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    CENTERLINE SUPPORT BAR FOR STEAM TURBINE COMPONENT
    2.
    发明申请
    CENTERLINE SUPPORT BAR FOR STEAM TURBINE COMPONENT 审中-公开
    蒸汽涡轮机组件的中心支撑杆

    公开(公告)号：US20160319701A1

    公开(公告)日：2016-11-03

    申请号：US15208802

    申请日：2016-07-13

    Applicant: General Electric Company

    Inventor： Stephen Roger Swan ,  Matthew Edward Renninger ,  Kevin John Lewis Roy ,  Prashant Prabhakar Sankolli

    IPC: F01D25/28 ,  F01D25/24 ,  F01D9/04

    CPC classification number: F02C7/20 ,  F01D9/04 ,  F01D9/042 ,  F01D25/246 ,  F01D25/28 ,  F05D2220/31 ,  F05D2230/644 ,  F05D2240/128 ,  F05D2240/14 ,  F05D2240/90

    Abstract: A centerline support bar for steam turbine component assembly, installation, and/or alignment is disclosed. In one embodiment, the support bar includes a body portion configured to be disposed across a centerline of a steam turbine, the body portion configured to transversely connect to a steam turbine component; and a first flange extending from the body portion and configured to contact a steam turbine casing, wherein the steam turbine support bar is configured to non-affixedly join the steam turbine casing to the steam turbine component.

    Abstract translation: 公开了用于汽轮机部件组装，安装和/或对准的中心线支撑杆。 在一个实施例中，支撑杆包括主体部分，该主体部分配置成跨越蒸汽轮机的中心线布置，主体部分被配置为横向连接到蒸汽轮机部件; 以及从所述主体部分延伸并且构造成接触蒸汽轮机壳体的第一凸缘，其中所述蒸气涡轮机支撑杆构造成将所述蒸汽涡轮机壳体非贴合地连接到所述蒸汽轮机部件。

    CENTERLINE SUPPORT BAR FOR STEAM TURBINE COMPONENT
    3.
    发明申请
    CENTERLINE SUPPORT BAR FOR STEAM TURBINE COMPONENT 有权
    蒸汽涡轮机组件的中心支撑杆

    公开(公告)号：US20140250915A1

    公开(公告)日：2014-09-11

    申请号：US13785869

    申请日：2013-03-05

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Stephen Roger Swan ,  Matthew Edward Renninger ,  Kevin John Lewis Roy ,  Prashant Prabhakar Sankolli

    IPC: F02C7/20

    CPC classification number: F02C7/20 ,  F01D9/04 ,  F01D9/042 ,  F01D25/246 ,  F01D25/28 ,  F05D2220/31 ,  F05D2230/644 ,  F05D2240/128 ,  F05D2240/14 ,  F05D2240/90

    Abstract: A centerline support bar for steam turbine component assembly, installation, and/or alignment is disclosed. In one embodiment, the support bar includes a body portion configured to be disposed across a centerline of a steam turbine, the body portion configured to transversely connect to a steam turbine component; and a first flange extending from the body portion and configured to contact a steam turbine casing, wherein the steam turbine support bar is configured to non-affixedly join the steam turbine casing to the steam turbine component.

    Abstract translation: 公开了用于汽轮机部件组装，安装和/或对准的中心线支撑杆。 在一个实施例中，支撑杆包括主体部分，该主体部分配置成跨越蒸汽轮机的中心线布置，主体部分被配置为横向连接到蒸汽轮机部件; 以及从所述主体部分延伸并且构造成接触蒸汽轮机壳体的第一凸缘，其中所述蒸气涡轮机支撑杆构造成将所述蒸汽涡轮机壳体非贴合地连接到所述蒸汽轮机部件。

    MODULAR TURBOMACHINE INNER AND OUTER CASINGS WITH MULTI-STAGE STEAM EXTRACTION SITES
    5.
    发明申请
    MODULAR TURBOMACHINE INNER AND OUTER CASINGS WITH MULTI-STAGE STEAM EXTRACTION SITES 审中-公开
    多级涡轮机内部和外部具有多级蒸汽提取站点

