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    SEAL RETAINING ASSEMBLY
    1.
    发明申请
    SEAL RETAINING ASSEMBLY 有权
    密封保持装置

    公开(公告)号：US20160102578A1

    公开(公告)日：2016-04-14

    申请号：US14511716

    申请日：2014-10-10

    Applicant: General Electric Company

    Inventor： Karol Filip Leszczynski ,  Christopher Warren Childs ,  David Matthew Clarida ,  Gregory Allan Crum ,  Mitchel Merck ,  Alexander Maxim Libers

    IPC: F01D25/24 ,  F01D25/30 ,  F16J15/32 ,  F01D25/26

    CPC classification number: F01D25/243 ,  F01D11/005 ,  F01D25/26 ,  F01D25/30 ,  F01D25/305 ,  F02C7/28 ,  F05D2240/55 ,  F16J15/061 ,  F16J15/322 ,  F16J15/3268

    Abstract: A seal retaining assembly includes a first segment coupled to a first structure. Also included is a recess of the first segment, the recess defined by a first and second wall, the first wall defining a first wall aperture, the second wall defining a second wall aperture. Further included is a second segment having a tab disposed within the recess in fitted contact with the first and second wall to retain the second segment to the first segment in a radial direction, the tab defining a tab aperture, the first and second segment defining an axial gap therebetween, the first wall aperture, the second wall aperture and the tab aperture are aligned to form a passage. Yet further included is a flex seal within the axial gap. Also included is a pin in the passage to fix the second segment to the first segment in axial and circumferential directions.

    Abstract translation: 密封保持组件包括联接到第一结构的第一段。 还包括第一段的凹部，由第一和第二壁限定的凹部，第一壁限定第一壁孔，第二壁限定第二壁孔。 还包括第二部分，其具有设置在凹部内的突出部，该突出部与第一和第二壁嵌合接触，以沿径向方向将第二部分保持在第一部分上，突出部限定突出部孔，第一和第二部分限定 第一壁孔，第二壁孔和突片孔对准以形成通道。 还包括在轴向间隙内的柔性密封。 还包括在通道中的销，以将第二段在轴向和圆周方向上固定到第一段。

    Gas turbine half-casing lifting and shipping fixture
    3.
    发明授权
    Gas turbine half-casing lifting and shipping fixture 有权
    燃气轮机半壳提升和运输夹具

    公开(公告)号：US09273569B2

    公开(公告)日：2016-03-01

    申请号：US13736421

    申请日：2013-01-08

    Applicant: General Electric Company

    Inventor： Jason Allen Seale ,  Gregory Allan Crum ,  Netaji Haribhau Mane

    IPC: F01D25/26 ,  F01D25/28 ,  F01D25/24

    CPC classification number: F01D25/243 ,  F01D25/26 ,  F01D25/285 ,  F05D2260/02

    Abstract: A lifting fixture assembly adapted for shipping and/or lifting includes a lower turbine casing having two horizontal joint flanges adapted to engage mating flanges on an upper-turbine casing. The horizontal joint flanges are provided with plural bolt holes used for securing the upper turbine casing to the lower turbine casing. A plurality of cross-beams extend transversely across the lower turbine casing, removably secured to said horizontal joint flanges, using selected ones of the existing bolt holes.

    Abstract translation: 适于运输和/或提升的起重工具组件包括具有两个水平接头凸缘的下涡轮机壳体，其适于接合上涡轮机壳体上的配合凸缘。 水平接头凸缘设有多个螺栓孔，用于将上涡轮机壳体固定到下涡轮机壳体。 多个横梁横向延伸穿过下涡轮机壳体，使用选定的现有螺栓孔可拆卸地固定到所述水平接头凸缘。

    HORIZONTAL JOINT FOR A ROTARY MACHINE AND METHOD OF ASSEMBLING SAME
    4.
    发明申请
    HORIZONTAL JOINT FOR A ROTARY MACHINE AND METHOD OF ASSEMBLING SAME 审中-公开
    旋转机的水平接头及其组装方法

