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1. 发明公开

EP2857178A1 Method for 3-D printing a pattern for the surface of a turbine shroud 有权转让
标题翻译： Verfahren zum 3D-Drucken eines ModellfürdieOberflächeeines Turbinendeckbands
公开(公告)号：EP2857178A1
公开(公告)日：2015-04-08
申请号：EP14185563.5
申请日：2014-09-19
申请人： General Electric Company
发明人： Bucci, David Vincent , Kottilingam, Srikanth Chandrudu , Singh, Prabhjot
IPC分类号： B29C67/00 , B28B1/00 , F01D5/20
CPC分类号： B28B1/001 , B05D5/00 , B28B17/02 , B29C64/00 , B29C64/165 , B33Y10/00 , F01D5/20 , F01D11/125 , F05D2230/30 , F05D2230/50 , F05D2230/60 , F05D2230/90 , F05D2250/18 , F05D2250/181
摘要： A method (900) of making an article of manufacture is provided and includes the steps of (910) spraying a first coating onto a substrate, and (920) depositing a second coating on the first coating by 3-D printing a material disposed in a pattern. The pattern includes ridges (16) disposed at a base surface (20) of a turbine part. Each ridge (16) defined by first (30) and second (32) sidewalls, each sidewall (30,32) having a first (31) and second (33) end. The ends (30,33) extend from the base surface (20), the sidewalls (30,32) slope toward each other until meeting at second ends (33) of respective first (30) and second (32) sidewalls defining a centerline (22) and a top portion (34) of the ridge (16). The sidewalls (30,32) are inclined with substantially equal but opposite slopes with respect to the base surface (20). The ridges (16) correspond to a back portion (11) of a turbine bucket and are oriented at a first angle (48) with respect to an axis of rotation of the bucket.
摘要翻译：提供了制造制品的方法（900），并且包括以下步骤：（910）将第一涂层喷涂到基材上，和（920）通过3D印刷在第一涂层上沉积第二涂层的材料一种模式。该图案包括设置在涡轮部分的基面（20）处的脊（16）。每个脊（16）由第一（30）和第二（32）侧壁限定，每个侧壁（30,32）具有第一（31）和第二（33）端。端部（30,33）从基面（20）延伸，侧壁（30,32）朝向彼此倾斜，直到在相应的第一（30）和第二（32）侧壁的第二端（33）处会聚，（22）和所述脊（16）的顶部（34）。侧壁（30,32）相对于基面（20）具有大致相等但相对的倾斜倾斜。脊（16）对应于涡轮机叶片的后部（11）并且相对于铲斗的旋转轴线以第一角度（48）定向。

2. 发明授权

EP2366476B1 Method for Fabricating Turbine Airfoils and Tip Structures Therefor 无效
标题翻译：一种用于制造涡轮机叶片和尖端结构的过程
公开(公告)号：EP2366476B1
公开(公告)日：2014-07-02
申请号：EP10156136.3
申请日：2010-03-10
申请人： General Electric Company
发明人： Qi, Huan , Singh, Prabhjot , Desander, Donald Brett , Azer, Magdi Naim , Tewari, Sudhir Kumar , Gledhill, Mark Douglas , Sabato, Joseph Giancarlo , Rockstroh, Todd Jay
IPC分类号： B22F3/105 , B22F7/06
CPC分类号： B22F3/1055 , B22C9/04 , B22F7/062 , B22F2007/068 , Y02P10/292 , Y02P10/295
摘要： A method for making a turbine airfoil (18) includes providing a mold core (40) and an outer shell (42) which cooperatively define a cavity in the shape of a hollow airfoil (18) having an outer wall, a root, and a tip. A tip portion of the core (40) extends completely through the portion of the cavity defining the tip of the airfoil (18). The core (40) is restrained to prevent movement between the core (40) and outer shell (42). Molten metal is introduced into the cavity and solidified to form an airfoil (18) having at least one outer wall which defines an open tip and a hollow interior. A metallic tip cap is formed on the outer wall which substantially closes off the open tip. The tip cap may be formed by packing the airfoil (18) with metallic powder; and laser sintering the exposed powder so as to form a tip cap which is metallurgically bonded to the outer wall.

