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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
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。
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12.发明授权公开(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。
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13.发明申请公开(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。
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公开(公告)号：US10888892B2
公开(公告)日：2021-01-12
申请号：US16110569
申请日：2018-08-23
Applicant: General Electric Company
Abstract: A method of protecting a hole in a component during a coating process is disclosed. The method includes: placing a plug in the hole, the plug including a water insoluble core and a water soluble layer surrounding at least a portion of an outer surface of the metal core. A coating is applied over the plug and at least a portion of the component. The component is immersed in water to dissolve the water soluble layer, allowing removal of the water insoluble core. Removal of the coating from over the hole and the water insoluble core from within the hole may follow.
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公开(公告)号：US10859367B2
公开(公告)日：2020-12-08
申请号：US15004277
申请日：2016-01-22
Applicant: General Electric Company
Inventor： Yusuf Eren Ozturk , Jonathan Matthew Lomas , Thomas Robert Reid
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.
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Patent Agency Ranking
公开(公告)号：US20190017413A1
公开(公告)日：2019-01-17
申请号：US16133622
申请日：2018-09-17
Applicant: General Electric Company
Inventor： Vadim Bromberg , Jonathan Matthew Lomas , Hongqiang Chen
Abstract: A method of fabricating and repairing a gas turbine component having a plurality of cooling holes defined therein is provided. The method includes determining a parameter of a first cooling hole defined in the gas turbine component, and generating a tool path for forming a protective cap around the first cooling hole. The tool path is based at least partially on the parameter of the first cooling hole. The method also includes directing a robotic device to follow the tool path, and discharging successive layers of ceramic slurry towards the gas turbine component as the tool path is followed such that the protective cap is formed around the first cooling hole.
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17.发明授权公开(公告)号：US09638051B2
公开(公告)日：2017-05-02
申请号：US14017690
申请日：2013-09-04
Applicant: General Electric Company
Inventor： Gareth William David Lewis , Andrew Daniel Grafitti , Jonathan Matthew Lomas , Felipe Roman-Morales , Ronald Lee Souther
IPC: F01D25/24 , F04D3/00 , F04D19/00 , F01D11/02 , F01D5/14 , B23P15/04 , B23P6/00 , F01D5/00 , F01D5/28 , F01D11/00
CPC classification number: F01D11/02 , B23P6/007 , B23P15/04 , F01D5/005 , F01D5/14 , F01D5/288 , F01D11/001 , F05D2230/80 , Y10T29/4932
Abstract: A turbomachine bucket may include an airfoil, a shank coupled to the airfoil, and an angel wing coupled to the shank, the angel wing having an axially extending tip sized to seal with a plurality of discouragers, each discourager having a different axial extent. Various methods for modifying an angel wing to accommodate different sized discouragers are also disclosed.
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18.发明申请公开(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
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。
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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
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。
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公开(公告)号：US20150090303A1
公开(公告)日：2015-04-02
申请号：US14040671
申请日：2013-09-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jonathan Matthew Lomas , Michelle Fullerton Simpson
IPC: B08B3/02
CPC classification number: B08B3/02 , F01D25/002
Abstract: A system includes a plurality of nozzles, a pump configured to pump a fluid through the nozzles, and a manifold configured to arrange the plurality of nozzles to substantially match a shape of a workpiece. Each nozzle of the plurality of nozzles is configured to impinge upon a section of the workpiece with the fluid.
Abstract translation: 一种系统包括多个喷嘴，构造成通过喷嘴泵送流体的泵和被配置成将多个喷嘴布置成基本匹配工件形状的歧管。 多个喷嘴中的每个喷嘴被配置为利用流体冲击工件的一部分。
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