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    TURBINE COMPONENT SURFACE TREATMENT PROCESSES AND SYSTEMS
    1.
    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 LOCATING FLUID FLOW ORIFICES ON A COMPONENT
    3.
    发明申请
    SYSTEM AND METHOD FOR LOCATING FLUID FLOW ORIFICES ON A COMPONENT 审中-公开
    用于定位流体流动元件的组件的系统和方法

    公开(公告)号：US20160223315A1

    公开(公告)日：2016-08-04

    申请号：US15004277

    申请日：2016-01-22

    Applicant: General Electric Company

    Inventor： Yusuf Eren Ozturk ,  Jonathan Matthew Lomas ,  Thomas Robert Reid

    IPC: G01B11/00 ,  H04N5/225 ,  H04N7/18

    CPC classification number: G01B11/002 ,  H04N5/2256 ,  H04N7/183

    Abstract: A fluid flow orifice locating system for locating fluid flow orifices on a component includes a light source, an image capture device, and a controller operably connected to the image capture device. The controller is configured and disposed to create a fluid flow orifice map of the component based on contrast differences on a surface of the component.

    Abstract translation: 用于将流体流孔定位在部件上的流体流量孔定位系统包括光源，图像捕获装置和可操作地连接到图像捕获装置的控制器。 控制器被配置和设置成基于组件的表面上的对比度差异来创建部件的流体流动孔口图。

    AUTOMATED MASKING OF COOLING APERTURES
    4.
    发明申请
    AUTOMATED MASKING OF COOLING APERTURES 审中-公开
    自动封面冷却孔

    公开(公告)号：US20150158044A1

    公开(公告)日：2015-06-11

    申请号：US14098777

    申请日：2013-12-06

    Applicant: General Electric Company

    Inventor： Thomas Robert Reid ,  Cem Murat Eminoglu ,  Jonathan Matthew Lomas

    IPC: B05B12/12 ,  B05D1/02 ,  B05B12/02

    CPC classification number: B05B12/12 ,  B05B12/02 ,  B05D1/02 ,  C23C4/02 ,  F01D5/005 ,  F01D5/186 ,  F05D2230/80

    Abstract: A system including: a masking applicator; and at least one computing device coupled with the masking applicator, the at least one computing device configured to provide instructions to the masking applicator to apply a masking material according to a masking plan for masking at least one cooling aperture in a turbomachine component during a cooling aperture coating process, the masking plan based upon at least one characteristic of the plurality of cooling apertures, the masking plan including masking the at least one cooling aperture using a first mask type.

    Abstract translation: 一种系统，包括：掩模施加器; 以及至少一个与所述掩蔽施用器耦合的计算设备，所述至少一个计算设备被配置为向所述掩蔽施加器提供指令，以根据掩蔽计划施加掩蔽材料，以在冷却过程中屏蔽所述涡轮机组件中的至少一个冷却孔 所述掩模计划基于所述多个冷却孔的至少一个特征，所述掩蔽平面包括使用第一掩模类型掩蔽所述至少一个冷却孔。

    Coating methods and a coated substrate
    5.
    发明授权
    Coating methods and a coated substrate 有权
    涂布方法和涂布基材

    公开(公告)号：US09551058B2

    公开(公告)日：2017-01-24

    申请号：US14098599

    申请日：2013-12-06

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Thomas Robert Reid ,  Paul Stephen Dimascio ,  Jonathan Matthew Lomas ,  Cem Murat Eminoglu

    IPC: B05D1/32 ,  C23C4/00 ,  C23C4/18 ,  C23C14/04 ,  C23C14/58

    CPC classification number: C23C4/01 ,  B05D1/32 ,  C23C4/134 ,  C23C4/18 ,  C23C14/044 ,  C23C14/588 ,  Y10T428/24322

    Abstract: Coating methods and a coated substrate are provided. The coating method includes providing a component having an aperture formed in a surface thereof, arranging and disposing a hollow member on a portion of the surface to define a hollow space above the aperture corresponding to a shape of the aperture at the surface, applying at least one coating over the surface of the component and the hollow member to form an applied coating having an applied coating thickness, and removing at least a portion of the hollow member to expose the hollow space through the applied coating. The coated substrate includes a component having an aperture formed in a surface thereof, a hollow member arranged and disposed on the surface to define a hollow space above the aperture, and an applied coating over the surface of the component, the hollow space being exposed through the applied coating.

