公开(公告)号：US5228292A

公开(公告)日：1993-07-20

申请号：US956260

申请日：1992-10-02

Applicant: Horst Hanauer ,  Michael Kuhn

Inventor： Horst Hanauer ,  Michael Kuhn

IPC: F02B37/24 ,  F02D41/00

CPC classification number: F02D41/1448 ,  F02B37/24 ,  F02D41/0007 ,  Y02T10/144

Abstract: An arrangement for adjusting the boost pressure in an internal-combustion engine, supercharged by an exhaust-gas turbocharger with adjustable turbine diffuser, to a predetermined desired boost-pressure value dependent on the operating point. To improve the efficiency of the internal-combustion engine in the non-steady-state mode, especially after a positive load change out of low load and speed ranges, or, after a positive load change during the non-steady-state mode, below a predetermined threshold value for the exhaust-gas counterpressure upstream of the turbine the boost pressure is regulated according to a first characteristic corresponding to the instantaneous true deviation of the actual boost-pressure value from the desired boost-pressure value. After this threshold value has been exceeded, the exhaust-gas counterpressure is regulated predetermining hypothetical control deviations for the boost-pressure control circuit according to a special characteristic.

Abstract translation: 用于调节由具有可调节的涡轮扩散器的废气涡轮增压器增压的内燃机中的增压压力到根据工作点的预定期望增压压力的装置。 为了提高非稳态模式下内燃机的效率，特别是在低负载和速度范围内的正负载变化之后，或者在非稳态模式下的正负载变化之后， 根据对应于实际增压压力值与期望增压压力值的瞬时真实偏差的第一特性，对涡轮上游的排气反压力的预定阈值进行调节。 在超过该阈值之后，根据特殊特性，调节排气反压力来预先确定升压压力控制电路的假设控制偏差。

公开(公告)号：US5174119A

公开(公告)日：1992-12-29

申请号：US745207

申请日：1991-08-15

Applicant: Horst Hanauer ,  Michael Kuhn

Inventor： Horst Hanauer ,  Michael Kuhn

IPC: F02B37/22 ,  F02B37/12 ,  F02B37/24 ,  F02D41/00

CPC classification number: F02D41/1448 ,  F02B37/24 ,  F02D41/0007 ,  Y02T10/144

Abstract: A process for adjusting the boost pressure in an internal-combustion engine, supercharged by an exhaust-gas turbocharger with adjustable turbine diffuser, to a predetermined desired boost-pressure value dependent on the operating point. To improve the efficiency of the internal-combustion engine in the non-steady-state mode, especially after a positive load change out of low load and speed ranges, or, after a positive load change during the non-stead-state mode, below a predetermined threshold value for the exhaust-gas counterpressure upstream of the turbine the boost pressure is regulated according to a first characteristic corresponding to the instantaneous true deviation of the actual boost-pressure value from the desired boost-pressure value. After this threshold value has been exceeded, the exhaust-gas counterpressure is regulated predetermining hypothetical control deviations for the boost-pressure control circuit according to a special characteristic.

Abstract translation: 一种用于调节由具有可调节的涡轮扩散器的排气涡轮增压器增压的内燃机中的增压压力到根据工作点的预定期望增压压力值的过程。 为了提高内燃机在非稳态模式下的效率，特别是在低负载和速度范围内的正负载变化之后，或者在非稳态模式下的正负载变化之后， 根据对应于实际增压压力值与期望增压压力值的瞬时真实偏差的第一特性，对涡轮上游的排气反压力的预定阈值进行调节。 在超过该阈值之后，根据特殊特性，调节排气反压力来预先确定升压压力控制电路的假设控制偏差。

公开(公告)号：US5906183A

公开(公告)日：1999-05-25

申请号：US46526

申请日：1998-03-24

Applicant: Harald Echtle ,  Horst Hanauer ,  Werner Rumez ,  Erwin Schmidt ,  Siegfried Sumser

Inventor： Harald Echtle ,  Horst Hanauer ,  Werner Rumez ,  Erwin Schmidt ,  Siegfried Sumser

IPC: F02B17/00 ,  F02B23/06 ,  F02B23/10 ,  F02B31/00 ,  F02B31/08 ,  F02B75/12 ,  F02F1/24 ,  F02F1/42 ,  F02M26/00 ,  F02M26/20

CPC classification number: F02B31/085 ,  F02B17/005 ,  F02B23/0696 ,  F02B23/101 ,  F02B31/08 ,  F02F1/4214 ,  F02M26/20 ,  F02B2023/108 ,  F02B2031/006 ,  F02B2075/125 ,  F02B2275/48 ,  F02B23/0621 ,  F02B23/0651 ,  F02F1/242 ,  F02F2001/241 ,  F02F2001/245 ,  F02M2026/009 ,  Y02T10/123 ,  Y02T10/125 ,  Y02T10/146

Abstract: In a method of forming a fuel/air mixture in an internal combustion engine with direct fuel injection, wherein a combustion air flow is admitted to each cylinder through at least one intake passage tangentially to the cylinder wall such that a combustion air spin flow about the cylinder axis is formed in the combustion chamber and fuel is injected into the combustion chamber in a fuel beam extending along the cylinder axis, at least one additional fluid stream is added to the combustion air flow in the intake passage at the side of the intake passage opposite the direction of the spin flow in the combustion chamber so as to provide an additional spin impulse to the combustion air in the combustion chamber.

