COMPRESSOR WHEEL AND SHAFT ASSEMBLY FOR TURBOCHARGER
    1.
    发明申请
    COMPRESSOR WHEEL AND SHAFT ASSEMBLY FOR TURBOCHARGER 审中-公开
    涡轮增压器的压缩机轮和轴组件

    公开(公告)号:WO1993002278A1

    公开(公告)日:1993-02-04

    申请号:PCT/US1992004803

    申请日:1992-06-09

    CPC classification number: F01D5/025 F04D29/266

    Abstract: A turbocharger (10) includes a compressor wheel (32) and shaft assembly in which a threaded connection is provided between the shaft (18) and the compressor wheel (32). A pair of pilot surfaces (76, 78) on the shaft (18) and on the compressor wheel are located on either end of the threaded sections (64, 66) of the shaft and compressor wheel, and are displaced radially from the threads (64, 66). Accordingly, the piloting functions which assure concentricity between the shaft (18) and compressor wheel (32) are kept entirely separate from the attachment function provided by the threads (64, 66), thereby permitting the concentricity between the compressor wheel (32) and shaft (18) to be held to tighter tolerances than would be possible if the threads (64, 66) also performed a piloting function.

    HIGH TEMPERATURE TURBINE ENGINE STRUCTURE
    2.
    发明申请
    HIGH TEMPERATURE TURBINE ENGINE STRUCTURE 审中-公开
    高温涡轮发动机结构

    公开(公告)号:WO1990006420A1

    公开(公告)日:1990-06-14

    申请号:PCT/US1989004228

    申请日:1989-09-27

    CPC classification number: F01D5/025 F01D5/284

    Abstract: A high temperature turbine engine (10) includes a hybrid ceramic/metallic rotor member having (20) ceramic/metal joint structure (62). The disclosed joint (62) is able to endure higher temperatures than previously possible, and aids in controlling heat transfer in the rotor member (20).

    Abstract translation: 高温涡轮发动机包括具有陶瓷/金属接头结构的混合陶瓷/金属转子构件。 所公开的接头能够承受比先前可能的更高的温度,并且有助于控制转子构件中的热传递。

    TURBINE SHAFT CONSISTING OF TWO ALLOYS
    3.
    发明申请
    TURBINE SHAFT CONSISTING OF TWO ALLOYS 审中-公开
    涡轮轴两种合金

    公开(公告)号:WO1997032112A1

    公开(公告)日:1997-09-04

    申请号:PCT/DE1997000307

    申请日:1997-02-19

    CPC classification number: C22C38/40 B32B15/011 F01D5/02 F01D5/28 Y10T428/12965

    Abstract: The invention relates to a turbine shaft (1) intended in particular for a steam turbine aligned along an axis (2) of rotation. The turbine shaft (1) has a first region (4) of maximum radius R1 and a second region (5) bordering on the first and of maximum radius R2 > R1. The first region (4) has a first base material for use at temperatures of over 550 DEG C and the second region (5) has a second base material for use at temperatures of below 550 DEG C. The steel alloy used for the first and second base material has a chromium content of between 8.0 and 12.5 wt.% respectively, the austenitization temperature being substantially the same in each case.

    Abstract translation: 本发明涉及一种涡轮机轴(1),特别是用于一蒸汽涡轮机,其沿旋转轴(2)定向。 涡轮机轴(1)具有第一区域(4)具有最大半径R1和与最大半径R2> R1与其相邻的(5)的第二区域。 所述第一区域(4)具有用于在低于550℃的温度上使用的第一基体材料使用的第二基体材料在约550℃的温度和所述第二区域(5)。 用于第一和第二基材每个钢合金具有铬的比例为8.0重量和12.5之间.-%重量%在基本相同奥氏体化温度。

    TURBOCHARGER COMPRESSOR WHEEL ASSEMBLY WITH BORELESS HUB COMPRESSOR WHEEL
    4.
    发明申请
    TURBOCHARGER COMPRESSOR WHEEL ASSEMBLY WITH BORELESS HUB COMPRESSOR WHEEL 审中-公开
    涡轮增压器压缩机轮组件与无轨道压缩机轮

    公开(公告)号:WO1991006749A1

    公开(公告)日:1991-05-16

    申请号:PCT/US1990002524

    申请日:1990-05-07

    Abstract: An improved compressor wheel assembly for a turbocharger or the like includes a centrifugal compressor wheel having a boreless hub to substantially improve wheel fatigue life. The compressor wheel is formed as by casting to include an integral and internally threaded mounting sleeve extending coaxially from the boreless hub. In the assembly, the mounting sleeve extends through an opening in a compressor backplate for threaded connection to a turbocharger shaft, with a thrust collar spacer being interposed between axially facing shoulders defined respectively on the mounting sleeve and shaft to ensure accurate axial positioning of the components. An annular seal flange on the thrust collar spacer extends axially into the backplate opening in generally concentric spaced relation about the mounting sleeve. This seal flange is adapted to carry one or more seal rings for engaging the backplate, thereby sealing the passage of the mounting sleeve and shaft through the backplate opening.

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