公开(公告)号：US20150252673A1

公开(公告)日：2015-09-10

申请号：US14198659

申请日：2014-03-06

Applicant: General Electric Company

Inventor： Brad Wilson VanTassel ,  James Ryan Connor ,  Bryan David Lewis ,  Adebukola Oluwaseun Benson

IPC: F01D5/08 ,  B23P15/02

CPC classification number: F01D5/082 ,  B23P15/02 ,  F01D5/187 ,  F01D11/24 ,  F05D2240/11 ,  F05D2240/81 ,  F05D2260/201 ,  Y02T50/676 ,  Y10T29/49341

Abstract: Platform cooling arrangements in a turbine rotor blade include a feedhole that extends from the suction side slash face to the interior cooling passage, and, one or more branch holes that each extends from the feedhole to the suction side slash face such that coolant flows from the interior cooling passage, through the feedhole to the one or more branch holes and exits the platform along the suction side slash face.

Abstract translation: 涡轮转子叶片中的平台冷却装置包括从吸入侧斜面向内部冷却通道延伸的进料孔，以及一个或多个分支孔，每个分支孔从进料孔延伸到吸入侧斜面，使得冷却剂从 内部冷却通道，通过进料孔到达一个或多个分支孔，并沿吸力侧斜面离开平台。

公开(公告)号：US09567860B2

公开(公告)日：2017-02-14

申请号：US13685943

申请日：2012-11-27

Applicant: General Electric Company

Inventor： Jacob Andrew Salm ,  James Ryan Connor ,  John David Ward, Jr.

IPC: B25B11/00 ,  F01D5/22 ,  B23P6/00 ,  F01D5/00

CPC classification number: F01D5/225 ,  B23P6/002 ,  F01D5/005 ,  F05D2260/94 ,  F05D2270/332 ,  Y10T29/49318

Abstract: According to one aspect, a fixture for an airfoil shroud having a first end edge, a second end edge, a leading edge, a trailing edge, a radially outer side and a radially inner side with respect to a rotor axis of a bucket having the airfoil shroud is provided. The fixture includes a base plate, a first member extending from the base plate configured to locate and abut the first end edge, a second member extending from the base plate configured to locate and abut a side of a seal rail, a third member extending from the base plate configured to locate and abut the radially outer side of the airfoil shroud and a template recess formed in the base plate proximate the first end edge to define a geometry of a relief cut in the trailing edge of the airfoil shroud.

Abstract translation: 根据一个方面，一种用于翼型护罩的固定装置，具有相对于桶的转子轴线具有第一端边缘，第二端边缘，前缘，后缘，径向外侧和径向内侧， 提供翼型护罩。 所述固定装置包括基板，从所述基板延伸的第一构件，所述第一构件被构造成定位和邻接所述第一端边缘;第二构件，其从所述基板延伸，所述第二构件从所述基板延伸，所述第二构件被构造成定位和邻接密封轨的侧面;第三构件， 所述基板被构造成定位并邻接所述翼型件护罩的径向外侧，以及形成在靠近所述第一端边缘的所述基板中的模板凹部，以限定在所述翼型件护罩的后缘中切割的浮雕的几何形状。

公开(公告)号：US20160146014A1

公开(公告)日：2016-05-26

申请号：US14548656

申请日：2014-11-20

Applicant: General Electric Company

Inventor： James Ryan Connor ,  Robert Trent Hullender ,  Keith Alan Lord

IPC: F01D5/14 ,  B23H9/10 ,  F01D5/00

CPC classification number: B23H9/10 ,  B23K26/342 ,  B23K2101/001 ,  B23P6/007 ,  F01D5/005 ,  F05D2230/31 ,  F05D2240/80

Abstract: Methods for modifying bucket platforms of turbine buckets include removing a portion of the bucket platform to form a void, wherein the void comprises a predetermined geometry, and adding a filler material in a plurality of layers to fill the void.

