公开(公告)号：US20040261413A1

公开(公告)日：2004-12-30

申请号：US10496934

申请日：2004-05-26

发明人： Toshihiko Nishiyama ,  Hiroshi Sugito ,  Takahisa Iino

IPC分类号： F02D023/00

CPC分类号： F02B37/24 ,  F01D17/165 ,  F02C6/12 ,  F05D2220/40 ,  Y02T10/144 ,  Y10T29/49323

摘要： One of the swing shafts 32 of the nozzle vanes 31 is selected so as to operate as swing drive shaft 33 that projects to the outside. As the swing drive shaft 33 is driven to revolve, all the nozzle vanes 31 are driven to turn by a same angle by way of the driving lever 21 and the coupling ring 18 linked to it. Therefore, it is only the swing drive shaft 33 that projects to the outside, the projecting part can be sealed in a simple and reliable manner to improve the sealing effect and the durability of the variable geometry turbocharger. Additionally, since the rotary motion of the swing drive shaft 33 is directly used to driven the nozzle vanes 31 to swing, the mechanism for transmitting the driving force is simplified.

公开(公告)号：US20040187495A1

公开(公告)日：2004-09-30

申请号：US10780910

申请日：2004-02-19

申请人： Jidosha Denki Kogyo Co., Ltd.

发明人： Yoshiyuki Ando ,  Takumi Arao ,  Takaaki Sekine ,  Haruo Saito

IPC分类号： F02D023/00

CPC分类号： H02K7/116 ,  F01D17/16 ,  F01D17/165 ,  F02B37/24 ,  F05D2220/40 ,  H02K5/225 ,  H02K11/00 ,  Y02T10/144

摘要： In a nozzle vane driving control apparatus of a variable nozzle turbocharger including an actuator for carrying out a driving operation for opening and closing a nozzle vane of a variable nozzle and an ECU for controlling the opening degree of the nozzle vane which is obtained by the actuator, an actuator cover for covering a pinion and reduction gears by interposing a base provided integrally with a motor case portion therebetween, a unit body accommodating each of control boards, a position sensor for detecting the rotating position of an output shaft and a connector having a terminal connecting a motor and each of the control boards, and a unit cover for covering the unit body are removably fastened and fixed with a bolt and are thus integrated with each other.

摘要翻译： 一种可变喷嘴涡轮增压器的喷嘴叶片驱动控制装置，包括用于执行用于打开和关闭可变喷嘴的喷嘴叶片的驱动操作的致动器和用于控制由致动器获得的喷嘴叶片的开度的ECU ，用于通过将与其间的电动机壳体部分整体设置的基座相互覆盖小齿轮和减速齿轮的致动器盖，容纳每个控制板的单元体，用于检测输出轴的旋转位置的位置传感器和具有 连接电动机和每个控制板的端子和用于覆盖单元主体的单元盖可拆卸地用螺栓紧固和固定，并因此彼此一体化。

公开(公告)号：US20040128997A1

公开(公告)日：2004-07-08

申请号：US10717232

申请日：2003-11-19

发明人： John Parker

IPC分类号： F02D023/00

CPC分类号： F02C9/18 ,  F01D17/14 ,  F01D17/165 ,  F02C6/12 ,  F05D2220/40

摘要： A variable geometry turbine has an annular inlet passageway defined between a radial wall of a moveable wall member and a facing wall of the turbine housing. The moveable wall member is mounted within an annular cavity provided within the housing and having inner and outer annular surfaces. An annular seal is disposed between an annular flange of the moveable wall member and the adjacent inner or outer annular surface of the cavity. One or more inlet bypass passages are provided in the annular flange or said adjacent cavity surface, such that the annular seal and bypass passageways move axially relative to one another as the moveable wall member moves. The annular seal and the or each bypass passage are axially located such as the annular wall member approaches the facing wall of the housing the or each bypass passage permits the flow of exhaust gas through said cavity to the turbine wheel thereby bypassing the annular inlet passageway.

