Exhaust gas turbocharger turbine
    1.
    发明授权
    Exhaust gas turbocharger turbine 失效
    废气涡轮增压器涡轮机

    公开(公告)号:US06443696B1

    公开(公告)日:2002-09-03

    申请号:US09673329

    申请日:2000-10-12

    Abstract: An exhaust-gas turbocharger turbine of an internal combustion engine is provided with a spiral guide passage arranged in a turbine housing, a turbine impeller, a flow gap be ween the guide passage and the turbine impeller, and guide blades forming a guide cascade. The guide cascade with the guide blades projects axially from a support, arranged so as to be displaceable in the axial direction in the turbine housing, in such a way that the guide blades, in normal operation, are mounted in recesses of a housing wall part of the turbine housing, the recesses, in the form of a female piece, forming a mating profile shape for the guide blades. In braking operation of the internal combustion engine, the guide blades project into the flow gap during an axial displacement of the support. The device with actuation for the braking operation can be fitted as a complete module into the turbine spiral.

    Abstract translation: 内燃机的排气涡轮增压器涡轮机设置有涡轮机壳体,涡轮叶轮,引导通道和涡轮机叶轮的流动间隙以及形成引导级联的引导叶片的螺旋引导通道。 与引导叶片的引导级联从支撑件轴向突出,布置成在涡轮机壳体中沿轴向移位,使得导向叶片在正常操作中安装在壳体壁部分的凹部中 涡轮机壳体的凹部,以阴形件的形式形成用于导向叶片的配合轮廓形状。 在内燃机的制动操作中,导向叶片在支撑件的轴向位移期间突出到流动间隙中。 具有用于制动操作的致动装置可以作为完整模块装配到涡轮螺旋中。

    Liquid cooled cylinder head
    2.
    发明授权
    Liquid cooled cylinder head 有权
    液冷缸头

    公开(公告)号:US06412452B1

    公开(公告)日:2002-07-02

    申请号:US09625556

    申请日:2000-07-25

    CPC classification number: F02F1/40 F02F1/4214 F02F2001/241 F02F2001/247

    Abstract: In an internal combustion engine, with a cylinder head having a coolant space associated with each combustion chamber, wherein the coolant space comprises, for each cylinder of the engine, a first coolant chamber and a second coolant chamber separate from one another, the coolant space has a coolant inlet which extends to the outside and is connected to a coolant supply line for directly supplying coolant from the outside to the first and second coolant chambers.

    Abstract translation: 在内燃机中,具有与每个燃烧室相关联的冷却剂空间的气缸盖,其中,对于发动机的每个气缸,冷却剂空间包括彼此分离的第一冷却剂室和第二冷却剂室,冷却剂空间 具有向外部延伸并连接到冷却剂供应管线的冷却剂入口,用于将冷却剂从外部直接供应到第一和第二冷却剂室。

    Engine-braking arrangement for an internal combustion engine with an exhaust-gas turbocharger
    3.
    发明授权
    Engine-braking arrangement for an internal combustion engine with an exhaust-gas turbocharger 有权
    具有排气涡轮增压器的内燃机的发动机制动装置

    公开(公告)号:US06223534B1

    公开(公告)日:2001-05-01

    申请号:US09370194

    申请日:1999-08-09

    CPC classification number: F02B37/025 F02D9/06 F02D9/16 Y02T10/144

    Abstract: In an engine braking arrangement for an internal combustion engine with an exhaust gas turbocharger including a turbine arranged in the engine exhaust duct and a compressor driven by the turbine and arranged in the engine intake duct, a brake valve disposed in the exhaust duct upstream of the turbine and a pressure relief line extending from the exhaust duct upstream of the turbine rotor to an area downstream of the turbine and including a stop valve, the stop valve is a rotationally adjustable rotary valve operable by an actuating device depending on the intake pressure in the intake duct.

    Abstract translation: 在具有排气涡轮增压器的内燃机的发动机制动装置中,所述排气涡轮增压器包括布置在所述发动机排气管道中的涡轮机和由所述涡轮机驱动并设置在所述发动机进气管道中的压缩机,设置在所述排气管道上游的制动阀 涡轮机和从涡轮转子上游的排气管道延伸到涡轮机下游的区域并包括截止阀的压力释放管线,该截止阀是可旋转地调节的旋转阀,其可由致动装置操作,这取决于在 进气管。

    Exhaust gas turbine of a turbocharger for an internal combustion engine
    4.
    发明授权
    Exhaust gas turbine of a turbocharger for an internal combustion engine 有权
    用于内燃机的涡轮增压器的废气涡轮

    公开(公告)号:US06314736B1

    公开(公告)日:2001-11-13

    申请号:US09558834

    申请日:2000-04-26

    CPC classification number: F01D17/16 F01D11/00 F01D17/165

    Abstract: An exhaust gas turbine portion of a vehicle engine turbocharger is provided with at least one variable guide-blade cascade with guide blades in a nozzle opening to the turbocharger rotor for effectively changing the cross section of the exhaust flow to the rotor wherein the angle of the guide blades is selectively settable by an adjusting device. The width dimension of the gap between the ends of the guide-blade cascade and the casing wall defining the nozzle is adjustable between a substantially zero gap dimension and a maximum gap dimension.

    Abstract translation: 车辆发动机涡轮增压器的废气涡轮机部分设置有至少一个与导向叶片级联的可变导向叶片,该导向叶片在与涡轮增压器转子相关的喷嘴开口中,用于有效地改变排气流到转子的横截面,其中, 导向叶片可由调节装置选择性地设定。 引导叶片级联的端部与限定喷嘴的壳体壁之间的间隙的宽度尺寸可在基本上零间隙尺寸和最大间隙尺寸之间调节。

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