TURBINE FOR AN EXHAUST GAS TURBOCHARGER
    1.
    发明申请
    TURBINE FOR AN EXHAUST GAS TURBOCHARGER 有权
    用于排气烟囱的涡轮机

    公开(公告)号:US20130327038A1

    公开(公告)日:2013-12-12

    申请号:US13907934

    申请日:2013-06-02

    Applicant: DAIMLER AG

    Abstract: In a turbine for an exhaust gas turbocharger of an internal combustion engine having a housing part with accommodation space including a turbine wheel and at least one spiral channel via which exhaust gas of the internal combustion engine may flow. The spiral channel has an outlet cross-section via which the turbine wheel accommodated in the accommodation space may be acted on by the exhaust gas, and has at least one blocking member, which is connected to an adjusting part so as to be movable hereby in the peripheral direction of the accommodation space for adjusting the outlet cross-section (AR, ARλ, AR,RGR). A bypass duct is provided, via, which exhaust gas can bypass the turbine wheel and whose flow cross-section is also adjustable by the blocking member moved the adjusting part.

    Abstract translation: 一种用于内燃机的排气涡轮增压器的涡轮机,具有具有容纳空间的壳体部分,该容纳部分包括涡轮机叶轮和至少一个螺旋通道,内燃机的废气可以通过该螺旋通道流动。 螺旋通道具有出口横截面,通过该出口横截面,容纳在容纳空间中的涡轮机轮可以被排气作用,并且具有至少一个阻挡构件,该阻挡构件连接到调节部件,以便在此可移动 用于调节出口横截面(AR,ARl,AR,RGR)的容纳空间的周向方向。 旁通管道经由该废气可以绕过涡轮机叶轮,并且其流动横截面也可通过阻挡构件移动调整部件来调节。

    Turbine for and exhaust gas turbocharger
    2.
    发明授权
    Turbine for and exhaust gas turbocharger 有权
    涡轮机和废气涡轮增压器

    公开(公告)号:US08997485B2

    公开(公告)日:2015-04-07

    申请号:US13684543

    申请日:2012-11-25

    Applicant: Daimler AG

    CPC classification number: F01D17/143 F01D9/026 F01D25/26 F05D2220/40

    Abstract: In a turbine for an exhaust gas turbocharger of an internal combustion engine comprising a turbine housing part, which has at least two spiral channels with respective inlets through which exhaust gas of the internal combustion engine is directed onto a turbine rotor disposed in the turbine housing part, the turbine housing part is disposed in an accommodating chamber, which is formed by a further housing part of the turbine, and from which accommodating chamber exhaust gas of the internal combustion engine can flow through the channel inlets into the spiral channels.

    Abstract translation: 在用于内燃机的废气涡轮增压器的涡轮机中,该涡轮机壳体部分具有至少两个具有相应入口的螺旋通道,涡轮机壳体部分具有各自的入口,内燃机的废气通过该入口引导到设置在涡轮机壳体部分中的涡轮转子上 涡轮机壳体部分设置在由涡轮机的另外的壳体部分形成的容纳室中,并且内燃机的容纳室排气可以从该通道入口进入螺旋通道。

    INSERT ELEMENT FOR A TURBINE OF AN EXHAUST GAS TURBOCHERGER, EXHAUST GAS TURBOCHARGER AND TURBINE FOR AN EXHAUST GAS TURBOCHARGER
    3.
    发明申请
    INSERT ELEMENT FOR A TURBINE OF AN EXHAUST GAS TURBOCHERGER, EXHAUST GAS TURBOCHARGER AND TURBINE FOR AN EXHAUST GAS TURBOCHARGER 审中-公开
    用于排气的涡轮机的排气元件,用于排气的涡轮增压器的排气涡轮增压器和涡轮机

    公开(公告)号:US20130330178A1

    公开(公告)日:2013-12-12

    申请号:US13893278

    申请日:2013-05-13

    Applicant: DAIMLER AG

    CPC classification number: F01D17/14 F01D17/141 F02C6/12 F05D2220/40

    Abstract: In a turbine of an exhaust gas turbocharger an insert element which is provided for insertion into a turbine housing has a spiral port which extends in the circumferential direction of the insert element over at least part of the circumference thereof and by which the exhaust gas flow through the turbine is controlled. The insert element is open in the axial direction on at least at one end face thereof which end face is biased in sealing contact with the turbine housing. The insert element has a central axial opening with a spiral port for accommodating a turbine wheel.