摘要翻译： 可变几何涡轮机具有限定在可移动壁构件的径向壁和涡轮机壳体的相对壁之间的环形入口通道。 可移动壁构件安装在设置在壳体内的环形空腔内并具有内环形表面和外环形表面。 环形密封件设置在可移动壁构件的环形凸缘和腔的相邻内部或外部环形表面之间。 一个或多个入口旁路通道设置在环形凸缘或所述相邻腔体表面中，使得当可移动壁构件移动时，环形密封件和旁路通道相对于彼此轴向移动。 环形密封件和每个旁路通道被轴向定位，例如环形壁构件接近壳体的相对壁，或者每个旁路通道允许废气通过所述空腔流到涡轮机轮，从而绕过环形入口通道。

公开(公告)号：US20040025505A1

公开(公告)日：2004-02-12

申请号：US10636627

申请日：2003-08-08

申请人： Bombardier-Rotax GmbH & Co. KG

发明人： Thomas Koch ,  Heinz Lippitsch ,  Johann Bayerl ,  Manfred Moseneder ,  Gerald Mayr

IPC分类号： F02D023/00

CPC分类号： F02D29/02 ,  B64C11/305 ,  B64C11/40 ,  B64C11/44 ,  B64D31/14 ,  F02B37/186 ,  F02D23/02 ,  Y02T10/144

摘要： An aircraft control system includes a propeller governor in which a stepper motor is used to apply a compression force on a speeder spring, and a turbocharger in which a stepper motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the stepper motor in the propeller governor and the stepper motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.

摘要翻译： 飞机控制系统包括螺旋桨调速器，其中步进马达用于对加速器弹簧施加压缩力;以及涡轮增压器，其中步进马达用于致动与隔膜单元相关联的针阀。 电子控制单元可用于控制螺旋桨调速器中的步进电机和涡轮增压器中的步进电机。 螺旋桨调速器和涡轮增压器集成到单个控制系统中可减少必须由飞行员手动执行的单独调整次数。

公开(公告)号：US20040016233A1

公开(公告)日：2004-01-29

申请号：US10602612

申请日：2003-06-25

发明人： Gianfranco Natali

IPC分类号： F02D023/00

CPC分类号： F02B37/186 ,  F02B37/12 ,  F02B37/24 ,  F02D41/0007 ,  F16K31/105 ,  Y02T10/144

摘要： An actuator composed of: a) a solenoid (1) with a ferromagnetic nucleus (2) which slides inside it and is combined with a rod (3) appropriate for interacting with the turbocharger's (5) pilot point (4) and provided with a sensing system (7) of the position of the ferromagnetic nucleus (2) in the solenoid (1); b) and an electronic circuit which:nullon the way in receives at least the signal from the engine's electronic control unit and the feedback signal, connected to the position of the ferromagnetic nucleus (2) of the solenoid (1);nullon the way out it distributes the electric current, connected to the said entry signals, with which it feeds the same solenoid (1).

摘要翻译： 一种致动器，包括：a）具有铁磁核（2）的螺线管（1），其在内部滑动并与适于与涡轮增压器（5）导向点（4）相互作用的杆（3）组合并且设置有 感测系统（7）中螺线管（1）中的铁磁核（2）的位置; b）和电子电路，其 - 在至少接收到来自发动机的电子控制单元的信号和连接到螺线管（1）的铁磁核（2）的位置的反馈信号的途中） - 在 出口它分配电流，连接到所述输入信号，其馈送相同的螺线管（1）。

公开(公告)号：US20040016232A1

公开(公告)日：2004-01-29

申请号：US10424246

申请日：2003-04-28

发明人： Oliver A. Warner ,  Mark A. Zurawski ,  Andrew May

IPC分类号： F02D013/04 ,  F02D009/06 ,  F02D023/00

CPC分类号： F02D13/04

摘要： A method of controlling an internal combustion engine when the engine is operating in an engine braking mode is provided. The engine operates in the engine braking mode and an exhaust valve for the cylinder is prematurely opened to dissipate power. The method includes controlling airflow to at least one cylinder based on a comparison of a desired mass airflow rate and an actual mass airflow rate such that the actual mass airflow rate tracks the desired mass airflow rate.

