Methods and apparatus for controlling peak firing pressure for turbo-charged diesel engines
    121.
    发明授权
    Methods and apparatus for controlling peak firing pressure for turbo-charged diesel engines 有权
    用于控制涡轮增压柴油发动机峰值点火压力的方法和装置

    公开(公告)号:US06557347B1

    公开(公告)日:2003-05-06

    申请号:US10284595

    申请日:2002-10-31

    Abstract: A method and apparatus of operating a turbo-charged diesel locomotive engine to facilitate controlling pressure in an engine cylinder is provided. The method includes determining an allowable peak firing pressure for the turbo-charged diesel engine, determining an actual peak firing pressure, and comparing the allowable peak firing pressure to actual peak firing pressure to control the operation of the turbocharger for controlling peak firing pressure. The apparatus includes a diesel engine including an intake manifold, an exhaust manifold, an electronic fuel controller, a turbo-charger, and a motor-generator coupled to the turbocharger and operable to at least one of increase turbocharger rotational speed, decrease turbocharger rotational speed, and maintain turbocharger rotational speed, and a controller including a first input corresponding intake manifold air pressure and a second input corresponding to fuel injection timing for the engine and including as an output a motor-generator configuration signal.

    Abstract translation: 提供了一种操作涡轮增压柴油机车发动机以便于控制发动机气缸中的压力的​​方法和装置。 该方法包括确定用于涡轮增压柴油发动机的允许峰值点火压力,确定实际峰值点火压力,以及将容许峰值点火压力与实际峰值点火压力进行比较,以控制用于控制峰值点火压力的涡轮增压器的运行。 该装置包括柴油发动机,其包括进气歧管,排气歧管,电子燃料控制器,涡轮增压器和联接到涡轮增压器的电动发电机,并可操作以增加涡轮增压器转速,降低涡轮增压器转速 并且保持涡轮增压器转速,以及控制器,其包括对应于所述发动机的燃料喷射正时的第一输入对应的进气歧管空气压力和第二输入,并且包括电动发电机配置信号作为输出。

    Multiple parallel turbocharger control with discrete step nozzles
    122.
    发明授权
    Multiple parallel turbocharger control with discrete step nozzles 有权
    具有离散步进喷嘴的多平行涡轮增压器控制

    公开(公告)号:US06550247B1

    公开(公告)日:2003-04-22

    申请号:US09943175

    申请日:2001-08-30

    Inventor: John R. Gladden

    CPC classification number: F02B37/24 F02B37/007 Y02T10/144

    Abstract: A control for a turbocharger system in an internal combustion engine particularly useful for multiple parallel turbochargers having turbines with discrete step variable nozzles. In response to a need for adjustment the variable nozzles are adjusted sequentially, not simultaneously. Sequential adjustment of the turbines minimizes the impact of the adjustment.

    Abstract translation: 用于内燃机中的涡轮增压器系统的控制装置,其特别适用于具有离散步长可变喷嘴的涡轮机的多个平行涡轮增压器。 响应于需要调节,可变喷嘴被顺序地调节,而不是同时调节。 涡轮机的顺序调节使调整的影响最小化。

    Two turbocharger engine emission control system
    123.
    发明授权
    Two turbocharger engine emission control system 有权
    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

    Abstract: 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.

    Abstract translation: 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。

    Exhaust turbocharger for internal combustion engine and turbocharging system

    公开(公告)号:US06457310B1

    公开(公告)日:2002-10-01

    申请号:US09790529

    申请日:2001-02-23

    CPC classification number: F01D25/183

    Abstract: A turbine impeller to be driven for rotation by exhaust gas of an internal combustion engine is fixed to a turbine shaft. The turbine shaft is supported by a radial bearing in radial directions and mounted to a bearing housing. The turbine shaft includes a stepped part which is formed between the turbine impeller and the radial bearing so that the outer diameter of the turbine shaft is greater at the turbine impeller side than at the radial bearing side. The bearing housing includes an oil drain for discharging oil which has lubricated the radial bearing. The distance L from a side face of the radial bearing to the stepped part is set to a value at which oil moving from an end of the radial bearing does not reach the stepped part when a turbine-revolution speed Nt is higher than that Nti which is produced by an idling operation of the internal combustion engine.