    Abstract translation: 提供涂布方法和涂布的基材。 该涂覆方法包括提供一个具有在其表面中形成的孔的部件，在该表面的一部分上布置和设置中空部件，以在孔的上方限定一个与表面上的孔的形状对应的中空空间，至少施加 一个涂层在部件的表面上和中空部件上，以形成具有涂覆涂层厚度的涂覆涂层，以及去除中空部件的至少一部分以通过涂覆的涂层露出中空空间。 涂覆的基底包括具有在其表面中形成的孔的部件，布置并设置在表面上以限定孔的上方的中空空间的中空部件，以及涂覆在部件表面上的涂层，中空空间暴露于 涂层。

    Method and system for detecting surface features on turbine components
    6.
    发明授权
    Method and system for detecting surface features on turbine components 有权
    用于检测涡轮机部件表面特征的方法和系统

    公开(公告)号：US09348001B2

    公开(公告)日：2016-05-24

    申请号：US14058513

    申请日：2013-10-21

    Applicant: General Electric Company

    Inventor： Thomas Robert Reid ,  Paul Stephen Dimascio ,  Jonathan Matthew Lomas

    IPC: G01M15/14 ,  G01R33/038 ,  G01N27/90

    CPC classification number: G01R33/038 ,  G01N27/90 ,  G01N27/902

    Abstract: A system for locating at least one surface feature, such as a cooling aperture, on a turbine component is provided. The system includes at least one feature marker configured for placement adjacent to the at least one surface feature. The system also includes at least one sensor configured for non-visual detection of the at least one feature marker. The system also includes a control device coupled to the at least one sensor for receiving signals from the at least one sensor, wherein the signals represent data indicative of one of a presence of the at least one feature marker and an absence of the at least one feature marker.

    Abstract translation: 提供了一种用于在涡轮机部件上定位至少一个表面特征（例如冷却孔）的系统。 所述系统包括至少一个特征标记，其被配置用于邻近所述至少一个表面特征的放置。 该系统还包括配置用于至少一个特征标记的非视觉检测的至少一个传感器。 所述系统还包括耦合到所述至少一个传感器的控制装置，用于接收来自所述至少一个传感器的信号，其中所述信号表示指示所述至少一个特征标记的存在之一的数据，以及所述至少一个 特征标记。

    METHOD AND SYSTEM FOR DETECTING SURFACE FEATURES ON TURBINE COMPONENTS
    7.
    发明申请
    METHOD AND SYSTEM FOR DETECTING SURFACE FEATURES ON TURBINE COMPONENTS 有权
    用于检测涡轮机组件表面特征的方法和系统

    公开(公告)号：US20150107341A1

    公开(公告)日：2015-04-23

    申请号：US14058513

    申请日：2013-10-21

    Applicant: General Electric Company

    Inventor： Thomas Robert Reid ,  Paul Stephen Dimascio ,  Jonathan Matthew Lomas

    IPC: G01M15/14 ,  G01R33/038

    CPC classification number: G01R33/038 ,  G01N27/90 ,  G01N27/902

    Abstract: A system for locating at least one surface feature, such as a cooling aperture, on a turbine component is provided. The system includes at least one feature marker configured for placement adjacent to the at least one surface feature. The system also includes at least one sensor configured for non-visual detection of the at least one feature marker. The system also includes a control device coupled to the at least one sensor for receiving signals from the at least one sensor, wherein the signals represent data indicative of one of a presence of the at least one feature marker and an absence of the at least one feature marker.

    Abstract translation: 提供了一种用于在涡轮机部件上定位至少一个表面特征（例如冷却孔）的系统。 所述系统包括至少一个特征标记，其被配置用于邻近所述至少一个表面特征的放置。 该系统还包括配置用于至少一个特征标记的非视觉检测的至少一个传感器。 所述系统还包括耦合到所述至少一个传感器的控制装置，用于接收来自所述至少一个传感器的信号，其中所述信号表示指示所述至少一个特征标记的存在之一的数据，以及所述至少一个 特征标记。

    TURBOMACHINE DIAPHRAGM RING WITH PACKING RETAINMENT APPARATUS
    8.
    发明申请
    TURBOMACHINE DIAPHRAGM RING WITH PACKING RETAINMENT APPARATUS 有权
    带包装保持装置的涡轮管膜

    公开(公告)号：US20140154070A1

    公开(公告)日：2014-06-05

    申请号：US13693644

    申请日：2012-12-04

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Thomas Robert Reid ,  James Peter Anderson ,  Steven Sebastian Burdgick ,  Mark Richard DeLorenzo

    IPC: F01D25/24 ,  F01D9/04

    CPC classification number: F01D25/246 ,  F01D9/04 ,  F01D11/003 ,  F01D25/24 ,  F05D2220/31

    Abstract: Various embodiments include a turbomachine diaphragm ring. In various particular embodiments, a turbomachine diaphragm ring includes: a packing slot sized to house a dovetail section of a turbomachine packing, the packing slot extending circumferentially about a rotational axis of the turbomachine; a key slot connected with the packing slot sized to house a portion of a key member, the key slot extending at least one of radially or axially from the packing slot; and a retaining slot connected with the key slot and extending substantially circumferentially from the key slot, the retaining slot sized to house a retaining member for retaining the key member.

    Abstract translation: 各种实施例包括涡轮机隔膜环。 在各种具体实施例中，涡轮机隔膜环包括：尺寸设计成容纳涡轮机填料的燕尾部分的填料槽，所述填料槽围绕涡轮机的旋转轴线周向延伸; 与所述包装槽连接的钥匙槽，其尺寸适于容纳钥匙件的一部分，所述钥匙槽从所述包装槽径向或轴向延伸至少一个; 以及保持狭槽，其与所述键槽连接并且从所述键槽基本上周向地延伸，所述保持狭槽的尺寸被设计成容纳用于保持所述键构件的保持构件。

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