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    • 33. 发明授权
    • Turbocharger comprising adjustable guide blades, blade lever and adjusting ring therefor
    • 涡轮增压器包括可调节导向叶片,叶片杆及其调节环
    • US08186944B2
    • 2012-05-29
    • US12279709
    • 2007-02-14
    • Timo TriesRalf Boening
    • Timo TriesRalf Boening
    • F01D17/12
    • F02C6/12F01D17/165F05D2220/40
    • A turbocharger (1) with a variable turbine geometry (VTG), includes a guide baffle (18), which has a blade bearing ring (6) with a plurality of guide blades (7), each of the latter having a blade shaft (8) that is mounted on the blade bearing ring (6). The guide baffle also has an adjusting ring (5), which interacts with the guide blades (7) by means of associated blade levers (20), which are fixed to the blade shafts (8) by one of their ends (21). The other end (22) of each blade lever (20) is provided with a lever head (23), which can be engaged in an associated engagement recess (24) of the adjusting ring (5). Each blade lever (20) is asymmetrical and has a bearing lug (25) in the form of an arched segment on only one side of the central section (26).
    • 具有可变涡轮机几何形状(VTG)的涡轮增压器(1)包括引导挡板(18),该引导挡板(18)具有带有多个引导叶片(7)的叶片轴承环(6),后者具有叶片轴 8)安装在叶片轴承环(6)上。 引导挡板还具有调节环(5),其通过相关联的叶片杆(20)与导向叶片(7)相互作用,叶片杆(20)通过其一端(21)固定到叶片轴(8)。 每个叶片杆(20)的另一端(22)设置有杠杆头(23),该杆头可接合在调节环(5)的相关接合凹槽(24)中。 每个叶片杆(20)是不对称的,并且仅在中心部分(26)的一侧上具有呈弓形部分形式的轴承凸耳(25)。
    • 34. 发明授权
    • Turbocharger with separately formed vane lever stops
    • 涡轮增压器具有单独形成的叶片控制杆
    • US08328520B2
    • 2012-12-11
    • US12300260
    • 2007-05-16
    • Ralf BoeningDietmar Metz
    • Ralf BoeningDietmar Metz
    • F01D17/12
    • F01D17/165F05D2220/40F05D2230/54F05D2230/61F05D2230/644F05D2260/30
    • The invention relates to a turbocharger (1) having variable turbine geometry (VTG) having a turbine housing (2) with a supply duct (9) for exhaust gases; having a turbine rotor (4) which is rotatably mounted in the turbine housing (2); and having a guide grate (18) which surrounds the turbine rotor (4) radially at the outside, which guide grate (18) has a blade mounting ring (6) which has a plurality of guide blades (7) which in each case have a blade shaft (8) mounted in the blade mounting ring (6), which guide grate (18) has an adjusting ring (5) which is operatively connected to the guide blades (7) by means of associated blade levers (20) which are fastened to the blade shafts (8) at one of their ends, wherein each blade lever (20) has, at the other end, a lever head (23) which can be placed in engagement with an associated engagement recess (24) of the adjusting ring (5), and which guide grate (18) has a stop (25) at least for setting the minimum throughflow through the nozzle cross sections which are formed by the guide blades (7), wherein the stop (25) is embodied as a separate component which can be fixed in the guide grate (18).