Abstract translation: 用于修改涡轮机铲斗的铲斗平台的方法包括移除铲斗平台的一部分以形成空隙，其中空隙包括预定几何形状，并且在多个层​​中加入填充材料以填充空隙。

公开(公告)号：US09151587B2

公开(公告)日：2015-10-06

申请号：US14076558

申请日：2013-11-11

Applicant: General Electric Company

Inventor： John David Ward, Jr. ,  Juan Pablo Cilia ,  James Ryan Connor ,  Jason Adam Neville ,  Christopher Allen Nafis ,  Neil Robert Peddar ,  Antonio Rodriguez ,  Daniel Howard Tragesser

IPC: G01B5/008 ,  G01B5/20 ,  G01B5/00 ,  F01D11/00

CPC classification number: G01B5/008 ,  F01D11/00 ,  F01D25/285 ,  F05D2260/83 ,  G01B5/0002 ,  G01B5/0004 ,  G01B5/205

Abstract: A bucket tip shroud measurement fixture includes a frame extending from a first end to a second end through an intermediate portion having a first surface and an opposing second surface, a first tip shroud fixing member extending from the second surface of the frame at the first end, and a second tip shroud fixing member extending from the second surface of the frame at the second end. The first and second tip shroud fixing members are configured and disposed to retain and establish an orientation of a bucket tip shroud relative the frame. A plurality of reference points are provided on the frame. The plurality of reference points are configured and disposed to receive a coordinate measuring machine (CMM) probe.

Abstract translation: 铲斗顶部护罩测量夹具包括：框架，其从第一端延伸到第二端，通过具有第一表面和相对的第二表面的中间部分;第一末端护罩固定件，在第一端从框架的第二表面延伸; 以及在第二端处从框架的第二表面延伸的第二顶端罩固定构件。 第一和第二末端罩固定构件被构造和设置成保持并建立相对于框架的铲斗顶部护罩的取向。 在框架上设置多个参考点。 多个参考点被配置和设置成接收坐标测量机（CMM）探针。

公开(公告)号：US20150128433A1

公开(公告)日：2015-05-14

申请号：US14076558

申请日：2013-11-11

Applicant: General Electric Company

Inventor： John David Ward, JR. ,  Juan Pablo Cilia ,  James Ryan Connor ,  Jason Adam Neville ,  Christopher Allen Nafis ,  Neil Robert Peddar ,  Antonio Rodriguez ,  Daniel Howard Tragesser

IPC: G01B5/008

CPC classification number: G01B5/008 ,  F01D11/00 ,  F01D25/285 ,  F05D2260/83 ,  G01B5/0002 ,  G01B5/0004 ,  G01B5/205

Abstract: A bucket tip shroud measurement fixture includes a frame extending from a first end to a second end through an intermediate portion having a first surface and an opposing second surface, a first tip shroud fixing member extending from the second surface of the frame at the first end, and a second tip shroud fixing member extending from the second surface of the frame at the second end. The first and second tip shroud fixing members are configured and disposed to retain and establish an orientation of a bucket tip shroud relative the frame. A plurality of reference points are provided on the frame. The plurality of reference points are configured and disposed to receive a coordinate measuring machine (CMM) probe.

Abstract translation: 铲斗顶部护罩测量夹具包括：框架，其从第一端延伸到第二端，通过具有第一表面和相对的第二表面的中间部分;第一末端护罩固定件，在第一端从框架的第二表面延伸; 以及在第二端处从框架的第二表面延伸的第二顶端罩固定构件。 第一和第二末端罩固定构件被构造和设置成保持并建立相对于框架的铲斗顶部护罩的取向。 在框架上设置多个参考点。 多个参考点被配置和设置成接收坐标测量机（CMM）探针。

公开(公告)号：US20140157597A1

公开(公告)日：2014-06-12

申请号：US13708069

申请日：2012-12-07

Applicant: GENERAL ELECTRIC COMPANY

Inventor： James Ryan Connor ,  Michael Anthony DePalma ,  Christine Ryan Parker ,  John David Ward, Jr.

IPC: B23P6/00

CPC classification number: B23P6/002 ,  C23C28/321 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/005 ,  F05D2230/80 ,  F05D2260/80 ,  Y10T29/49318 ,  Y10T29/49764

Abstract: A method of locally inspecting and repairing a coated component is provided. The method includes determining an area of interest on the coated component, wherein the area of interest has little to no visible damage. The method also includes removing a coating proximate the area of interest to expose a base material of the coated component. The method further includes inspecting the area of interest for damage to the base material.

Abstract translation: 提供了一种局部检查和修复涂覆部件的方法。 该方法包括确定涂覆部件上的感兴趣区域，其中感兴趣的区域几乎没有或没有可见的损伤。 该方法还包括去除感兴趣区域附近的涂层以暴露涂覆部件的基底材料。 该方法还包括检查感兴趣区域是否损坏基材。