摘要翻译： 提供了一种当发动机以发动机制动模式操作时控制内燃机的方法。 发动机在发动机制动模式下工作，并且用于气缸的排气阀被过早地打开以消散功率。 该方法包括基于所需质量气流速率和实际质量气流速率的比较来控制至少一个气缸的气流，使得实际质量气流速率跟踪期望的质量气流速率。

公开(公告)号：US20040011035A1

公开(公告)日：2004-01-22

申请号：US10199703

申请日：2002-07-19

发明人： Steven Don Arnold

IPC分类号： F02D023/00

CPC分类号： F02B37/24 ,  F02D41/0007 ,  Y02T10/144

摘要： A control system of this invention for use with a variable geometry turbocharger is designed to enable turbocharger control based solely on engine speed. The control system takes measured engine speed and sends the same to an engine control unit (ECU) having an actuator position v. engine speed map. The ECU utilizes only the measured engine speed to determine a desired actuator position from the map, and produces a control signal for effecting actuator operation. The control signal generated by the ECU can be converted to an analog signal by pulse width modulation, for example. The control signal is sent to an actuator for placing the actuator into the desired actuator position. The actuator is connected to a variable geometry member in the turbocharger so that operation and placement of the actuator into the desired actuator position thereby places the variable geometry member into a desired position to effect the desired change in turbocharger operation. In an example embodiment, the variably geometry member is a number of movable vanes that can be positioned to change the amount of exhaust gas flow directed to a turbine wheel of the turbocharger.

摘要翻译： 本发明的用于可变几何形状涡轮增压器的控制系统被设计成仅基于发动机转速实现涡轮增压器控制。 控制系统测量发动机转速并将其发送到具有执行器位置v。发动机转速图的发动机控制单元（ECU）。 ECU仅利用测量的发动机速度从地图确定期望的致动器位置，并且产生用于实现致动器操作的控制信号。 例如，由ECU产生的控制信号可以通过脉宽调制转换为模拟信号。 控制信号被发送到致动器，以将致动器放置在期望的致动器位置。 致动器连接到涡轮增压器中的可变几何构件，使得致动器的操作和放置到期望的致动器位置，从而将可变几何构件放置在期望位置以实现涡轮增压器操作期望的变化。 在示例性实施例中，可变几何构件是多个可移动叶片，其可被定位成改变被引导到涡轮增压器的涡轮机叶轮的废气流量。

公开(公告)号：US20030182940A1

公开(公告)日：2003-10-02

申请号：US10402066

申请日：2003-03-27

申请人： Komatsu Ltd.

发明人： Toshihiko Nishiyama ,  Hiroshi Sugito ,  Takahisa Iino

IPC分类号： F02D023/00

CPC分类号： F02D41/0007 ,  F02B37/24 ,  Y02T10/144

摘要： The present invention provides a variable nozzle opening control unit insuring a low fuel consumption rate and excellent response speed in the low load mode for an exhaust turbine supercharger. To achieve the purpose described above, an opening of the variable nozzle of the exhaust turbine supercharger 10 is set to and maintained at the maximum value in the constant operating state when the load is not more than a prespecified load level, and also the opening is gradually made smaller, when the load is not less than the specified load level, as the load becomes higher. When the load shifts from the high load region to the low load region, the variable nozzle is more closed or maintained at the original opening. Further when the operating state may get close to the surging limit, the variable nozzle is more opened. When shifting from the low load region to the high load region, or when sifting from the low speed to the high speed, the variable nozzle is once opened more, and then closed more to return to the constant operating state.

