Methods and systems for forming cooling holes having circular inlets and non-circular outlets
    1.
    发明申请
    Methods and systems for forming cooling holes having circular inlets and non-circular outlets 有权
    用于形成具有圆形入口和非圆形出口的冷却孔的方法和系统

    公开(公告)号:US20080230379A1

    公开(公告)日:2008-09-25

    申请号:US11726418

    申请日:2007-03-22

    Abstract: A method for forming a hole in an object is provided. The method includes forming a starter hole in the object, providing an electrochemical machining electrode that includes insulation that extends only partially around the electrode, and inserting the electrode into the starter hole to form a hole in the object that has an inlet defined by a first cross-sectional area and an outlet defined by a second cross-sectional area.

    Abstract translation: 提供了一种在物体中形成孔的方法。 该方法包括在物体中形成起动器孔,提供电化学加工电极,其包括仅部分地围绕电极延伸的绝缘体,以及将电极插入起动器孔中以在物体中形成孔,该孔具有由第一 横截面积和由第二横截面积限定的出口。

    Methods and systems for forming tapered cooling holes
    2.
    发明授权
    Methods and systems for forming tapered cooling holes 失效
    用于形成锥形冷却孔的方法和系统

    公开(公告)号:US07938951B2

    公开(公告)日:2011-05-10

    申请号:US11726410

    申请日:2007-03-22

    CPC classification number: B23H9/00 B23H3/00 B23H3/04 B23H3/06 B23H9/10 B23H9/14

    Abstract: A method for forming holes in an object is provided. The method includes providing an electrochemical machining (ECM) electrode including a first section having insulation that circumscribes the first section, and a second section having insulation that extends only partially around the second section. The method also includes inserting the electrode into the object, such that in a single pass the electrode forms a hole that includes a first portion having a first cross-sectional area and a second portion having a second cross-sectional area.

    Abstract translation: 提供了一种在物体中形成孔的方法。 该方法包括提供电化学加工(ECM)电极,其包括具有围绕第一部分的绝缘体的第一部分和具有仅部分地围绕第二部分延伸的绝缘体的第二部分。 该方法还包括将电极插入到物体中,使得在单次通过中,电极形成包括具有第一横截面积的第一部分和具有第二横截面积的第二部分的孔。

    Methods and systems for forming turbulated cooling holes
    4.
    发明申请
    Methods and systems for forming turbulated cooling holes 审中-公开
    用于形成混浊冷却孔的方法和系统

    公开(公告)号:US20080230396A1

    公开(公告)日:2008-09-25

    申请号:US11726424

    申请日:2007-03-22

    Abstract: A method for forming holes in an object is provided. The method includes forming a starter hole in the object, providing an electrochemical machining electrode having at least one insulated section that substantially circumscribes the electrode and at least one uninsulated section, and inserting the electrode into the starter hole to facilitate forming a hole defined by at least one first section having a first cross-sectional area and at least one second section having a second cross-sectional area.

    Abstract translation: 提供了一种在物体中形成孔的方法。 该方法包括在物体中形成起动器孔,提供电化学加工电极,其具有至少一个绝缘部分,绝缘部分基本上限定电极和至少一个非绝缘部分,并将电极插入起动器孔中,以便于形成由 至少一个具有第一横截面积的第一部分和至少一个具有第二横截面积的第二部分。

    Methods and systems for forming tapered cooling holes
    5.
    发明申请
    Methods and systems for forming tapered cooling holes 失效
    用于形成锥形冷却孔的方法和系统

    公开(公告)号:US20080230378A1

    公开(公告)日:2008-09-25

    申请号:US11726410

    申请日:2007-03-22

    CPC classification number: B23H9/00 B23H3/00 B23H3/04 B23H3/06 B23H9/10 B23H9/14

    Abstract: A method for forming holes in an object is provided. The method includes providing an electrochemical machining (ECM) electrode including a first section having insulation that circumscribes the first section, and a second section having insulation that extends only partially around the second section. The method also includes inserting the electrode into the object, such that in a single pass the electrode forms a hole that includes a first portion having a first cross-sectional area and a second portion having a second cross-sectional area.