Abstract translation: 在具有直接燃料喷射的内燃机中形成燃料/空气混合物的方法中，其中燃烧空气流通过与气缸壁相切的至少一个进气通道进入每个气缸，使得燃烧空气自由流动 缸体轴线形成在燃烧室中，并且燃料沿着汽缸轴线延伸的燃料束喷射到燃烧室中，至少一个额外的流体流被添加到进气通道中的进气通道侧面的燃烧空气流中 与燃烧室中的自旋流动的方向相反，以便向燃烧室中的燃烧空气提供额外的旋转脉冲。

公开(公告)号：US5850737A

公开(公告)日：1998-12-22

申请号：US706318

申请日：1996-08-30

Applicant: Werner Aschner ,  Horst Hanauer ,  Gernot Hertweck

Inventor： Werner Aschner ,  Horst Hanauer ,  Gernot Hertweck

IPC: F02B37/24 ,  F02D41/00 ,  F02D41/14 ,  F02B37/22

CPC classification number: F02B37/24 ,  F02D41/0007 ,  F02D41/1404 ,  Y02T10/144

Abstract: The invention provides a process for adjustment of the charging pressure in an internal-combustion engine exhaust gas turbocharger having an adjustable turbine geometry, to a predetermined operating-point-dependent desired charging pressure value. A fuzzy control function in an electronic control unit has as input quantities, a control difference and a control quantity, the latter being determined as the difference between an engine-operating-point-dependent maximum permissible differential pressure and a current differential pressure. The differential pressure is calculated as the difference from the exhaust back pressure and the charging pressure, so that unacceptable super elevation of the exhaust back pressure is recognized in the case of a positive load change, and is corrected by opening the blade position of the exhaust gas turbocharger with the variable turbine geometry, so that an optimum buildup of the torque takes place.

Abstract translation: 本发明提供了一种用于将具有可调涡轮机几何形状的内燃机排气涡轮增压器中的充气压力调节到预定的与操作点相关的期望充气压力值的过程。 电子控制单元中的模糊控制功能具有输入量，控制差和控制量，后者被确定为发动机工作点相关最大允许压差和电流差压之间的差值。 差压被计算为与排气背压和充气压力的差，从而在正负载变化的情况下识别排气背压的不可接受的超高程，并且通过打开排气的叶片位置来校正 具有可变涡轮机几何形状的气体涡轮增压器，使得发生扭矩的最佳累积。

公开(公告)号：US5454225A

公开(公告)日：1995-10-03

申请号：US301807

申请日：1994-09-07

Applicant: Siegfried Sumser ,  Wolfgang Erdmann ,  Erwin Schmidt ,  Horst Hanauer ,  Klaus Wunderlich

Inventor： Siegfried Sumser ,  Wolfgang Erdmann ,  Erwin Schmidt ,  Horst Hanauer ,  Klaus Wunderlich

IPC: F01D9/04 ,  F01D17/16 ,  F02B37/24 ,  F02B37/12

CPC classification number: F01D17/167 ,  F01D17/165 ,  F01D9/045 ,  F02B37/025 ,  F02B37/24 ,  F05D2220/40 ,  Y02T10/144

Abstract: In an exhaust gas turbocharger for an internal combustion engine comprising a compressor and an exhaust gas turbine mounted on a common shaft, the exhaust gas turbine includes a rotor with radial and semi-axial flow inlet areas and a single-flow duct surrounding the rotor and having port regions in the form of annular nozzle structures with guide vanes disposed adjacent each flow inlet area which are divided from one another by a ring of streamlined shape which is mounted to the guide vanes of one of the adjacent nozzle structures, said guide vanes having at least portions which are movable for adjusting the flow cross-section of the respective annular nozzle structures for controlling the flow through the radial and semi-axial flow inlet areas.

Abstract translation: 在用于内燃机的排气涡轮增压器中，其包括安装在公共轴上的压缩机和排气涡轮机，该排气涡轮包括具有径向和半轴流入口区域的转子和围绕转子的单流管道， 具有环形喷嘴结构形式的端口区域，导向叶片邻近每个流入口区域设置，所述导向叶片通过安装到相邻喷嘴结构之一的导向叶片的流线型形状的环彼此分开，所述导向叶片具有 至少部分可移动以调节相应的环形喷嘴结构的流动横截面，以控制通过径向和半轴流入口区域的流动。

公开(公告)号：US5335500A

公开(公告)日：1994-08-09

申请号：US34712

申请日：1993-03-19

Applicant: Klaus Wunderlich ,  Franz Neubrand ,  Erwin Schmidt ,  Hans-Wilhelm Buhl ,  Friedrich Wirbeleit ,  Horst Hanauer