    Abstract translation: 在废气涡轮增压器的涡轮机中,设置用于插入涡轮机壳体中的插入元件具有在插入元件的圆周方向上在其周边的至少一部分上延伸的螺旋形端口,并且排气流过 涡轮机被控制。 插入元件至少在其一个端面处在轴向方向上敞开,该端面被偏压以与涡轮壳体密封接触。 插入元件具有中心轴向开口,其具有用于容纳涡轮机叶轮的螺旋端口。

    Turbine for an exhaust gas turbocharger
    4.
    发明授权
    Turbine for an exhaust gas turbocharger 有权
    用于排气涡轮增压器的涡轮机

    公开(公告)号:US09291092B2

    公开(公告)日:2016-03-22

    申请号:US13907934

    申请日:2013-06-02

    Applicant: DAIMLER AG

    Abstract: In a turbine for an exhaust gas turbocharger of an internal combustion engine having a housing part with accommodation space including a turbine wheel and at least one spiral channel via which exhaust gas of the internal combustion engine may flow. The spiral channel has an outlet cross-section via which the turbine wheel accommodated in the accommodation space may be acted on by the exhaust gas, and has at least one blocking member, which is connected to an adjusting part so as to be movable hereby in the peripheral direction of the accommodation space for adjusting the outlet cross-section (AR, ARλ, AR,RGR). A bypass duct is provided, via which exhaust gas can bypass the turbine wheel and whose flow cross-section is also adjustable by the blocking member moved the adjusting part.

    Abstract translation: 一种用于内燃机的排气涡轮增压器的涡轮机,具有具有容纳空间的壳体部分,该容纳部分包括涡轮机叶轮和至少一个螺旋通道,内燃机的废气可以通过该螺旋通道流动。 螺旋通道具有出口横截面,通过该出口横截面,容纳在容纳空间中的涡轮机轮可以被排气作用,并且具有至少一个阻挡构件,该阻挡构件连接到调节部件,以便在此可移动 用于调节出口横截面(AR,ARλ,AR,RGR)的容纳空间的周向方向。 提供旁通管道,通过该旁路管道,废气可以绕过涡轮机叶轮,并且其流动横截面也可通过阻挡构件移动调节部件来调节。

    Turbine for an exhaust turbocharger of an internal combustion engine
    5.
    发明授权
    Turbine for an exhaust turbocharger of an internal combustion engine 有权
    用于内燃机排气涡轮增压器的涡轮机

    公开(公告)号:US09121345B2

    公开(公告)日:2015-09-01

    申请号:US13897400

    申请日:2013-05-18

    Applicant: DAIMLER AG

    CPC classification number: F02C7/00 F01D17/141 F01D17/167 F05D2220/40

    Abstract: In a turbine for an exhaust gas turbocharger of an internal combustion engine having a housing part which has a receiving chamber and which comprises a spiral duct through which exhaust gas of the internal combustion engine can flow, the spiral duct having an outlet cross-section via which exhaust gas is directed onto a turbine wheel disposed in the receiving chamber whereby the turbine wheel can be rotated, at least one flow control member is provided which can be moved in the circumferential direction of the receiving chamber and by means of which the flow cross-section can be adjusted, wherein a warp angle of the outer contour region of the wall over which the flow cross-section can be adjusted is smaller than a wrap angle over which the outer contour region thereof extends.

    Abstract translation: 在内燃机的排气涡轮增压器的涡轮机中,具有具有容纳室的壳体部分的内燃机的涡轮增压器,其包括内燃机的废气能够流过的螺旋管道,螺旋管道具有出口横截面通过 该排气被引导到设置在容纳室中的涡轮机叶轮上,由此涡轮机叶轮可以旋转,设置至少一个流动控制构件,该流动控制构件可以在接收室的圆周方向上移动,并且通过该流动交叉 可以调节切片,其中可以调节流动横截面的壁的外轮廓区域的翘角小于其外轮廓区域延伸的包角。

    TURBINE FOR AN EXHAUST TURBOCHARGER OF AN INTERNAL COMBUSTION ENGINE
    7.
    发明申请
    TURBINE FOR AN EXHAUST TURBOCHARGER OF AN INTERNAL COMBUSTION ENGINE 有权
    用于内燃机排气涡轮机的涡轮机

    公开(公告)号:US20130276444A1

    公开(公告)日:2013-10-24

    申请号:US13897400

    申请日:2013-05-18

    Applicant: DAIMLER AG

    CPC classification number: F02C7/00 F01D17/141 F01D17/167 F05D2220/40

    Abstract: In a turbine for an exhaust gas turbocharger of an internal combustion engine having a housing part which has a receiving chamber and which comprises a spiral duct through which exhaust gas of the internal combustion engine can flow, the spiral duct having an outlet cross-section via which exhaust gas is directed onto a turbine wheel disposed in the receiving chamber whereby the turbine wheel can be rotated, at least one flow control member is provided which can be moved in the circumferential direction of the receiving chamber and by means of which the flow cross-section can be adjusted, wherein a warp angle of the outer contour region of the wall over which the flow cross-section can be adjusted is smaller than a wrap angle over which the outer contour region thereof extends.

    Abstract translation: 在内燃机的排气涡轮增压器的涡轮机中,具有具有容纳室的壳体部分的内燃机的涡轮增压器,其包括内燃机的废气能够流过的螺旋管道,螺旋管道具有出口横截面通过 该排气被引导到设置在容纳室中的涡轮机叶轮上,由此涡轮机叶轮可以旋转,设置至少一个流动控制构件,该流动控制构件可以在接收室的圆周方向上移动,并且通过该流动交叉 可以调节切片,其中可以调节流动横截面的壁的外轮廓区域的翘角小于其外轮廓区域延伸的包角。

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