮设置有压缩机叶轮，空气经由轴向入口通道轴向供应，径向通过径向轮入口区域，压缩机叶轮包括设置在其外圆周表面处的轮廓环，辅助叶片设置 并且与压缩机叶轮的径向和轴向轮入口区域中的压缩机叶轮对准并对齐。
-
50.发明申请公开(公告)号：US20070125082A1
公开(公告)日：2007-06-07
申请号：US11655955
申请日：2007-01-19
CPC分类号： F02C7/36 , F02B29/0406 , F02B37/013 , F02B37/025 , F02B37/225 , F02B37/24 , F02B39/12 , F02C3/113 , F02M26/05 , F02M26/23 , F04D25/026 , F04D25/04 , F04D27/0269 , F04D29/052 , F05D2220/40 , F05D2240/24 , F05D2260/50 , Y02T10/144
摘要： In a compressor of an exhaust gas turbocharger of an internal combustion engine including a compressor wheel with an auxiliary rotor wheel which is rotatably supported adjacent to, and upstream of, the compressor wheel and which is movable axially between a coupled position with the compressor wheel and a decoupled position, wherein, in the coupled position, the auxiliary rotor wheel is rotationally connected to the compressor wheel, without contacting the compressor wheel, by means of a magnetic clutch for transferring a torque from the auxiliary rotor wheel to the compressor wheel in a low engine power operating range in order to maintain the compressor wheel at an increased speed.
摘要翻译： 在内燃机的排气涡轮增压器的压缩机中，该内燃机的排气涡轮增压器包括具有辅助转子轮的压缩机叶轮，所述压缩机叶片可与压缩机叶轮相邻并且上游地可旋转地支撑，该压缩机叶轮可在与压缩机叶轮的联接位置和 解耦位置，其中，在联接位置，辅助转子轮通过用于将转矩从辅助转子轮传递到压缩机叶轮的磁性离合器而不与压缩机叶轮接触而旋转地连接到压缩机叶轮 低发动机功率工作范围，以保持压缩机叶轮的速度提高。
-
-
-
-
-
-
-
-
-
搜索结果
161 条记录 (耗时 0.027 秒)
