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    METHOD FOR REMOVING AN END CAP OF A COMBUSTOR CAP ASSEMBLY
    2.
    发明申请
    METHOD FOR REMOVING AN END CAP OF A COMBUSTOR CAP ASSEMBLY 审中-公开
    用于移除燃烧器盖组件的端盖的方法

    公开(公告)号：US20150059177A1

    公开(公告)日：2015-03-05

    申请号：US14010638

    申请日：2013-08-27

    Applicant: General Electric Company

    Inventor： Mark Carmine Bellino ,  Patrick Shawn Reilly ,  James Carroll Baummer ,  Heath Michael Ostebee

    IPC: F23R3/46

    CPC classification number: F23R3/46 ,  F23R3/60 ,  F23R2900/00019 ,  Y10T29/49346

    Abstract: A method for removing an end cap assembly from a combustor cap assembly includes inserting a push rod through an opening in a back plate portion of the cap assembly. One end of the push rod is engaged with a radial support feature of the end cap assembly and a substantially linear force is applied to the push rod. The force is distributed to the radial support feature, thereby preventing damage to a cap plate portion of the end cap assembly.

    Abstract translation: 从燃烧器盖组件移除端盖组件的方法包括将推杆穿过盖组件的后板部分中的开口插入。 推杆的一端与端盖组件的径向支撑部件接合，并且基本上线性的力被施加到推杆上。 力被分配到径向支撑特征，从而防止对端盖组件的盖板部分的损坏。

    SEAL TEST FIXTURE FOR A GAS TURBINE FUEL NOZZLE
    3.
    发明申请
    SEAL TEST FIXTURE FOR A GAS TURBINE FUEL NOZZLE 审中-公开
    燃气涡轮喷嘴的密封测试仪器

    公开(公告)号：US20140250981A1

    公开(公告)日：2014-09-11

    申请号：US13790348

    申请日：2013-03-08

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Brandon Taylor Overby ,  James Carroll Baummer ,  Mark Carmine Bellino

    IPC: G01M3/02

    CPC classification number: G01M15/14 ,  F01D25/285 ,  F23R3/28 ,  F23R2900/00012 ,  G01M3/3281 ,  G01M13/005

    Abstract: A seal test fixture for a gas turbine fuel nozzle including an enclosed container for receiving a body of the gas turbine fuel nozzle including a seal; a test chamber coupled to the enclosed container for sealingly enclosing a flange of the gas turbine fuel nozzle and fluidly communicating with a leak path of the gas turbine fuel nozzle; an air injector opening through which pressurized air is injected into a main fuel chamber of the gas turbine fuel nozzle; and a pressure gauge for measuring an air pressure within the test chamber.

    Abstract translation: 一种用于燃气轮机燃料喷嘴的密封测试夹具，包括用于容纳包括密封件的燃气轮机燃料喷嘴的主体的封闭容器; 耦合到所述封闭容器的测试室，用于密封地封闭所述燃气轮机燃料喷嘴的凸缘并与所述燃气轮机燃料喷嘴的泄漏路径流体连通; 空气喷射器开口，加压空气通过该开口喷射到燃气轮机燃料喷嘴的主燃料室中; 以及用于测量测试室内的空气压力的压力计。

    TURBINE COMPONENT SURFACE TREATMENT PROCESSES AND SYSTEMS
    6.
    发明申请
    TURBINE COMPONENT SURFACE TREATMENT PROCESSES AND SYSTEMS 有权
    涡轮组件表面处理工艺和系统

    公开(公告)号：US20160169035A1

    公开(公告)日：2016-06-16

    申请号：US14568424

    申请日：2014-12-12

    Applicant: General Electric Company

    Inventor： James Carroll Baummer ,  Thomas Robert Reid

    IPC: F01D25/08 ,  B05D1/32 ,  B05C9/04 ,  B05C7/00 ,  B05C9/12 ,  F01D25/00 ,  B05D3/06

    CPC classification number: F01D25/08 ,  B05C7/00 ,  B05C9/04 ,  B05C9/12 ,  B05D1/322 ,  B05D3/067 ,  C23C4/01 ,  C23C14/042 ,  F01D25/002 ,  F05D2230/90

    Abstract: A turbine component surface treatment process includes passing a UV-curable maskant through one or more fluid flow passages, wherein at least a portion of the UV-curable maskant exits the one or more fluid flow passages at an exterior surface of the turbine component, applying a UV light to the exterior surface of the turbine component, wherein the UV light cures at least a portion of the UV-curable maskant exiting the one or more fluid flow passages, and, treating the exterior surface with a treatment material, wherein the portion of the UV-curable maskant cured by the UV light substantially blocks the treatment material from entering the one or more fluid flow passages.

    Abstract translation: 涡轮机部件表面处理方法包括使可UV固化掩蔽剂通过一个或多个流体流动通道，其中至少一部分可UV固化的掩模剂在涡轮机部件的外表面处离开一个或多个流体流动通道，施加 UV光到达所述涡轮机部件的外表面，其中所述UV光固化出离开所述一个或多个流体流动通道的所述UV可固化掩蔽剂的至少一部分，以及用处理材料处理所述外表面，其中所述部分 通过UV光固化的UV可固化掩模剂基本上阻止处理材料进入一个或多个流体流动通道。

    System and method for qualifying usability risk associated with subsurface defects in a multilayer coating
    7.
    发明授权
    System and method for qualifying usability risk associated with subsurface defects in a multilayer coating 有权
    用于评估与多层涂层中的地下缺陷相关的可用性风险的系统和方法

    公开(公告)号：US08759770B1

    公开(公告)日：2014-06-24

    申请号：US13858172

    申请日：2013-04-08

    Applicant: General Electric Company

    Inventor： Steven Charles Woods ,  James Carroll Baummer

    IPC: G01J5/02 ,  G01N25/00 ,  G01N21/88

    CPC classification number: G01N25/72 ,  F01D5/288 ,  F01D21/003 ,  G01N2021/8427 ,  G01N2021/8438 ,  G01N2021/8864

    Abstract: A system for qualifying usability risk associated with subsurface defects in a multilayer coating includes a component having a multilayer coating, an infrared detection device for capturing infrared images of the multilayered coating and a processing unit that is in electronic communication with the infrared detection device where the processing unit generates a subsurface defect map of the multilayer coating based on the infrared images. The system further includes a risk map of the component.

    Abstract translation: 用于限定与多层涂层中的地下缺陷相关的可用性风险的系统包括具有多层涂层的部件，用于捕获多层涂层的红外图像的红外检测装置和与红外线检测装置电子通信的处理单元， 处理单元基于红外图像生成多层涂层的地下缺陷图。 系统还包括组件的风险图。

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