    • 本发明涉及具有可变涡轮机几何形状(VTG)的涡轮增压器(1),其具有涡轮机壳体(2),其具有用于排气的供应管道(9) 具有可旋转地安装在所述涡轮机壳体(2)中的涡轮机转子(4); 并且具有在外部径向包围涡轮机转子(4)的引导炉篦(18),所述导向炉篦(18)具有刀片安装环(6),所述刀片安装环具有多个导向叶片(7),每个导向叶片 安装在所述叶片安装环(6)中的叶片轴(8),所述导向栅格(18)具有调节环(5),所述调节环通过相关联的叶片杆(20)可操作地连接到所述引导叶片(7) 在其一端处固定到所述刀片轴(8),其中每个刀片杆(20)在另一端具有杠杆头(23),所述杠杆头(23)可以被放置成与相关联的接合凹部(24)接合 所述调节环(5)和所述导向炉篦(18)至少具有通过由所述导向叶片(7)形成的所述喷嘴横截面设定所述最小通流的止挡件(25),其中所述止动件 体现为可以固定在引导格栅(18)中的单独部件。
    • 39. 发明授权
    • Guiding grid of variable geometry and turbocharger
    • 可变几何和涡轮增压器的导向网格
    • US06916153B2
    • 2005-07-12
    • US10659786
    • 2003-09-10
    • Ralf Boening
    • Ralf Boening
    • F02B37/24F01D17/16F01D25/24
    • F01D17/165F05D2220/40
    • A guiding grid of variable geometry comprises a plurality of guiding vanes in a housing in angular distances around a central axis in an axially extending vane space of a predetermined axial distance. Each vane is pivotal about an associated pivoting axis to assume different angles in relation to the central axis and, thus, to form a nozzle of variable cross-section between each pair of adjacent vanes. A nozzle ring supports the vanes around the central axis and forms a first axial limitation of the vane space. A unison ring is displaceable relative to the nozzle ring and is connected to the vanes to pivot them. An annular disk is fixed to the housing and faces the nozzle ring in an axial distance to form a second axial limitation of the vane space and a central opening. Into this opening, a sleeve may be inserted. A fixing arrangement determines the axial position of the annular disk with respect to the housing.
    • 可变几何形状的引导格栅包括围绕轴线延伸的叶片空间中心轴线以预定轴向距离的角距离的壳体中的多个引导叶片。 每个叶片围绕关联的枢转轴线枢转以相对于中心轴线呈现不同的角度,并且因此在每对相邻叶片之间形成可变横截面的喷嘴。 喷嘴环围绕中心轴线支撑叶片并形成翼片空间的第一轴向限制。 协调环可相对于喷嘴环移动并且连接到叶片以枢转它们。 环形盘被固定到壳体并且以轴向方向面对喷嘴环,以形成叶片空间和中心开口的第二轴向限制。 在该开口中,可以插入套筒。 固定装置确定环形盘相对于壳体的轴向位置。
    • 40. 发明申请
    • TURBOCHARGER COMPRISING ADJUSTABLE GUIDE BLADES, BLADE LEVER AND ADJUSTING RING THEREFOR
    • 涡轮增压器包括可调节导向叶片,叶片和调节环
    • US20090022581A1
    • 2009-01-22
    • US12279709
    • 2007-02-14
    • Timo TriesRalf Boening
    • Timo TriesRalf Boening
    • F04D29/56
    • F02C6/12F01D17/165F05D2220/40
    • The invention relates to a turbocharger (1) with a variable turbine geometry (VTG), comprising a turbine housing (2) that has a supply channel (9) for exhaust gases, a turbine rotor (4), which is rotatably mounted in the turbine housing (2) and a guide baffle (18), which radially surrounds the exterior of the turbine rotor (4) and has a blade bearing ring (6) with a plurality of guide blades (7), each of the latter having a blade shaft (8) that is mounted on the blade bearing ring (6). The guide baffle also has an adjusting ring (5), which interacts with the guide blades (7) by means of associated blade levers (20), which are fixed to the blade shafts (8) by one of their ends (21). The other end (22) of each blade lever (20) is provided with a lever head (23), which can be engaged in an associated engagement recess (24) of the adjusting ring (5). Each blade lever (20) is asymmetrical and has a bearing lug (25) in the form of an arched segment on only one side of the central section (26), said lug being located on the same plane as the lever head (23).
    • 本发明涉及具有可变涡轮机几何形状(VTG)的涡轮增压器(1),其包括具有用于排气的供应通道(9)的涡轮机壳体(2),涡轮转子(4),其可旋转地安装在 涡轮机壳体(2)和引导挡板(18),所述引导挡板(18)径向地围绕所述涡轮机转子(4)的外部并且具有带有多个引导叶片(7)的叶片轴承环(6),每个所述导向叶片具有 叶片轴(8),其安装在叶片轴承环(6)上。 引导挡板还具有调节环(5),其通过相关联的叶片杆(20)与导向叶片(7)相互作用,叶片杆(20)通过其一端(21)固定到叶片轴(8)。 每个叶片杆(20)的另一端(22)设置有杠杆头(23),该杆头可接合在调节环(5)的相关接合凹槽(24)中。 每个叶片杆(20)是不对称的,并且在中心部分(26)的一侧仅具有弓形段形式的轴承凸耳(25),所述凸耳位于与杆头(23)相同的平面上, 。