    Abstract translation: 提供了一种在物体中形成孔的方法。 该方法包括提供电化学加工(ECM)电极,其包括具有围绕第一部分的绝缘体的第一部分和具有仅部分地围绕第二部分延伸的绝缘体的第二部分。 该方法还包括将电极插入到物体中,使得在单次通过中,电极形成包括具有第一横截面积的第一部分和具有第二横截面积的第二部分的孔。

    METHODS FOR OPTIMIZING PARAMETERS OF GAS TURBINE ENGINE COMPONENTS
    6.
    发明申请
    METHODS FOR OPTIMIZING PARAMETERS OF GAS TURBINE ENGINE COMPONENTS 有权
    优化气体涡轮发动机部件参数的方法

    公开(公告)号:US20080281562A1

    公开(公告)日:2008-11-13

    申请号:US11747351

    申请日:2007-05-11

    CPC classification number: G01M9/065 B33Y80/00

    Abstract: Methods for optimizing at least one operating parameter of an engine component using an experimentally measured 3D flow field involving providing a magnetic resonance imaging machine, providing a model of an engine component, placing the model into the magnetic resonance imaging machine with a fluid flow source for applying an external fluid flow, applying the external fluid flow to the model, collecting data related to the external fluid flow about the model, and optimizing at least one operating parameter of the component using the data.

    Abstract translation: 使用实验测量的3D流场来优化发动机部件的至少一个操作参数的方法,包括提供磁共振成像机,提供发动机部件的模型,将所述模型放置在磁共振成像机中,所述流体流动源用于 施加外部流体流,将外部流体流施加到模型,收集与模型相关的外部流体流动的数据,以及使用该数据来优化组件的至少一个操作参数。

    Methods for optimizing parameters of gas turbine engine components
    7.
    发明授权
    Methods for optimizing parameters of gas turbine engine components 有权
    燃气轮机发动机部件参数优化方法

    公开(公告)号:US07774171B2

    公开(公告)日:2010-08-10

    申请号:US11747351

    申请日:2007-05-11

    CPC classification number: G01M9/065 B33Y80/00

    Abstract: Methods for optimizing at least one operating parameter of an engine component using an experimentally measured 3D flow field involving providing a magnetic resonance imaging machine, providing a model of an engine component, placing the model into the magnetic resonance imaging machine with a fluid flow source for applying an external fluid flow, applying the external fluid flow to the model, collecting data related to the external fluid flow about the model, and optimizing at least one operating parameter of the component using the data.

    Abstract translation: 使用实验测量的3D流场来优化发动机部件的至少一个操作参数的方法,包括提供磁共振成像机,提供发动机部件的模型,将所述模型放置在磁共振成像机中,所述流体流动源用于 施加外部流体流,将外部流体流施加到模型,收集与模型相关的外部流体流动的数据,以及使用该数据来优化组件的至少一个操作参数。

    Electrochemical machining process, electrode therefor and turbine bucket with turbulated cooling passage
    8.
    发明授权
    Electrochemical machining process, electrode therefor and turbine bucket with turbulated cooling passage 有权
    电化学加工工艺,其电极和涡轮机桶与紊流冷却通道

    公开(公告)号:US06416283B1

    公开(公告)日:2002-07-09

    申请号:US09688579

    申请日:2000-10-16

    CPC classification number: B23H1/04 B23H9/10 B23H9/14 F05B2260/222

    Abstract: An electrode having a dielectric coating is patterned to provide axially spaced rows of insulating material on the external surface of the electrode with one or more gaps in the insulating material of each row. The electrode is placed in a preformed hole of a turbine bucket and an electrolyte is provided for flow between the electrode and the walls of the hole. Upon application of an electrical current, portions of the material of the interior wall surface directly opposite the non-insulated portions of the electrode are dissolved, forming grooves. The insulated portions of the electrode leave axially spaced rows of projections extending toward the axis of the hole. The gaps in the rows or projections are axially misaligned. The projections form turbulators in the cooling flow passages of the bucket, enhancing the heat transfer coefficient.

