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    • 1. 发明申请
    • EXHAUST GAS TURBOCHARGER
    • 排风机涡轮增压器
    • US20140322005A1
    • 2014-10-30
    • US14324196
    • 2014-07-06
    • IHI CHARGING SYSTEMS INTERNATIONAL GMBH
    • Thomas IHLIRoberto DE SANTIS
    • F02B47/08
    • F02B47/08F01D9/045F01D11/005F01D17/165F02C6/12F05D2220/40
    • In an exhaust gas turbocharger with a casing part in which a guide apparatus comprising two axially spaced insert elements forming a flow duct is arranged with guide vanes supported on at least one of the insert elements via which exhaust gas flowing through the flow duct is guided into the turbine of the turbocharger and wherein a first of the insert elements comprises a first wall portion which extends at least essentially in the radial direction and an adjoining second wall portion which extends essentially in the axial direction so as to form a corner area of the first insert element, wherein in the first wall portion and/or in the corner area in a side facing the casing part at least one recess is provided.
    • 在具有壳体部分的排气涡轮增压器中,其中包括形成流动管道的两个轴向间隔开的插入元件的引导装置布置成具有支撑在至少一个插入元件上的导向叶片,通过该插入元件流过流道的废气被引导到 涡轮增压器的涡轮机,并且其中第一插入元件包括至少基本沿径向延伸的第一壁部分和邻近的第二壁部分,该第二壁部分基本沿轴向方向延伸,以形成第一 插入元件,其中在第一壁部分和/或在面向壳体部分的一侧的拐角区域中提供至少一个凹部。
    • 3. 发明申请
    • TURBINE FOR AN EXHAUST GAS TURBOCHARGER
    • 用于排气烟囱的涡轮机
    • US20140286759A1
    • 2014-09-25
    • US14292931
    • 2014-06-01
    • IHI CHARGING SYSTEMS INTERNATIONAL GMBH
    • Thomas IHLI
    • F01D17/00
    • F01D17/00F01D17/141F02C6/12
    • In a turbine for an exhaust gas turbocharger with a turbine casing comprising a housing space for the turbine wheel of a turbine with guide vanes arranged upstream of the turbine wheel in a radial direction of the turbine wheel so as to be stationary relative to the turbine casing for guiding exhaust gas to the turbine wheel, and with an actuating element by which an inlet flow cross-section of the turbine through which the exhaust gas flows is variably adjustable and which is movable in the axial direction of the turbine between a blocking position restricting the flow cross-section and an open position clearing the flow cross-section relative to the turbine casing, the actuating elements extend through conforming openings formed in the guide walls between the guide vanes into the spaces defined between the guide vanes for controlling the turbine inlet flow cross-section.
    • 在具有涡轮壳体的涡轮机涡轮机中,涡轮机壳体包括用于涡轮机的涡轮机的壳体空间,其具有沿涡轮机叶轮的径向布置在涡轮机叶轮的上游的引导叶片,以相对于涡轮机壳体固定 用于将废气引导到涡轮机叶轮,并且具有致动元件,通过该致动元件,排气流过的涡轮机的入口流动横截面可变地可调节,并且可在涡轮机的轴向方向上移动,阻塞位置限制 所述流动横截面和打开位置相对于所述涡轮机壳体清除所述流动横截面,所述致动元件延伸穿过形成在所述导向叶片之间的引导壁中的适形开口进入所述导向叶片之间限定的空间中,以控制所述涡轮机入口 流动截面。