Exhaust-gas turbine in an exhaust-gas turbocharger
    1.
    发明申请
    Exhaust-gas turbine in an exhaust-gas turbocharger 失效
    排气涡轮增压器中的废气涡轮机

    公开(公告)号:US20080152484A1

    公开(公告)日:2008-06-26

    申请号:US12001078

    申请日:2007-12-08

    IPC分类号: F02B37/24 F04D15/00

    CPC分类号: F02C6/12 F01D17/143 F02C9/18

    摘要: In an exhaust-gas turbine of an exhaust-gas turbo-charger including a turbine wheel which is rotatably supported in a housing and to which exhaust gas can be supplied via an inlet channel and discharged out of the exhaust-gas turbine via an outlet duct, wherein a guide vane structure and an axial slide which interacts with the latter, are disposed in the turbine inlet at the transition from the inlet channel to the turbine wheel, the guide vane structure is fixedly mounted with respect to the housing and the axial slide is arranged at the turbine outlet side and is movably supported on an outlet duct contour sleeve and provided with an axial opening for accommodating the guide vane structure, and the contour sleeve includes openings which conduct exhaust gas from the inlet channel directly to the outlet duct and which are arranged so that they are covered by the axial slide when the axial slide is moved out of its open position, the guide vane structure extending axially over the contour sleeve openings so as to impart a swirl to the exhaust gas being discharged via the contour sleeve openings when the slide member is in an open position.

    摘要翻译: 在排气涡轮增压器的废气涡轮机中,该排气涡轮增压器包括可旋转地支撑在壳体中的涡轮机叶轮,并且可以经由入口通道向其供给废气,并经由出口管道排出废气涡轮机 ,其中在从所述入口通道到所述涡轮机叶轮的过渡处,在所述涡轮机入口处设置有与所述涡轮机入口相互作用的导向叶片结构和轴向滑动件,所述导向叶片结构相对于所述壳体和所述轴向滑块 布置在涡轮出口侧并且可移动地支撑在出口管道轮廓套筒上并且设置有用于容纳引导叶片结构的轴向开口,并且轮廓套筒包括将排气从入口通道直接引导到出口管道的开口, 它们被布置成使得当轴向滑动件从其打开位置移出时它们被轴向滑动件覆盖,导向叶片结构在轴线上延伸超过轮廓 ur套筒开口,以便当滑动构件处于打开位置时,经由轮廓套筒开口排出的废气产生漩涡。

    Exhaust-gas turbine in an exhaust-gas turbocharger
    2.
    发明授权
    Exhaust-gas turbine in an exhaust-gas turbocharger 失效
    排气涡轮增压器中的废气涡轮机

    公开(公告)号:US08186943B2

    公开(公告)日:2012-05-29

    申请号:US12001078

    申请日:2007-12-08

    IPC分类号: F01B25/02

    CPC分类号: F02C6/12 F01D17/143 F02C9/18

    摘要: In an exhaust-gas turbine of an exhaust-gas turbo-charger including a turbine wheel which is rotatably supported in a housing and to which exhaust gas can be supplied via an inlet channel and discharged out of the exhaust-gas turbine via an outlet duct, wherein a guide vane structure and an axial slide which interacts with the latter, are disposed in the turbine inlet at the transition from the inlet channel to the turbine wheel, the guide vane structure is fixedly mounted with respect to the housing and the axial slide is arranged at the turbine outlet side and is movably supported on an outlet duct contour sleeve and provided with an axial opening for accommodating the guide vane structure, and the contour sleeve includes openings which conduct exhaust gas from the inlet channel directly to the outlet duct and which are arranged so that they are covered by the axial slide when the axial slide is moved out of its open position, the guide vane structure extending axially over the contour sleeve openings so as to impart a swirl to the exhaust gas being discharged via the contour sleeve openings when the slide member is in an open position.

    摘要翻译: 在排气涡轮增压器的废气涡轮机中,该排气涡轮增压器包括可旋转地支撑在壳体中的涡轮机叶轮,并且可以经由入口通道向其供给废气,并经由出口管道排出废气涡轮机 ,其中在从所述入口通道到所述涡轮机叶轮的过渡处,在所述涡轮机入口处设置有与所述涡轮机入口相互作用的导向叶片结构和轴向滑动件,所述导向叶片结构相对于所述壳体和所述轴向滑块 布置在涡轮出口侧并且可移动地支撑在出口管道轮廓套筒上并且设置有用于容纳引导叶片结构的轴向开口,并且轮廓套筒包括将排气从入口通道直接引导到出口管道的开口, 它们被布置成使得当轴向滑动件从其打开位置移出时它们被轴向滑动件覆盖,导向叶片结构在轴线上延伸超过轮廓 ur套筒开口,以便当滑动构件处于打开位置时,经由轮廓套筒开口排出的废气产生漩涡。

    Compressor and turbine wheel for a secondary air feed device
    4.
    发明授权
    Compressor and turbine wheel for a secondary air feed device 有权
    用于二次空气供给装置的压缩机和涡轮机叶轮

    公开(公告)号:US07438529B2

    公开(公告)日:2008-10-21

    申请号:US11399686

    申请日:2006-04-06

    摘要: In a compressor and turbine wheel for a secondary air feed device formed as a single component, a rotor which includes a center disc structure consisting of at least two discs of different materials is provided at one side with compressor blades and on the opposite side with turbine blades, and the discs consist of an alloy based on Al, Mg, Ti, Fe, or Ni and are preferably arranged in axially spaced relationship with a disc carrier of a plastic material disposed in the space between the two bladed discs.