Inventor： Klaus Wunderlich ,  Franz Neubrand ,  Erwin Schmidt ,  Hans-Wilhelm Buhl ,  Friedrich Wirbeleit ,  Horst Hanauer

IPC: F02B3/06 ,  F02B37/04 ,  F02B37/16 ,  F02B39/04 ,  F02B39/16 ,  F02B33/44

CPC classification number: F02B37/16 ,  F02B37/04 ,  F02B39/04 ,  F02B39/16 ,  F02B3/06 ,  Y02T10/144

Abstract: An internal combustion engine with combined pressure charging has an exhaust turbocharger turbine arranged in an exhaust conduit of the internal combustion engine driving a compressor arranged in an intake conduit. A mechanically driven supercharger is arranged downstream of the compressor and is coupled continuously variably to the engine via a Fottinger speed transformer with variable-pitch guide vanes and variable speed slip. To bypass the mechanically driven supercharger, a bypass conduit is provided. A circulating-air slide is arranged in the bypass conduit for controlling the air quantity bypassing the mechanically driven supercharger. The degree of opening of the circulating-air slide and the slip of the Fottinger speed transformer are controlled as a function of operating parameters such that the charge-air pressure is adjusted to a predetermined set point value.

Abstract translation: 具有组合式加压的内燃机具有布置在内燃机的排气管道中的排气涡轮增压器涡轮，其驱动布置在进气管道中的压缩机。 机械驱动的增压器设置在压缩机的下游，并通过具有可变桨距导向叶片和变速滑移的Föttinger变速器连续地可变地联接到发动机。 为了绕过机械驱动的增压器，提供旁路管道。 循环空气滑块布置在旁路管道中，用于控制绕过机械驱动的增压器的空气量。 控制循环空气滑块的开度和Föttinger变速器的滑动作为操作参数的函数，使得增压 - 空气压力被调节到预定的设定值。

公开(公告)号：US4773225A

公开(公告)日：1988-09-27

申请号：US75729

申请日：1987-07-20

Applicant: Reiner Bachschmid ,  Horst Hanauer ,  Manfred Fortnagel ,  Klaus Blumensaat

Inventor： Reiner Bachschmid ,  Horst Hanauer ,  Manfred Fortnagel ,  Klaus Blumensaat

IPC: F01D17/04 ,  F02B37/22 ,  F02B37/24 ,  F02C9/20 ,  F02D23/00

CPC classification number: F01D17/04 ,  F02B37/22 ,  F02B37/24 ,  F02C9/20 ,  Y02T10/144

Abstract: A method and apparatus for the load-dependent control of a turbocharger which is arranged in an internal combustion engine, a turbocharger includes an adjustable turbine guide apparatus which is adapted to be moved by way of an adjusting drive in the direction closing position or in the direction opening position. In order to be able to keep the response time of the turbocharger minimal during positive load changes with an optimum fuel consumption, the turbine guide apparatus is initially guided along a first predetermined characteristic curve in the direction closing position and subsequently in dependence on the charging pressure increase conditioned on the load increase according to a second predetermined characteristic curve again in the opening direction.

Abstract translation: 一种用于对内燃机中布置的涡轮增压器进行负载相关控制的方法和装置，涡轮增压器包括可调节的涡轮引导装置，其适于通过在关闭位置的调节驱动器或在关闭位置 方向开放位置。 为了在具有最佳燃料消耗的正负载变化期间能够使涡轮增压器的响应时间保持最小，首先沿着关闭位置的方向沿着第一预定特性曲线引导涡轮引导装置，随后根据充气压力 在打开方向再次根据第二预定特性曲线对负载增加进行调节。

公开(公告)号：US5758500A

公开(公告)日：1998-06-02

申请号：US839351

申请日：1997-04-17

Applicant: Siegfried Sumser ,  Horst Hanauer

Inventor： Siegfried Sumser ,  Horst Hanauer

IPC: F01D17/14 ,  F01D17/16 ,  F02B37/12

CPC classification number: F01D17/167 ,  F01D17/141 ,  F02B37/025 ,  F02B37/24 ,  F05D2220/40 ,  Y02T10/144

Abstract: In an exhaust gas turbocharger for an internal combustion engine comprising a compressor and a turbine with an impeller and a turbine wheel mounted on a common shaft, the exhaust turbine includes radial and semi-axial flow passages through which the exhaust gas is conducted to the turbine wheel and which are separated by a guide ring, and an annular sleeve is mounted in the turbine housing so as to be slideable therein along the axis of the turbine wheel across the radial flow passage for closing the radial flow passage of the turbine.

Abstract translation: 在用于内燃机的排气涡轮增压器中，所述排气涡轮机包括压缩机和具有安装在公共轴上的叶轮和涡轮机叶轮的涡轮机，所述排气涡轮机包括径向和半轴流动通道，废气通过该径向和半轴流动通道传导至涡轮机 并且由引导环分隔开，并且环形套筒安装在涡轮机壳体中，以便沿着涡轮机叶轮的轴线可跨过​​该径向流动通道滑动，以关闭涡轮机的径向流动通道。