公开(公告)号：US20160047253A1

公开(公告)日：2016-02-18

申请号：US14096087

申请日：2013-12-04

Applicant: General Electric Company

Inventor： John David Ward, JR. ,  Canan Uslu Hardwicke ,  Jonathan Matthew Lomas ,  Cem Murat Eminoglu ,  Thomas Robert Reid

IPC: F01D5/28 ,  B05B15/04

CPC classification number: F01D5/288 ,  B05B12/16 ,  B23P2700/06 ,  C23C4/02 ,  F01D5/186 ,  F01D11/122 ,  F05D2240/11 ,  Y02T50/676 ,  Y02T50/6765

Abstract: Methods for selective localized coating deposition for a turbine component include providing the turbine component comprising an exterior surface with one or more surface features and selectively coating at least a portion of the exterior surface using a localized coating deposition apparatus based on a location of at least one of the one or more surface features.

Abstract translation: 用于涡轮机部件的选择性局部涂覆沉积的方法包括提供包括具有一个或多个表面特征的外表面的涡轮机部件，并且使用局部涂覆沉积设备选择性地涂覆外表面的至少一部分，基于至少一个 的一个或多个表面特征。

公开(公告)号：US20150174837A1

公开(公告)日：2015-06-25

申请号：US14568443

申请日：2014-12-12

Applicant: General Electric Company

Inventor： Sandra Beverly Kolvick ,  Don Mark Lipkin ,  Jonathan Matthew Lomas ,  Thomas Robert Reid ,  Jacob John Kittleson

IPC: B29C73/02

CPC classification number: B29C73/025 ,  B29K2103/04 ,  B29L2031/08

Abstract: A turbine component patch delivery system can include a support arm and a deposition tool supported by the support arm. The deposition tool can include a reservoir configured to house a turbine component patch material and a dispenser configured to dispense the turbine component patch material from the reservoir onto a surface of a turbine component.

Abstract translation: 涡轮机部件补片输送系统可以包括由支撑臂支撑的支撑臂和沉积工具。 沉积工具可以包括构造成容纳涡轮机部件补片材料的储存器和配置成将涡轮机部件补片材料从储存器分配到涡轮机部件的表面上的分配器。

公开(公告)号：US10960481B2

公开(公告)日：2021-03-30

申请号：US15656063

申请日：2017-07-21

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Thomas Robert Reid ,  Jonathan Matthew Lomas ,  Gary Charles Shubert

IPC: B23K9/04 ,  F01D5/28 ,  F23R3/00 ,  F02C7/22 ,  F01D5/22 ,  B23K9/173 ,  B23K9/32 ,  B23P15/02 ,  B23P15/04 ,  F01D5/12 ,  B23K101/00 ,  B23K103/18 ,  F01D5/00 ,  F01D5/18

Abstract: A method for modifying an aperture in a component, a system for modifying flow through a component, and a turbine component are disclosed. The method includes providing a substrate having at least one aperture having an electrically-conductive surface, providing a deposition device including an ESD torch, the ESD torch including an aperture penetrating electrode including a conductive material, inserting the aperture penetrating electrode at least partially into the aperture, and generating an arc between the aperture penetrating electrode and the electrically-conductive surface to deposit electrode material within the aperture. The system includes the ESD torch removably supported in an electrode holder. The turbine component includes at least one aperture having an electrospark deposited material along an electrically-conductive surface, the electrospark deposited material providing modified fluid flow through the turbine component.

公开(公告)号：US09744614B2

公开(公告)日：2017-08-29

申请号：US14082814

申请日：2013-11-18

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Thomas Robert Reid ,  Jonathan Matthew Lomas ,  Gary Charles Shubert

IPC: B23K9/04 ,  F01D5/28 ,  F23R3/00 ,  F02C7/22 ,  F01D5/22 ,  B23K9/173 ,  B23K9/32 ,  B23P15/02 ,  B23P15/04 ,  F01D5/12 ,  B23K101/00 ,  F01D5/00 ,  F01D5/18 ,  B23K103/18

