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    • 2. 发明申请
    • TURBOCHARGER VANE
    • 涡轮增压器
    • US20100098529A1
    • 2010-04-22
    • US12525724
    • 2008-02-14
    • Steve RobyDavid M. DeckerDietmar Metz
    • Steve RobyDavid M. DeckerDietmar Metz
    • F04D29/56
    • F01D17/165F01D5/143F02B37/24F05D2220/40F05D2230/21F05D2240/80
    • A vane (234) is provided which reduces leakage of gas in a variable geometry turbocharger (210) from the high pressure side of the vane (234) to the low pressure side of the vane (234). The vane (234) can have a channel (330, 430) along a gas bearing surface (325, 425) for reducing the leakage. The channel (330, 430) can be defined at least in part by sideplates (300, 350). The sideplates (300, 350) can be integrally cast with the rest of the vane (234). At least one of the sideplates (300, 350) can have a hole therein for a vane shaft (228) which allows movement of the vane (234) for gas flow control. The 340 sideplates (300, 350) can have edges (301, 351) that conform to the shape of the gas bearing surface (325, 425).
    • 提供了一种叶片(234),其减少了可变几何涡轮增压器(210)中的气体从叶片(234)的高压侧到叶片(234)的低压侧的泄漏。 叶片(234)可以沿着气体支承表面(325,425)具有用于减少泄漏的通道(330,430)。 通道(330,430)可以至少部分地由侧板(300,350)限定。 侧板(300,350)可以与叶片(234)的其余部分整体铸造。 侧板(300,350)中的至少一个可以在其中具有用于叶片轴(228)的孔,其允许叶片(234)的运动用于气体流量控制。 340个侧板(300,350)可以具有与气体支承表面(325,425)的形状一致的边缘(301,351)。
    • 5. 发明授权
    • Turbocharger vane
    • 涡轮增压器叶片
    • US08500395B2
    • 2013-08-06
    • US12525724
    • 2008-02-14
    • Steve RobyDavid M. DeckerDietmar Metz
    • Steve RobyDavid M. DeckerDietmar Metz
    • F01D9/04
    • F01D17/165F01D5/143F02B37/24F05D2220/40F05D2230/21F05D2240/80
    • A vane (234) is provided which reduces leakage of gas in a variable geometry turbocharger (210) from the high pressure side of the vane (234) to the low pressure side of the vane (234). The vane (234) can have a channel (330, 430) along a gas bearing surface (325, 425) for reducing the leakage. The channel (330, 430) can be defined at least in part by sideplates (300, 350). The sideplates (300, 350) can be integrally cast with the rest of the vane (234). At least one of the sideplates (300, 350) can have a hole therein for a vane shaft (228) which allows movement of the vane (234) for gas flow control. The sideplates (300, 350) can have edges (301, 351) that conform to the shape of the gas bearing surface (325, 425).
    • 提供了一种叶片(234),其减少了可变几何涡轮增压器(210)中的气体从叶片(234)的高压侧到叶片(234)的低压侧的泄漏。 叶片(234)可以沿着气体支承表面(325,425)具有用于减少泄漏的通道(330,430)。 通道(330,430)可以至少部分地由侧板(300,350)限定。 侧板(300,350)可以与叶片(234)的其余部分整体铸造。 侧板(300,350)中的至少一个可以在其中具有用于叶片轴(228)的孔,其允许叶片(234)的运动用于气体流量控制。 侧板(300,350)可以具有与气体支承表面(325,425)的形状一致的边缘(301,351)。
    • 8. 发明授权
    • Titanium aluminide wheel and steel shaft connection thereto
    • 钛酸铝轮与钢轴连接
    • US07287960B2
    • 2007-10-30
    • US10900645
    • 2004-07-28
    • David M. Decker
    • David M. Decker
    • F01D5/04
    • F01D5/025F04D29/266F05D2220/40F05D2230/237F05D2260/37F05D2300/174Y10T29/4932Y10T29/49332Y10T29/49334
    • Titanium aluminide (TiAl) rotor shaft assembly (10) of a type used in a turbocharger has a TiAl rotor (20) with an axially protruded portion (40) that is fixedly joined to a recessed portion (50) of a metal shaft (30) by the synergistic combination of an interference fit, such as a heat shrinkage fit, further supported by a brazed joint (60) in which a thin layer of a brazing material (110) is interposed between the surface of the protruded portion (120) and the recessed surface (130). Optionally, one or both of the jointed surfaces have braze channels (90) to facilitate braze flow within the joint. Methods for producing the rotor shaft assembly (10) and a turbocharger having the rotor shaft assembly (10) are provided.
    • 一种用于涡轮增压器的钛铝化合物(TiAl)转子轴组件(10)具有TiAl转子(20),其具有轴向突出部分(40),该轴向突出部分(40)固定地接合到金属轴(30)的凹部(50) )通过由钎焊接头(60)进一步支撑的过盈配合(例如热收缩配合)的协同组合,其中钎料(110)的薄层插入在突出部分(120)的表面之间, 和凹入表面(130)。 可选地,一个或两个接合表面具有钎焊通道(90)以便于在接头内的钎焊流动。 提供了用于生产转子轴组件(10)的方法和具有转子轴组件(10)的涡轮增压器。