3. 发明授权

EP1952932B1 LASER NET SHAPE MANUFACTURING USING AN ADAPTIVE TOOLPATH DEPOSITION METHOD 有权
公开(公告)号：EP1952932B1
公开(公告)日：2019-04-24
申请号：EP08100850.0
申请日：2008-01-24
申请人： GENERAL ELECTRIC COMPANY
发明人： Qi, Huan , Singh, Prabhjot , Azer, Magdi Naim
IPC分类号： B22F3/105 , B22F5/04 , B23K35/30 , B23K35/32 , B23P6/00 , B23K35/02 , B23K26/342 , B23K101/00 , C23C24/10

4. 发明公开

EP2469258A2 Method And System For Online Creep Monitoring 审中-公开
标题翻译： Verfahren und System zur Online-Kriechüberwachung
公开(公告)号：EP2469258A2
公开(公告)日：2012-06-27
申请号：EP11193135.8
申请日：2011-12-13
申请人： General Electric Company
发明人： Nieters, Edward James , Ruud, James Anthony , Harding, Kevin George , Hasz, Wayne Charles , Aandarawis, Emad Andarawis , Batzinger, Thomas James , Nirmalan, Nirm Velumylum , Singh, Prabhjot , Wang, Guanghua
IPC分类号： G01M15/05
CPC分类号： G01M5/0016
摘要： A creep monitoring system (100) is provided. The system includes a creep sensor assembly (116) formed onto a surface of an object (114) rotatable about an axis, the creep sensor assembly including an image pattern (300), an optical monitoring system with line of sight to the creep sensor assembly, the optical monitoring system configured to collect information from the creep sensor assembly, a processor (110) programmed to receive the information, and determine at least one of an amount of creep (124) of the object.
摘要翻译：提供了一种蠕变监测系统（100）。所述系统包括形成在可围绕轴线旋转的物体（114）的表面上的蠕变传感器组件（116），所述蠕变传感器组件包括图像图案（300），具有到所述蠕变传感器组件的视线的光学监控系统，所述光学监视系统被配置为从所述蠕变传感器组件收集信息，被编程为接收所述信息的处理器（110）以及确定所述对象的蠕变量（124）中的至少一个。

5. 发明公开

EP2366476A1 Method for Fabricating Turbine Airfoils and Tip Structures Therefor 无效
标题翻译： Verfahren zur Herstellung von Turbinenschaufeln und Spitzenstrukturendafür
公开(公告)号：EP2366476A1
公开(公告)日：2011-09-21
申请号：EP10156136.3
申请日：2010-03-10
申请人： General Electric Company
发明人： Qi, Huan , Singh, Prabhjot , Desander, Donald Brett , Azer, Magdi Naim , Tewari, Sudhir Kumar , Gledhill, Mark Douglas , Sabato, Joseph Giancarlo , Rockstroh, Todd Jay
IPC分类号： B22F3/105 , B22F7/06
CPC分类号： B22F3/1055 , B22C9/04 , B22F7/062 , B22F2007/068 , Y02P10/292 , Y02P10/295
摘要： A method for making a turbine airfoil (18) includes providing a mold core (40) and an outer shell (42) which cooperatively define a cavity in the shape of a hollow airfoil (18) having an outer wall, a root, and a tip. A tip portion of the core (40) extends completely through the portion of the cavity defining the tip of the airfoil (18). The core (40) is restrained to prevent movement between the core (40) and outer shell (42). Molten metal is introduced into the cavity and solidified to form an airfoil (18) having at least one outer wall which defines an open tip and a hollow interior. A metallic tip cap is formed on the outer wall which substantially closes off the open tip. The tip cap may be formed by packing the airfoil (18) with metallic powder; and laser sintering the exposed powder so as to form a tip cap which is metallurgically bonded to the outer wall.
摘要翻译：一种用于制造涡轮机翼（18）的方法包括提供模芯（40）和外壳（42），所述模芯和外壳（42）协同地限定了具有外壁，根部和中空翼型件小费。芯部（40）的尖端部分完全延伸穿过限定翼型件（18）尖端的空腔部分。芯（40）被限制以防止芯（40）和外壳（42）之间的移动。将熔融金属引入空腔中并固化以形成具有至少一个限定开口尖端和中空内部的外壁的翼型件（18）。金属顶盖形成在外壁上，基本封闭开口尖端。顶盖可以通过用金属粉末包装机翼（18）而形成; 并激光烧结暴露的粉末，以形成冶金结合到外壁的尖端盖。

6. 发明授权

EP2857178B1 Method for 3-D printing a pattern for the surface of a turbine shroud 有权转让
公开(公告)号：EP2857178B1
公开(公告)日：2019-06-05
申请号：EP14185563.5
申请日：2014-09-19
申请人： General Electric Company
发明人： Bucci, David Vincent , Kottilingam, Srikanth Chandrudu , Singh, Prabhjot
IPC分类号： B29C67/00 , B28B1/00 , F01D5/20