CPC classification number: B23K9/044 ,  B23K9/048 ,  B23K9/173 ,  B23K9/32 ,  B23K2101/001 ,  B23K2103/26 ,  B23P15/02 ,  B23P15/04 ,  B23P2700/06 ,  F01D5/005 ,  F01D5/12 ,  F01D5/186 ,  F01D5/225 ,  F01D5/286 ,  F02C7/22 ,  F05D2230/12 ,  F05D2230/80 ,  F05D2260/20 ,  F23R3/002 ,  Y10T428/13 ,  Y10T428/24273

Abstract: A method for modifying an aperture in a component, a system for modifying flow through a component, and a turbine component are disclosed. The method includes providing a substrate having at least one aperture having an electrically-conductive surface, providing a deposition device including an ESD torch, the ESD torch including an aperture penetrating electrode including a conductive material, inserting the aperture penetrating electrode at least partially into the aperture, and generating an arc between the aperture penetrating electrode and the electrically-conductive surface to deposit electrode material within the aperture. The system includes the ESD torch removably supported in an electrode holder. The turbine component includes at least one aperture having an electrospark deposited material along an electrically-conductive surface, the electrospark deposited material providing modified fluid flow through the turbine component.

公开(公告)号：US09382813B2

公开(公告)日：2016-07-05

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 ,  F01D11/00

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。

公开(公告)号：US20160089692A1

公开(公告)日：2016-03-31

申请号：US14501607

申请日：2014-09-30

Applicant: General Electric Company

Inventor： Thomas Robert Reid ,  Jonathan Matthew Lomas

IPC: B05D1/32 ,  B05D1/28 ,  B05D3/12 ,  F01D25/00 ,  B05D5/00 ,  C23C4/12 ,  C23C28/00 ,  F01D5/28 ,  B05D1/36 ,  B05D7/14

CPC classification number: B05D1/322 ,  B05D1/28 ,  B05D1/36 ,  B05D3/12 ,  B05D5/00 ,  B05D7/14 ,  C23C4/01 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  C23C24/04 ,  C23C28/00 ,  F01D5/186 ,  F01D5/288 ,  F05D2230/90 ,  F05D2260/201 ,  F05D2260/202

Abstract: Turbine component coating processes include applying a malleable masking material to one or more apertures of one or more fluid flow passages within a turbine component surface and then applying a first coating over the malleable masking material and on the turbine component surface. The turbine component coating processes further include locally applying a local masking material to the one or more apertures of the one or more fluid flow passages and then applying a second coating over the local masking material and on the first coating.

Abstract translation: 涡轮机部件涂覆方法包括将可延展的掩模材料施加到涡轮机部件表面内的一个或多个流体流动通道的一个或多个孔中，然后在可延展的掩模材料上和涡轮机部件表面上施加第一涂层。 涡轮机部件涂覆方法还包括将局部掩蔽材料局部施加到一个或多个流体流动通道的一个或多个孔中，然后在局部掩蔽材料上和第一涂层上施加第二涂层。

公开(公告)号：US20150160644A1

公开(公告)日：2015-06-11

申请号：US14097902

申请日：2013-12-05

Applicant: General Electric Company

Inventor： Thomas Robert Reid ,  Mustafa Yuvalaklioglu ,  Blake Allen Fulton ,  Julio Eduardo Lanza ,  Gareth William David Lewis ,  Jonathan Matthew Lomas ,  Francis Alexander Reed

IPC: G05B19/18 ,  G05D7/06

CPC classification number: G05B19/182 ,  G05B19/401 ,  G05B19/4099 ,  G05B2219/37205 ,  G05B2219/45147 ,  G05B2219/49001 ,  G05B2219/50214 ,  G05D7/0617 ,  Y10T29/49748

Abstract: A repair method is provided and includes deriving, from a model of a component, drilling vectors respectively associated with fluid flow passages of the component, obtaining location data of each of the fluid flow passages at least partially from a source other than the model and relying upon the derived drilling vectors and the obtained location data of each of the fluid flow passages to position a tool configured to modify each of the fluid flow passages.

Abstract translation: 提供了一种修复方法，包括从部件的模型中导出分别与部件的流体流动通道相关联的钻井矢量，至少部分地从除模型之外的源获得每个流体流动通道的位置数据，并依赖 在所得到的钻井矢量和获得的每个流体流动通道的位置数据之间定位用于修改每个流体流动通道的工具。