Compressor, particularly in an exhaust gas turbocharger for an internal combustion engine
    1.
    发明申请
    Compressor, particularly in an exhaust gas turbocharger for an internal combustion engine 失效
    压缩机,特别是用于内燃机的排气涡轮增压器

    公开(公告)号:US20050207885A1

    公开(公告)日:2005-09-22

    申请号:US11064417

    申请日:2005-02-23

    摘要: In a compressor particularly of an exhaust gas turbocharger of an internal combustion engine having a compressor wheel rotatably supported in a compressor housing which includes a diffuser structure with an adjustable diffuser geometry comprising guide vanes pivotally supported, an adjustment ring is provided with engagement elements which engage forked end structures of the guide vanes at the outer ends of the guide vanes opposite the pivotal guide vane support so that the pivot position of the guide vanes can be adjusted by rotation of the adjustment ring.

    摘要翻译: 在特别是具有可旋转地支撑在压缩机壳体中的压缩机叶轮的内燃机的排气涡轮增压器的压缩机中,压缩机叶轮包括具有可调节的扩散器几何形状的扩散器结构,该导向器几何形状包括枢转地支撑的引导叶片,调节环设有接合元件, 在导向叶片的外端与转动导向叶片支撑件相对的导叶的叉形端部结构,使得可以通过调节环的旋转来调整导叶的枢转位置。

    Compressor, particularly in an exhaust gas turbocharger for an internal combustion engine
    3.
    发明授权
    Compressor, particularly in an exhaust gas turbocharger for an internal combustion engine 失效
    压缩机,特别是用于内燃机的排气涡轮增压器

    公开(公告)号:US07186077B2

    公开(公告)日:2007-03-06

    申请号:US11064417

    申请日:2005-02-23

    IPC分类号: F01D17/16

    摘要: In a compressor particularly of an exhaust gas turbocharger of an internal combustion engine having a compressor wheel rotatably supported in a compressor housing which includes a diffuser structure with an adjustable diffuser geometry comprising guide vanes pivotally supported, an adjustment ring is provided with engagement elements which engage forked end structures of the guide vanes at the outer ends of the guide vanes opposite the pivotal guide vane support so that the pivot position of the guide vanes can be adjusted by rotation of the adjustment ring.

    摘要翻译: 在特别是具有可旋转地支撑在压缩机壳体中的压缩机叶轮的内燃机的排气涡轮增压器的压缩机中,压缩机叶轮包括具有可调节的扩散器几何形状的扩散器结构,该导向器几何形状包括枢转地支撑的引导叶片,调节环设有接合元件, 在导向叶片的外端与转动导向叶片支撑件相对的导叶的叉形端部结构,使得可以通过调节环的旋转来调整导叶的枢转位置。

    Radial compressor with wall slits
    4.
    发明授权
    Radial compressor with wall slits 失效
    径向压缩机带壁缝

    公开(公告)号:US06394751B1

    公开(公告)日:2002-05-28

    申请号:US09563822

    申请日:2000-05-03

    IPC分类号: F04D2954

    摘要: The invention relates to a radial compressor for producing a compressed gas flow, having a casing, an impeller which is arranged therein has a hub which carries blades. A ring is arranged in the flow duct concentrically with the hub, and is accommodated in a recess in the inner surface of the casing. The ring has wall slits on its inner surface. An annular gap is provided between that end face of the ring which is directed downstream and an end face of the recess which corresponds thereto and is directed upstream.

    摘要翻译: 本发明涉及一种用于生产压缩气流的径向压缩机,其具有壳体,其中布置有叶轮,其具有承载叶片的轮毂。 流体管道中的环与轮毂同心地布置,并且容纳在壳体的内表面的凹部中。 环在其内表面上具有壁狭缝。 环形间隙设置在环向下游的端面和与之对应的凹槽的端面之间并且被定向到上游。

    Hydrodynamic propulsion device
    5.
    发明授权
    Hydrodynamic propulsion device 失效
    流体动力推进装置

    公开(公告)号:US5421153A

    公开(公告)日:1995-06-06

    申请号:US134092

    申请日:1993-10-08

    IPC分类号: B63H11/16 B63H11/00

    CPC分类号: B63H11/16

    摘要: A hydrodynamic propulsion device possessing an expansion chamber located downstream of a cross-sectional widening for the inflow of a medium which is to be expelled through a discharge nozzle. The propulsion device is constructed as a static propulsion mechanism without movable components, in that the gaseous operating medium is produced in the propulsion device through the reaction of a hydrofuel, such as NaK with water.

    摘要翻译: 一种流体动力推进装置,其具有位于横截面加宽下游的膨胀室,用于通过排放喷嘴排出的介质的流入。 推进装置被构造为没有可移动部件的静态推进机构,因为气态操作介质通过诸如NaK与水的氢氧化钠的反应在推进装置中产生。