    摘要翻译: 在形成为单个部件的二次空气供给装置的压缩机和涡轮机叶轮中,包括由至少两个不同材料的盘构成的中心盘结构的转子在一侧设置有压缩机叶片,并且在与涡轮相反的一侧 叶片,并且盘由基于Al,Mg,Ti,Fe或Ni的合金组成,并且优选地与设置在两个叶片盘之间的空间中的塑料材料的盘式载体轴向间隔开地布置。

    Compressor and turbine wheel for a secondary air feed device
    5.
    发明申请
    Compressor and turbine wheel for a secondary air feed device 有权
    用于二次空气供给装置的压缩机和涡轮机叶轮

    公开(公告)号:US20060222503A1

    公开(公告)日:2006-10-05

    申请号:US11399686

    申请日:2006-04-06

    IPC分类号: F01D5/14

    摘要: In a compressor and turbine wheel for a secondary air feed device formed as a single component, a rotor which includes a center disc structure consisting of at least two discs of different materials is provided at one side with compressor blades and on the opposite side with turbine blades, and the discs consist of an alloy based on Al, Mg, Ti, Fe, or Ni and are preferably arranged in axially spaced relationship with a disc carrier of a plastic material disposed in the space between the two bladed discs.

    摘要翻译: 在形成为单个部件的二次空气供给装置的压缩机和涡轮机叶轮中,包括由至少两个不同材料的盘构成的中心盘结构的转子在一侧设置有压缩机叶片,并且在与涡轮相反的一侧 叶片,并且盘由基于Al,Mg,Ti,Fe或Ni的合金组成,并且优选地与设置在两个叶片盘之间的空间中的塑料材料的盘式载体轴向间隔开地布置。

    Reciprocating-piston internal combustion engine with variable compression ratio
    6.
    发明申请
    Reciprocating-piston internal combustion engine with variable compression ratio 审中-公开
    具有可变压缩比的往复活塞内燃机

    公开(公告)号:US20090000598A1

    公开(公告)日:2009-01-01

    申请号:US12152867

    申请日:2008-05-16

    IPC分类号: F02B75/04

    摘要: In a reciprocating-piston internal combustion engine with a piston movably arranged in a cylinder and coupled via a connecting rod to a transverse lever having a center of gravity, the transverse lever which is supported by a crankshaft and connected to an auxiliary connecting rod by an eccentric for adjusting the compression ratio of the internal combustion engine, the transverse lever has a weight and configuration providing for the center of gravity located so that an excellent operating smoothness of the engine is obtained with simple means.

    摘要翻译: 在具有活塞可移动地布置在气缸中并且通过连杆耦合到具有重心的横向杠杆的往复活塞内燃机中,横杆由曲轴支撑并通过一个辅助连杆连接到辅助连杆上 用于调节内燃机的压缩比的偏心件,横杆具有提供重心的重量和构造,使得以简单的方式获得发动机的优异的操作平滑度。

    Turboengine and Method for Adjusting the Stator and Rotor of a Turboengine
    8.
    发明申请
    Turboengine and Method for Adjusting the Stator and Rotor of a Turboengine 有权
    涡轮发动机和调整涡轮发动机定子和转子的方法

    公开(公告)号:US20070212216A1

    公开(公告)日:2007-09-13

    申请号:US10575750

    申请日:2004-09-15

    IPC分类号: F04D29/44

    摘要: A turbo-machine (1), including a stator (2), internally coated with a running-in layer (6), a rotor (4) within the stator (2), wherein the turbo-machine (1) supplementally includes a device for parallel displacement and rotation of the rotation axis of the rotor (10) about the axis of symmetry of the stator (2). By means of this device the gap width between stator (2) and rotor (4) is minimized and therewith the economy of the turbo-machine (1) is increased.

    摘要翻译: 一种涡轮机(1),其包括定子(2),其内部涂覆有流入层(6),所述定子(2)内的转子(4),其中所述涡轮机(1)补充地包括 用于使转子(10)的旋转轴线围绕定子(2)的对称轴平行移动和旋转的装置。 通过该装置,定子(2)和转子(4)之间的间隙宽度被最小化,并且涡轮机(1)的经济性增加。

    Arrangement for reducing exhaust gas emissions
    9.
    发明申请
    Arrangement for reducing exhaust gas emissions 失效
    减排废气排放的安排

    公开(公告)号:US20050150210A1

    公开(公告)日:2005-07-14

    申请号:US11035764

    申请日:2005-01-14

    IPC分类号: F01N3/32 F02D9/02 F01N5/04

    摘要: In an arrangement for reducing exhaust emissions and utilizing the throttling energy of an internal combustion engine, a compressor and a generator are operatively connected to a turbine by which the intake air flow is controlled while transferring the throttling energy recuperated by the turbine to the compressor and the generator and, in the engine start-up phase, the compressor supplies fresh air to an engine air intake duct, the intake air flow volume being controlled by the energy withdrawn from the turbine via the compressor and the generator thus eliminating the need for a throttle valve in the fresh air intake line.

    摘要翻译: 在用于减少废气排放并利用内燃机的节流能量的装置中,压缩机和发电机可操作地连接到涡轮机,通过该涡轮机控制进气流,同时将由涡轮机回收的节流能量传递到压缩机, 发电机,并且在发动机起动阶段,压缩机将新鲜空气供应到发动机进气管道,进气流量由通过压缩机和发电机从涡轮机排出的能量控制,因此不需要一个 节气门在新鲜空气进气管路中。