    Abstract translation: 具有电介质涂层的电极被图案化以在电极的外表面上提供轴向隔开的一排绝缘材料,其中每行的绝缘材料中具有一个或多个间隙。 将电极放置在涡轮机桶的预制孔中,并且提供电解质以在电极和孔的壁之间流动。 在施加电流时,直接与电极的非绝缘部分相对的内壁表面的材料部分被溶解,形成凹槽。 电极的绝缘部分沿着孔的轴线离开轴向间隔开的一列突起。 行或突起中的间隙轴向不对准。 这些突起在铲斗的冷却流动通道中形成涡轮,提高了传热系数。

    Curved turbulator configuration for airfoils and method and electrode for machining the configuration
    9.
    发明授权
    Curved turbulator configuration for airfoils and method and electrode for machining the configuration 有权
    用于机翼的弯曲湍流器配置和用于加工配置的方法和电极

    公开(公告)号:US06554571B1

    公开(公告)日:2003-04-29

    申请号:US09683189

    申请日:2001-11-29

    Abstract: A curved turbulator configuration is in a radial cooling passage of an airfoil, where the radial cooling passage is defined by at least a leading wall and a trailing wall, and the airfoil includes a tip and a root. The curved turbulator configuration includes a number of spaced curved turbulator pairs positioned along a center-line on an inner surface of the leading wall and a number of spaced complementary curved turbulator pairs positioned along a center-line on an inner surface of the trailing wall. An electrode for forming the curved turbulator configuration in the radial cooling passage includes a leading face having a curved turbulator pattern, a trailing face having a complementary curved turbulator pattern, a conductive core, and an insulating coating disposed thereon that is partly removed.

    Abstract translation: 弯曲的湍流器构造在翼型件的径向冷却通道中,其中径向冷却通道由至少前导壁和后壁限定,并且翼型件包括尖端和根部。 弯曲的湍流器构造包括沿着前壁的内表面上的中心线定位的多个间隔开的弯曲的湍流器对,以及沿着后壁的内表面上的中心线定位的多个间隔开的互补弯曲湍流器对。 用于在径向冷却通道中形成弯曲的湍流器构造的电极包括具有弯曲的湍流器图案的前表面,具有互补弯曲湍流器图案的后表面,导电芯和位于其上的部分去除的绝缘涂层。

    Apparatus and method for rejuvenating cooling passages within a turbine airfoil
    10.
    发明授权
    Apparatus and method for rejuvenating cooling passages within a turbine airfoil 失效
    涡轮机翼中的冷却通道的再生装置和方法

    公开(公告)号:US06743350B2

    公开(公告)日:2004-06-01

    申请号:US10063087

    申请日:2002-03-18

    CPC classification number: B23H9/16 B23H9/10

    Abstract: An electrode for rejuvenating a cooling passage within an airfoil, the electrode including a tip, an end, a conductive core extending between the tip and the end, and an insulating coating disposed on the conductive core. The insulating coating exposes a number of conductive strips of the conductive core extending between the tip and the end. The insulating coating forms a number of insulating portions and further exposes a number of spacer portions of the conductive core longitudinally positioned between the insulating portions. The insulating portions substantially span a distance between the tip and the end and are positioned between the conductive strips.

    Abstract translation: 一种用于振动翼型内的冷却通道的电极,所述电极包括尖端,端部,在尖端和端部之间延伸的导电芯,以及设置在导电芯上的绝缘涂层。 绝缘涂层暴露出在尖端和端部之间延伸的多个导电芯的导电条。 绝缘涂层形成多个绝缘部分,并进一步暴露导体芯的多个间隔部分纵向定位在绝缘部分之间。 绝缘部分基本上跨越尖端和端部之间的距离并且位于导电条之间。

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