摘要翻译： 本发明提供了一种可变喷嘴开度控制单元，其确保在用于排气涡轮增压器的低负载模式下的低燃料消耗率和优异的响应速度。 为了实现上述目的，当负载不大于预定的负载水平时，排气涡轮增压器10的可变喷嘴的开度被设定为并保持在恒定运行状态下的最大值，并且开度是 逐渐变小，当负载不小于规定的负载水平时，负载变得更高。 当负载从高负载区域移动到低负载区域时，可变喷嘴更加闭合或保持在原始开口处。 此外，当操作状态可能接近浪涌极限时，可变喷嘴更开放。 当从低负载区域移动到高负载区域时，或者从低速到高速的过滤时，可变喷嘴一次打开，然后再闭合以返回到恒定的运行状态。

公开(公告)号：US20030167767A1

公开(公告)日：2003-09-11

申请号：US10091780

申请日：2002-03-05

发明人： Steven Don Arnold

IPC分类号： F02D023/00 ,  F01D017/12 ,  F04D015/00

CPC分类号： F01D17/12 ,  F01D17/165 ,  F02B37/24 ,  F02D23/00 ,  F04D25/04 ,  F04D29/462 ,  F05D2220/40 ,  Y02T10/144

摘要： A turbocharger comprises a center housing, and a shaft positioned therein having a first end and a second end. A turbine housing is attached to one side of the center housing and has a turbine wheel disposed therein that is coupled to the first end of the shaft. A first variable geometry member is disposed within the turbine housing between an exhaust gas inlet and the turbine wheel. A compressor housing is attached to another side of the center housing opposite the turbine housing, and includes a compressor impeller disposed therein. The compressor impeller is coupled to the second end of the shaft. A second variable geometry member is disposed within the compressor housing, and is interposed between an air outlet and the compressor impeller. An actuator assembly is disposed within the turbocharger and is connected to both of the variable geometry members to provide simultaneous actuation of the same.

摘要翻译： 涡轮增压器包括中心壳体和位于其中的具有第一端和第二端的轴。 涡轮机壳体附接到中心壳体的一侧，并且具有设置在其中的涡轮机叶轮，其联接到轴的第一端。 第一可变几何构件设置在涡轮机壳体内的废气入口和涡轮机叶轮之间。 压缩机壳体附接到与涡轮机壳体相对的中心壳体的另一侧，并且包括设置在其中的压缩机叶轮。 压缩机叶轮联接到轴的第二端。 第二可变几何构件设置在压缩机壳体内，并且介于空气出口和压缩机叶轮之间。 致动器组件设置在涡轮增压器内并且连接到两个可变几何构件以提供同时致动。

公开(公告)号：US20030121263A1

公开(公告)日：2003-07-03

申请号：US10319100

申请日：2002-12-13

申请人： Isuzu Motors Limited

发明人： Shoshi Hidaka

IPC分类号： F02D023/00

CPC分类号： F02B37/24 ,  F02D2041/1422 ,  F02M26/05 ,  F02M26/23 ,  F02M63/0225 ,  Y02T10/144

摘要： The wasteful escape of exhaust energy during transitional operation of the engine due to unnecessary opening control of the nozzle vanes is prevented. In a control device for a variable-geometry turbocharger which allows adjustment of the opening of the nozzle in the turbine inlet, the basic opening target value of the nozzle is calculated on the basis of the actual engine rotational speed and load. The final opening target value of the nozzle is then calculated by adding a nozzle opening correction value VNta to this basic opening target value. In the calculation of this nozzle opening correction value VNta, the amount of variation nullAc in the engine load is multiplied by a correction gain calculated on the basis of the engine rotational speed and pressure ratio, and a filter processing using a specified transmission function is performed on the resulting value nullAc1. The amount of variation in load nullAc2 following this filter processing is used as the input value for the calculation of the nozzle opening correction value VNta.

摘要翻译： 防止由于喷嘴叶片的不必要的打开控制而在发动机的过渡操作期间排气能量的浪费。 在可变形涡轮增压器的控制装置中，其可以调节涡轮机入口处的喷嘴的开度，基于实际的发动机转速和负载来计算喷嘴的基本开启目标值。 然后通过将喷嘴开口校正值VNta与该基本打开目标值相加来计算喷嘴的最终打开目标值。 在该喷嘴开度校正值VNta的计算中，将发动机负荷中的变化量DELTAAc乘以基于发动机转速和压力比计算的校正增益，并且执行使用规定的传动功能的过滤器处理 对结果值DELTAAc1。 使用该滤波处理之后的负载DELTAAc2的变化量用作计算喷嘴开度校正值VNta的输入值。