    Single stage or multi-stage compressor for a turbocharger
    125.
    发明授权
    Single stage or multi-stage compressor for a turbocharger 失效
    用于涡轮增压器的单级或多级压缩机

    公开(公告)号:US06442936B1

    公开(公告)日:2002-09-03

    申请号:US09737110

    申请日:2000-12-14

    Inventor: Phillip J. Houtz

    Abstract: A turbocharger for an internal combustion engine has a compressor operable as a single stage or multi-stage compressor. A first compressor stage includes a first compressor wheel carried by a shaft, an axially extending first inlet and a radially extending first outlet. A second compressor stage includes a second compressor wheel carried by the shaft and axially extending second inlet and a radially extending second outlet. An interstage duct fluidly connects in series the first outlet of the first compressor with the second inlet of the second compressor. The interstage duct includes a bypass opening includes in communication with an ambient environment. A valve is positioned within the interstage duct. The valve is moveable to and between a first position to close the interstage duct and a second position to close the bypass opening.

    Abstract translation: 用于内燃机的涡轮增压器具有可操作为单级或多级压缩机的压缩机。 第一压缩机级包括由轴承载的第一压缩机叶轮,轴向延伸的第一入口和径向延伸的第一出口。 第二压缩机级包括由轴承载的第二压缩机叶轮和轴向延伸的第二入口和径向延伸的第二出口。 级间管道将第一压缩机的第一出口与第二压缩机的第二入口串联连接。 级间管道包括与周围环境连通的旁路开口。 阀门位于级间管道内。 阀可以移动到第一位置之间并且在第一位置之间移动以关闭级间管道和第二位置以关闭旁路开口。

    Method of operating an internal-combustion engine, and internal-combustion engine
    126.
    发明授权
    Method of operating an internal-combustion engine, and internal-combustion engine 失效
    操作内燃机和内燃机的方法

    公开(公告)号:US06438956B1

    公开(公告)日:2002-08-27

    申请号:US09806317

    申请日:2001-04-20

    Applicant: Eric Olofsson

    Inventor: Eric Olofsson

    CPC classification number: F02D23/00 F01N13/107 F02B37/02 Y02T10/144

    Abstract: In an internal-combustion engine (1) of the Otto type, in which exhaust gases are used in order to drive a turbocompressor (14, 15) for supercharging the engine, the engine is designed in such a manner that it can, at high load, be run with a lean mixture during supercharging, the air/fuel ratio being at least 19:1. The lean mixture is brought about by virtue of the fact that the charging pressure increases while the fuel quantity is maintained. The engine is advantageously provided with a divided exhaust-gas discharge in order to improve the operating characteristics.

    Abstract translation: 在奥托式的内燃机(1)中,其中使用排气来驱动用于对发动机进行增压的涡轮压缩机(14,15),发动机的设计方式可以是高的 加载时,在增压过程中,用稀混合物运行,空气/燃料比至少为19:1。 由于在保持燃料量的同时充气压力增加的事实而产生贫混合物。 发动机有利地设置有分开的废气排放,以便改善操作特性。

    Low pressure gaseous fuel system
    127.
    发明授权
    Low pressure gaseous fuel system 失效
    低压气体燃料系统

    公开(公告)号:US06418723B1

    公开(公告)日:2002-07-16

    申请号:US09666818

    申请日:2000-09-21

    Inventor: John R. Gladden

    Abstract: A low pressure fuel system for a gaseous fuel internal combustion engine in which the source of gaseous fuel is at a pressure lower than the intake manifold pressure of the internal combustion engine. The gaseous fuel is inducted into the interstage duct of a multi-compressor combustion air turbocharger associated with the internal combustion engine. The combined flow of air and gaseous fuel is further compressed in the second compressor stage of the turbocharger.