    公开(公告)号：US20150345332A1

    公开(公告)日：2015-12-03

    申请号：US14287717

    申请日：2014-05-27

    Applicant: General Electric Company

    Inventor： Christopher Paul Cox ,  Kenneth Damon Black ,  Mitchell Allan Merrill ,  Gregory Allan Crum

    IPC: F01D25/24 ,  F04D29/52

    CPC classification number: F01D25/243 ,  F01D9/041 ,  F04D17/122 ,  F04D19/02 ,  F04D29/522 ,  F04D29/624 ,  F04D29/644 ,  F05D2230/64 ,  Y10T29/49321 ,  Y10T403/7075

    Abstract: A horizontal joint of a rotary machine barrel includes first and second section mating surfaces that extend axially adjacent to the joint, and a plurality of gaps and a plurality of tangs disposed axially along the first and second section mating surfaces, respectively. Each tang has an axially extending tang aperture defined therethrough. Each gap is sized and axially spaced to receive a corresponding tang. Additionally, the joint includes a plurality of mating surface segments defined along the first section mating surface. Each segment extends axially between a corresponding pair of gaps and has an axially extending segment aperture defined therethrough. The tang apertures and segment apertures align to form a generally continuous axial pin aperture when the second section mating surface is positioned against the first section mating surface.

    Abstract translation: 旋转机筒的水平接头包括分别沿轴向相对于接头延伸的第一和第二部分配合表面，以及分别沿第一和第二部分配合表面轴向设置的多个间隙和多个柄脚。 每个脚具有穿过其限定的轴向延伸的脚孔。 每个间隙的尺寸和轴向间隔开以接收相应的柄脚。 另外，接头包括沿着第一部分配合表面限定的多个配合表面段。 每个段在相应的一对间隙之间轴向延伸并且具有通过其限定的轴向延伸的节段孔。 当第二部分配合表面抵靠第一部分配合表面定位时，柄部孔和节段孔对齐以形成大致连续的轴向销孔。

    Gas turbine half-casing shipping fixture
    6.
    发明授权
    Gas turbine half-casing shipping fixture 有权
    燃气轮机半壳运输夹具

    公开(公告)号：US08876448B1

    公开(公告)日：2014-11-04

    申请号：US14012503

    申请日：2013-08-28

    Applicant: General Electric Company

    Inventor： John Raymond Hess ,  Netaji Haribhau Mane ,  Gregory Allan Crum ,  Jason Allen Seale ,  David William Hogg

    IPC: B60P7/08 ,  B60P7/06

    CPC classification number: B60P7/06 ,  F01D25/28 ,  F01D25/285 ,  F05D2260/02

    Abstract: A shipping fixture for a turbine lower casing includes a frame having a substantially rectangular shape including a pair of elongated, laterally-spaced side beams and a pair of transverse end beams. A first lateral support structure extends between the side beams at a first location corresponding to a first vertically-oriented joint between the turbine compressor casing section and the turbine combustor casing section; and a second lateral support structure includes support blocks mounted on the side beams at a second location corresponding to a second vertically-oriented joint between the turbine combustor casing section and the turbine stage casing section.

    Abstract translation: 用于涡轮机下壳体的运输夹具包括具有基本上矩形形状的框架，该框架包括一对细长的，横向间隔开的侧梁和一对横向端梁。 第一侧向支撑结构在对应于涡轮压缩机壳体部分和涡轮机燃烧器壳体部分之间的第一垂直定向接头的第一位置处在侧梁之间延伸; 并且第二横向支撑结构包括安装在所述侧梁上的支撑块，所述支撑块在对应于所述涡轮燃烧器壳体部分和所述涡轮级壳体部分之间的第二垂直定向接头的第二位置处。

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