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    INTERNALLY COOLED AIRFOIL FOR A ROTARY MACHINE
    1.
    发明申请
    INTERNALLY COOLED AIRFOIL FOR A ROTARY MACHINE 有权
    用于旋转机的内部冷却空气

    公开(公告)号：US20150159490A1

    公开(公告)日：2015-06-11

    申请号：US14625734

    申请日：2015-02-19

    Applicant: ALSTOM Technology Ltd

    Inventor： Joerg KRUECKELS ,  Brian Kenneth Wardle ,  Herbert Brandl ,  Marc Widmer

    IPC: F01D5/18 ,  F01D9/02

    CPC classification number: F01D5/189 ,  B22C9/24 ,  F01D5/186 ,  F01D9/02 ,  F05D2260/201 ,  F05D2260/202

    Abstract: The invention refers to an internally cooled casted airfoil for a rotary machine, preferably a gas turbine engine comprising a suction and a pressure side wall each extending in an axial direction, i.e. from a leading to a trailing edge region of said airfoil. At least one suction wall sided cooling channel extends in axial direction confined by the suction side wall and a first inner wall. At least one pressure wall sided cooling channel extends in axial direction confined by the pressure side wall and a second inner wall. At least one feed chamber is defined between the first and second inner wall for feeding said at least one suction and pressure sided cooling channel each by at least one through hole inside of the first and second inner wall. At least one suction wall sided cooling channel and the at least one pressure wall sided cooling channel extend into the trailing edge region separately. At least one suction wall sided cooling channel and at least one pressure wall sided cooling channel join before discharging at the trailing edge.

    Abstract translation: 本发明涉及一种用于旋转机器的内部冷却铸造翼型件，优选地是包括抽吸和压力侧壁的燃气涡轮发动机，其各自在轴向方向上延伸，即从所述翼型的导向到后缘区域延伸。 至少一个抽吸壁侧冷却通道在被吸入侧壁和第一内壁限制的轴向方向上延伸。 至少一个压力壁侧冷却通道在受压侧壁和第二内壁限制的轴向方向上延伸。 至少一个进料室限定在第一和第二内壁之间，用于将第一和第二内壁内的至少一个通孔各自供给至少一个吸入和压力侧冷却通道。 至少一个抽吸壁侧冷却通道和至少一个压力壁侧冷却通道分别延伸到后缘区域。 至少一个抽吸壁侧冷却通道和至少一个压力壁侧冷却通道在后缘排放之前连接。

    ROTOR BLADE AND GUIDE VANE AIRFOIL FOR A GAS TURBINE ENGINE
    3.
    发明申请
    ROTOR BLADE AND GUIDE VANE AIRFOIL FOR A GAS TURBINE ENGINE 有权
    用于气体涡轮发动机的转子叶片和导向空气涡轮机

    公开(公告)号：US20150176412A1

    公开(公告)日：2015-06-25

    申请号：US14574897

    申请日：2014-12-18

    Applicant: ALSTOM Technology Ltd

    Inventor： Joerg KRUECKELS ,  Marc WIDMER

    IPC: F01D5/18 ,  F01D9/02

    CPC classification number: F01D5/187 ,  F01D9/02 ,  F05D2250/292 ,  F05D2260/2212 ,  F05D2260/22141

    Abstract: The invention refers to a rotor blade or guide vane airfoil for a gas turbine engine having a longitudinal axis and a source of cooling fluid. The airfoil has a pressure wall, a suction wall, a leading edge, a trailing edge and at least one cooling fluid flow passage. The cooling fluid flow passage is in fluid communication with the source of cooling fluid. Means for directing cooling fluid at least to the trailing edge are provided, whereas the cooling fluid flow passage including: a plurality of axially extending walls, each of the walls extending laterally between the pressure wall and suction wall. The plurality of walls are radially spaced within the cooling fluid flow passage such that adjacent pairs of walls define a channel. The axial spacing between the adjacent walls include in radial direction of the airfoil a pins and a ribs structure, wherein the pins holistic or approximately cover the axial height of the channel. The ribs have a deeper level with respect to the pins and the ribs establish a bridge-like connection between each of adjacent ribs.

    Abstract translation: 本发明涉及一种用于燃气涡轮发动机的转子叶片或导叶翼型件，其具有纵向轴线和冷却流体源。 翼型件具有压力壁，吸力壁，前缘，后缘和至少一个冷却流体流动通道。 冷却流体流动通道与冷却流体源流体连通。 提供了用于将冷却流体引导至后缘的装置，而冷却流体流动通道包括：多个轴向延伸的壁，每个壁在压力壁和抽吸壁之间横向延伸。 多个壁在冷却流体流动通道内径向间隔开，使得相邻的壁对形成通道。 相邻壁之间的轴向间隔在翼型件的径向方向上包括销和肋结构，其中销整体地或近似地覆盖通道的轴向高度。 这些肋相对于销具有更深的水平，并且肋在每个相邻的肋之间建立桥状连接。

    FLUID SEAL ARRANGEMENT AND METHOD FOR CONSTRICTING A LEAKAGE FLOW THROUGH A LEAKAGE GAP
    4.
    发明申请
    FLUID SEAL ARRANGEMENT AND METHOD FOR CONSTRICTING A LEAKAGE FLOW THROUGH A LEAKAGE GAP 审中-公开
    流体密封装置和通过泄漏漏气约束泄漏流量的方法

    公开(公告)号：US20150050125A1

    公开(公告)日：2015-02-19

    申请号：US14341264

    申请日：2014-07-25

    Applicant: ALSTOM Technology Ltd

    Inventor： Carlos SIMON-DELGADO ,  Vasileios STEFANIS ,  Sergey SHCHUKIN ,  Joerg KRUECKELS

    IPC: F01D11/10 ,  F16J15/40

    CPC classification number: F01D11/10 ,  F16J15/162 ,  F16J15/40 ,  F16J15/444 ,  F16J15/4472

    Abstract: The invention refers to a fluid seal arrangement for constricting a leakage flow directed through a leakage gap bordered by a rotational and a stationary component including at least one nozzle opening in the rotating and/or stationary component facing towards the rotating or stationary component of an opposite side of the leakage gap respectively in order for injecting a liquid or gaseous fluid flow through the nozzle opening into the leakage gap. The at least one nozzle opening is fluidly connected to a cooling channel inside said rotating and/or stationary component, so that said fluid flow emanating at the nozzle opening consists of a cooling fluid of the rotating and/or stationary component exclusively.

    Abstract translation: 本发明涉及一种流体密封装置，用于限制通过由旋转和静止部件界定的泄漏间隙的泄漏流动，所述泄漏间隙包括旋转和/或固定部件中的至少一个喷嘴开口，所述喷嘴开口面向相对的旋转部件或固定部件 以便将液体或气体流体流经喷嘴开口注入到泄漏间隙中。 至少一个喷嘴开口流体地连接到所述旋转和/或固定部件内的冷却通道，使得在喷嘴开口处发出的所述流体流由仅旋转和/或静止部件的冷却流体组成。

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