    Abstract translation: 一种用于气体燃料内燃机的低压燃料系统,其中气态燃料源的压力低于内燃机的进气歧管压力。 气体燃料被引入到与内燃机相关联的多压缩机燃烧空气涡轮增压器的级间管道中。 在涡轮增压器的第二压缩机级中进一步压缩空气和气体燃料的组合流。

    Turbocharger bearing system
    128.
    发明授权
    Turbocharger bearing system 有权
    涡轮增压器轴承系统

    公开(公告)号:US06418722B1

    公开(公告)日:2002-07-16

    申请号:US09838721

    申请日:2001-04-19

    Abstract: An enhanced bearing system for turbochargers incorporates a thrust collar centrally mounted on the rotating shaft interconnecting the turbine and compressor and a thrust bearing centrally located within the center housing to constrain the thrust collar. Central placement of the thrust collar allows journal bearings and journal seals to be placed immediately adjacent the turbine and compressor wheel attachment points on the shaft enhancing the shaft motion characteristics and sealing capability.

    Abstract translation: 用于涡轮增压器的增强的轴承系统包括中心地安装在互连涡轮机和压缩机的旋转轴上的推力轴环和位于中心壳体内的中心的止推轴承,以约束推力轴环。 止推环的中心布置允许轴颈轴承和轴颈密封件紧紧地放置在轴上的涡轮机和压缩机叶轮附接点上,增强轴的运动特性和密封能力。

    Method and apparatus for turbocharging an engine of a locomotive
    129.
    发明授权
    Method and apparatus for turbocharging an engine of a locomotive 有权
    用于对机车的发动机进行涡轮增压的方法和装置

    公开(公告)号:US06415606B1

    公开(公告)日:2002-07-09

    申请号:US09617968

    申请日:2000-10-02

    CPC classification number: F02B37/14 F02B37/10 F02B39/10 F02D41/0007 Y02T10/144

    Abstract: The method for turbocharging an engine of a locomotive in which the engine is operable at a plurality of discrete operating power levels includes controlling at least one of energy to a motor-assisted turbocharger at a plurality of discrete energy levels and air pressure from the motor-assisted turbocharger to the engine at a plurality of discrete air pressure levels above ambient air pressure based on at least some of the plurality of discrete operating power levels (e.g., low power levels) of the engine. Desirably, the method also includes controlling generation of electrical energy from the motor-assisted turbocharger at some of the plurality of discrete operating power levels (e.g., high power levels) of the engine. Apparatus for turbocharging a diesel engine of a locomotive incorporating the above methods are also disclosed.

    Abstract translation: 用于对机车的发动机进行涡轮增压的方法,其中所述发动机可以在多个离散的操作功率水平下操作,所述方法包括以多个离散的能量级别和来自所述电动机的空气压力将至少一个能量控制到电动辅助涡轮增压器, 基于发动机的多个离散操作功率水平(例如,低功率水平)中的至少一些,辅助涡轮增压器以高于环境空气压力的多个离散空气压力水平向发动机提供。 期望地,该方法还包括在发动机的多个离散操作功率水平(例如,高功率水平)中的某些处控制来自马达辅助涡轮增压器的电能的产生。 还公开了包含上述方法的机车的柴油发动机涡轮增压装置。

    Device for limiting the speed of an exhaust-gas turbocharger
    130.
    发明授权
    Device for limiting the speed of an exhaust-gas turbocharger 有权
    用于限制排气涡轮增压器速度的装置

    公开(公告)号:US06378306B2

    公开(公告)日:2002-04-30

    申请号:US09785683

    申请日:2001-02-16

    CPC classification number: F02B37/18 F02B2039/168 Y02T10/144

    Abstract: A device for limiting the supercharger speed which makes do without a speed sensor or an atmospheric pressure sensor has a bandpass filter which filters out a spectral component from the output signal of a boost pressure sensor arranged in the induction pipe of the engine, the spectral component appearing in the signal spectrum of the boost pressure sensor when the air column in the induction pipe is set into a vibration which develops when the compressor of the turbocharger rotates at the maximum permissible speed.

    Abstract translation: 用于限制没有速度传感器或大气压力传感器的增压器速度的装置具有带通滤波器,其从布置在发动机的感应管中的增压压力传感器的输出信号滤除频谱分量,频谱分量 出现在增压压力传感器的信号频谱中,当感应管中的空气柱被设定为当涡轮增压器的压缩机以最大允许速度旋转时产生的振动。

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