7. 发明公开

EP2535511A3 Apparatus and method for servicing dynamolectric machine components in-situ 审中-公开
标题翻译：用于现场维修电动机器部件的设备和方法
公开(公告)号：EP2535511A3
公开(公告)日：2017-05-31
申请号：EP12171699.7
申请日：2012-06-12
申请人： General Electric Company
发明人： Zhang, Zhipeng , Shoemaker, Philip Alexander , Pieciuk, Robert Jeffrey , Griffin, Weston Blaine , Rangarajan, Arvind , Quinones, Diego , Singh, Prabhjot
IPC分类号： F01D5/00 , F01D25/28 , B23P6/00
CPC分类号： F01D5/005 , B23P6/02 , F01D25/285 , F05D2230/80
摘要： An apparatus and method are provided for servicing a dynamoelectric machine. The apparatus includes a tool delivery mechanism adapted for delivering a tool (560) to a desired location in the dynamoelectric machine, and a tool support fixture (700) adapted to be secured onto the body of the dynamoelectric machine, where the tool support fixture (700) can be used for supporting and adjusting the tool delivery mechanism. A sleeve mechanism (710) is attached to the tool support fixture (700), and the sleeve mechanism (710) is disposed around a portion of the tool delivery mechanism. The apparatus is adapted to service the component of the dynamoelectric machine in-situ.
摘要翻译：提供了一种用于维修电动机器的设备和方法。该设备包括适于将工具（560）传送到电动机器中的期望位置的工具传送机构以及适于被固定到电动机器的主体上的工具支撑夹具（700），其中工具支撑夹具（ 700）可用于支撑和调整工具传送机构。套筒机构（710）附接到工具支撑固定件（700），并且套筒机构（710）围绕工具递送机构的一部分设置。该设备适用于原位维修电动机器的部件。

8. 发明公开

EP2535511A2 Apparatus and method for servicing dynamolectric machine components in-situ 审中-公开
标题翻译：装置和方法用于原位维修电动机组件的
公开(公告)号：EP2535511A2
公开(公告)日：2012-12-19
申请号：EP12171699.7
申请日：2012-06-12
申请人： General Electric Company
发明人： Zhang, Zhipeng , Shoemaker, Philip Alexander , Pieciuk, Robert Jeffrey , Griffin, Weston Blaine , Rangarajan, Arvind , Quinones, Diego , Singh, Prabhjot
IPC分类号： F01D5/00 , F01D25/28
CPC分类号： F01D5/005 , B23P6/02 , F01D25/285 , F05D2230/80
摘要： An apparatus and method are provided for servicing a dynamoelectric machine. The apparatus includes a tool delivery mechanism adapted for delivering a tool (560) to a desired location in the dynamoelectric machine, and a tool support fixture (700) adapted to be secured onto the body of the dynamoelectric machine, where the tool support fixture (700) can be used for supporting and adjusting the tool delivery mechanism. A sleeve mechanism (710) is attached to the tool support fixture (700), and the sleeve mechanism (710) is disposed around a portion of the tool delivery mechanism. The apparatus is adapted to service the component of the dynamoelectric machine in-situ.

9. 发明公开

EP1952932A3 Laser net shape manufacturing using an adaptive toolpath deposition method 有权
标题翻译： Laserendformherstellung自适应工具路径沉积工艺
公开(公告)号：EP1952932A3
公开(公告)日：2010-05-26
申请号：EP08100850.0
申请日：2008-01-24
申请人： GENERAL ELECTRIC COMPANY
发明人： Qi, Huan , Singh, Prabhjot , Azer, Magdi Naim
IPC分类号： B23K26/34 , B23K101/00
CPC分类号： F01D5/005 , B22F3/1055 , B22F5/04 , B23K26/342 , B23K35/0244 , B23K35/3033 , B23K35/3046 , B23K35/3053 , B23K35/325 , B23K2101/001 , B23P6/007 , C23C24/106 , F01D5/02 , F01D5/147 , F04D29/388 , F05D2220/30 , F05D2230/31 , F05D2230/80 , Y02P10/295
摘要： A method is disclosed for laser cladding a substrate 3, comprising providing the substrate 3; depositing a first determined variable bead width of a material along a toolpath upon the substrate; depositing a second adjacent determined variable bead width of a material along the toolpath which overlaps the first determined variable bead width of deposited material 7; continuing to deposit a plurality of overlapping predetermined adjacent variable bead widths of a material until a first material layer is complete; forming a second material layer by depositing a plurality of overlapping predetermined variable bead widths of a material on top of the first material layer; and continuing to deposit material layers on top of deposited material layers until the cladding is complete; wherein the variable bead width of the deposited material is controlled by a computer having a plurality of input parameters to maintain an approximately constant percent of bead width overlap.

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