    公开(公告)号：US20150252681A1

    公开(公告)日：2015-09-10

    申请号：US14197720

    申请日：2014-03-05

    Applicant: General Electric Company

    Inventor： Dayananda Thukra Kotian ,  Jeyaruban Selliah Amirtharajah ,  Stephen Roger Swan

    IPC: F01D9/06 ,  F01D25/26

    CPC classification number: F01D9/065 ,  F01D25/24 ,  F01D25/26 ,  F01D25/32 ,  F05D2220/31 ,  F05D2230/21 ,  F05D2230/61 ,  Y10T29/49229

    Abstract: Various embodiments include methods and apparatuses of forming turbomachine casing intermediate structures. In some embodiments apparatuses include a steam turbomachine casing intermediate structure including an inner shell having an external surface and inner shell cavity, and defining an opening for allowing fluid entry to the cavity and an outer shell having an internal surface, these surfaces defining at least one closed, axial-extending chamber, the inner shell and outer shells each having access regions adjacent the closed chamber, each of the access regions including a plurality of locations, selectable to be machined to create an exhaust slot or an exhaust opening in the inner casing or the outer casing, respectively, and wherein a structural integrity of the casing is uniform regardless of which of the axial locations are selected to be machined, where the exhaust opening is fluidly connected with the at least one closed chamber through the outer shell.

    Abstract translation: 各种实施例包括形成涡轮机壳体中间结构的方法和装置。 在一些实施例中，设备包括蒸汽涡轮机壳体中间结构，其包括具有外表面和内壳腔的内壳，并且限定用于允许流体进入空腔的开口和具有内表面的外壳，这些表面限定至少一个 封闭的轴向延伸室，所述内壳和外壳各自具有邻近所述封闭室的进入区域，每个所述进入区域包括多个位置，所述多个位置可选择被加工以在所述内壳体中产生排气狭槽或排气开口 或外壳，并且其中壳体的结构完整性是均匀的，而不管选择哪个轴向位置被加工，其中排气口通过外壳与至少一个封闭室流体连接。

    CASING SUPPORT BLOCK FOR STEAM TURBINE NOZZLE ASSEMBLY
    7.
    发明申请
    CASING SUPPORT BLOCK FOR STEAM TURBINE NOZZLE ASSEMBLY 有权
    用于蒸汽涡轮喷嘴组件的支撑块

    公开(公告)号：US20160169047A1

    公开(公告)日：2016-06-16

    申请号：US14567711

    申请日：2014-12-11

    Applicant: General Electric Company

    Inventor： Steven Sebastian Burdgick ,  Jesus Mendoza ,  John Paul Davis ,  Stephen Roger Swan

    IPC: F01D25/28 ,  F01D25/24 ,  F01D5/02 ,  F01D9/04

    CPC classification number: F01D25/28 ,  F01D25/002 ,  F01D25/246 ,  F05D2220/31

    Abstract: A support block for a steam turbine casing, a related assembly and apparatus. Various embodiments include a steam turbine casing support block having: a body portion sized to substantially fill a pocket in a steam turbine casing, the body portion having a greater length than a depth or a width; a set of tabs extending from the body portion, each of the set of tabs sized to substantially fill a corresponding slot in the steam turbine casing, wherein the set of tabs are located at a radially outwardly facing wall of the body portion; and a pin hole on a bottom surface of the body portion for receiving a retaining member.

    Abstract translation: 用于汽轮机壳体的支撑块，相关组件和装置。 各种实施例包括汽轮机壳体支撑块，其具有：主体部分，其大小基本上填充蒸汽轮机壳体中的凹部，主体部分具有比深度或宽度更大的长度; 一组翼片，其从主体部分延伸，每组翼片的尺寸被设计成基本上填充汽轮机壳体中相应的狭槽，其中该组翼片位于主体部分的径向向外的壁上; 以及在主体部分的底表面上的用于接收保持构件的销孔。

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