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    • 6. 发明授权
    • Charging equipment
    • 充电设备
    • US08328503B2
    • 2012-12-11
    • US12604537
    • 2009-10-23
    • Timo TriesGunter WinklerMatthias Stein
    • Timo TriesGunter WinklerMatthias Stein
    • F01D17/16
    • F01D17/165F01D9/045F02B37/24F05D2220/40F05D2240/12F05D2250/30F05D2250/70Y02T10/144
    • Charging equipment is disclosed, comprising a variable turbine geometry, and a plurality of guide vanes rotatably mounted between at least one of a guide vane carrier, a cover disc and a turbine housing. The guide vane carrier is positioned on at least one of the cover disc and on the turbine housing by at least one spacer. The geometry has at least two different types of flow channels, a first flow channel wherein flow is influenced by the spacer, and a second flow channel wherein flow is not influenced by the spacer. The first flow channel guide vanes have a radial distance (R1) to a turbine wheel axis, and to a distance from an adjacent guide vane are configured and adjusted such that a gas flow from the first flow channel meeting the turbine wheel corresponds to a gas flow from the second flow channel meeting the turbine wheel.
    • 公开了一种充电设备,其包括可变的涡轮机几何形状,以及可转动地安装在导叶载体,盖盘和涡轮壳体中的至少一个之间的多个导向叶片。 导叶载体通过至少一个间隔件定位在至少一个盖盘上和涡轮壳体上。 该几何形状具有至少两种不同类型的流动通道,其中流动受间隔物影响的第一流动通道和其中流动不受间隔物影响的第二流动通道。 第一流道导流叶片具有与涡轮机叶轮轴线的径向距离(R1),并且与相邻导向叶片的距离被构造和调节,使得来自与涡轮机叶轮相遇的第一流动通道的气流对应于气体 从第二流动通道流入涡轮机叶轮。
    • 7. 发明申请
    • CHARGING EQUIPMENT
    • 充电设备
    • US20100104425A1
    • 2010-04-29
    • US12604537
    • 2009-10-23
    • Timo TriesGunter WinklerMatthias Stein
    • Timo TriesGunter WinklerMatthias Stein
    • F04D29/56
    • F01D17/165F01D9/045F02B37/24F05D2220/40F05D2240/12F05D2250/30F05D2250/70Y02T10/144
    • The invention relates to a piece of charging equipment having a variable turbine geometry (1), which has guide vanes (3, 4) that are rotatably mounted between a guide vane carrier (2) and a cover disc, wherein the cover disc is fixed/positioned on the guide vane carrier (2) by means of spacers (5) and wherein the variable turbine geometry (1) has at least two different types of flow channels (6, 7), namely a first flow channel (6) in which a flow behaviour is influenced by an associated spacer (5), and a second flow channel (7) in which a flow behaviour is not influenced by the spacers (5). Necessary for the definition of the invention is that the guide vanes (3) respectively arranged in the region of the first flow channel (6) with regard to their shape, their radial distance (R1) to a turbine wheel axis (8), and/or with regard to their distance from an adjacent guide vane (4) are configured and adjusted in such a manner that a gas flow, which is from the first flow channel (6), meeting the turbine wheel is at least matched to the gas flow, which is from the second flow channel (7), meeting the turbine wheel.
    • 本发明涉及一种具有可变涡轮机几何形状(1)的充电设备,其具有可旋转地安装在导向叶片承载件(2)和盖盘之间的导向叶片(3,4),其中盖盘固定 通过间隔件(5)定位在导叶载体(2)上,并且其中可变涡轮机几何形状(1)具有至少两种不同类型的流动通道(6,7),即第一流动通道(6) 流动特性受到相关联的间隔件(5)的影响,以及第二流动通道(7),其中流动行为不受间隔件(5)的影响。 对于本发明的定义所必需的是,分别布置在第一流动通道(6)的区域中的导向叶片(3)的形状,其与涡轮机叶轮轴线(8)的径向距离(R1)以及 或相对于与相邻的引导叶片(4)的距离被构造和调节,使得来自第一流动通道(6)的气流与涡轮机叶轮相匹配至少与气体匹配 来自第二流动通道(7)的流动与涡轮机叶轮相遇。