公开(公告)号：US20140356056A1

公开(公告)日：2014-12-04

申请号：US13905669

申请日：2013-05-30

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Liangde XIE ,  Ronald Lee SOUTHER ,  Mark Lawrence HUNT ,  Steven Charles WOODS

IPC: B23K1/00 ,  B23K1/005 ,  B23K1/002

CPC classification number: B23K1/0018 ,  B22F5/04 ,  B22F7/064 ,  B23K1/002 ,  B23K1/005 ,  B23K1/0056 ,  B23K1/008 ,  B23K20/026 ,  B23K2101/001 ,  B23P6/007 ,  F01D5/005 ,  F05D2230/236 ,  F05D2230/237 ,  F05D2230/31 ,  Y10T403/479

Abstract: A hybrid diffusion-brazing process and hybrid diffusion-brazed article are disclosed. The hybrid diffusion-brazing process includes providing a component having a temperature-tolerant region and a temperature-sensitive region, brazing a braze material to the temperature-tolerant region during a localized brazing cycle, then heating the component in a furnace during a diffusion cycle. The brazing and the heating diffusion-braze the braze material to the component, and the localized brazing cycle is performed independent of the diffusion cycle in the hybrid diffusion-brazing process. The hybrid diffusion-brazed article includes a component, and a braze material diffusion-brazed to the component with a filler material. The filler material has a melting temperature that is above a tolerance temperature of the component.

Abstract translation: 公开了混合扩散钎焊工艺和混合扩散钎焊制品。 混合扩散钎焊方法包括提供具有耐温区域和温度敏感区域的部件，在局部钎焊循环期间将钎焊材料钎焊到耐温区域，然后在扩散循环期间加热炉中的组分 。 钎焊和加热扩散 - 将钎焊材料钎焊到部件上，并且在混合扩散钎焊工艺中独立于扩散循环进行局部钎焊循环。 混合扩散钎焊制品包括一种组分，以及用填料材料扩散钎焊到该组件上的钎焊材料。 填充材料具有高于组分的耐受温度的熔化温度。

公开(公告)号：US20150071788A1

公开(公告)日：2015-03-12

申请号：US14023568

申请日：2013-09-11

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Christopher Edward THOMPSON ,  John David WARD ,  James Ryan CONNOR ,  Mark Lawrence HUNT ,  Blake Allen FULTON

IPC: B23P6/04 ,  F01D5/14

CPC classification number: F01D5/14 ,  B23P6/005 ,  F01D5/005 ,  Y10T29/49734

Abstract: A modification process and modified article are disclosed. The modification process includes locating an area in an article, removing the area by machining to form a machined region, inserting a modification material into the machined region, securing the modification material to the article, machining the modification material flush with a geometry of the article, and applying a coating over at least a portion of the article. Another modification process includes locating an area under a suction side leading edge tip shroud fillet of an airfoil, removing the area by machining to form a hole, inserting a modification material having improved material properties as compared to an original base material into the hole, securing the modification material in place, machining the modification material and the airfoil to form a new fillet contour, and applying a coating over at least a portion of the airfoil. Also disclosed is the modified article.

Abstract translation: 公开了修改过程和修改的文章。 修改过程包括将制品中的区域定位，通过机加工去除区域以形成机加工区域，将改性材料插入加工区域，将改性材料固定到制品上，用制品的几何形状加工改性材料 ，并且在所述制品的至少一部分上施加涂层。 另一种改进方法包括将机翼的吸力侧前缘尖端护罩圆角下方的区域定位，通过加工去除该区域以形成孔，将与原始基底材料相比具有改善的材料特性的改性材料插入到孔中，固定 所述改性材料就位，加工所述改性材料和所述翼型件以形成新的圆角轮廓，以及在所述翼型的至少一部分上施加涂层。 还公开了修改的文章。

公开(公告)号：US20140193664A1

公开(公告)日：2014-07-10

申请号：US13735342

申请日：2013-01-07

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Christopher Edward THOMPSON ,  John D. WARD, JR. ,  Mark Lawrence HUNT ,  Jonathan Matthew LOMAS ,  Gareth William David LEWIS ,  Michael Anthony DEPALMA, III

IPC: F01D5/28

CPC classification number: F01D5/288 ,  F01D5/005 ,  F05D2230/31 ,  Y10T428/12618

Abstract: Recoating process and recoated turbine blade are disclosed. The recoating process includes providing a coated turbine blade, then removing a portion of the thermal barrier coating system to form a partially-stripped turbine blade, then applying a bond recoat to the stripped region of the partially-stripped turbine blade; and then applying a thermal barrier recoat to the bond recoat to form a recoated turbine blade. The recoated turbine blade comprises the bond coating portion abutting the bond recoat, the thermal barrier coating portion abutting the thermal barrier recoat, and the stepped configuration. The coated turbine blade has a thermal barrier coating system positioned on a substrate. The partially-stripped turbine blade has a stripped region, a bond coating portion, a thermal barrier coating portion, and a stepped configuration.

Abstract translation: 公开了再循环工艺和重新涂覆的涡轮叶片。 重涂过程包括提供涂覆的涡轮叶片，然后移除热障涂层系统的一部分以形成部分剥离的涡轮叶片，然后将粘合重涂施加到部分剥离的涡轮叶片的剥离区域; 然后将热屏蔽涂层施加到粘结重涂层以形成重新涂覆的涡轮叶片。 重新包覆的涡轮机叶片包括邻接粘结重涂的粘合涂层部分，邻接热障涂层的热障涂层部分和阶梯状构造。 涂覆的涡轮叶片具有定位在基底上的热障涂层系统。 部分剥离的涡轮叶片具有剥离区域，粘合涂覆部分，热障涂层部分和阶梯构造。