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1. 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.

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

EP1795620B1 Laser shock peening system with time-of-flight monitoring 有权
标题翻译：激光冲击强化系统与航班时刻监控
公开(公告)号：EP1795620B1
公开(公告)日：2010-06-23
申请号：EP06125146.8
申请日：2006-11-30
申请人： GENERAL ELECTRIC COMPANY
发明人： Deaton, John Broddus, Jr. , Azad, Farzin Homayoun , Azer, Magdi Naim , Rockstroh, Todd Jay
IPC分类号： C21D10/00 , F01D5/28 , G01N29/12 , B23K26/00
CPC分类号： C21D10/005 , F01D5/286 , G01N29/12 , G01N2291/0234 , Y02T50/671

4. 发明公开

EP1637616A3 System and method for monitoring laser shock processing 有权
标题翻译：装置和方法用于监测激光震动喷丸处理
公开(公告)号：EP1637616A3
公开(公告)日：2009-03-11
申请号：EP05255498.7
申请日：2005-09-08
申请人： GENERAL ELECTRIC COMPANY
发明人： Pingfan, Peter Wu , Azer, Magdi Naim , Benicewicz, Pamela King
IPC分类号： C21D10/00 , B23K26/00 , G01N21/00
CPC分类号： G01N21/718 , B23K26/00 , B23K26/0066 , B23K26/0069 , B23K26/032 , C21D1/09 , C21D10/00 , C21D10/005 , C21D11/00 , G01J5/60 , G01N21/63
摘要： A method and system (14) for monitoring laser shock peening of a work piece (18). A line spectrum is obtained from radiation emitted by a plasma (32) produced by a laser shock peening process. The shape of the line spectrum about its emission peak is compared to a defined line shape to verify proper operation of the laser shock peening process. The line shape may be a Lorentzian line shape corresponding to a desired line shape. The line shape may a Gaussian line shape corresponding to an undesired line shape. The system (14) can also detect the failure mode that occurs when the opaque layer (22) is broken through by detecting the plasma spectral component produced by the work piece material, along with the plasma produced by the opaque layer.

5. 发明授权

EP1795887B1 Laser shock peening plasma diagnostics sensors for real time process monitoring 有权
标题翻译：激光冲击凝固血浆用于实时过程监控诊断传感器
公开(公告)号：EP1795887B1
公开(公告)日：2011-06-15
申请号：EP06125751.5
申请日：2006-12-08
申请人： GENERAL ELECTRIC COMPANY
发明人： Benicewicz, Pamela King , Azer, Magdi Naim , Deaton, Jr., John Broddus , Wu, Pingfan Peter , Rockstroh, Todd Jay
IPC分类号： G01N21/70 , C21D10/00
CPC分类号： G01N21/718 , B23K26/0069 , B23K26/032

6. 发明公开

EP1795620A1 Laser shock peening system with time-of-flight monitoring 有权
标题翻译： Laserschockstrahlensystem mitFlugzeitüberwachung
公开(公告)号：EP1795620A1
公开(公告)日：2007-06-13
申请号：EP06125146.8
申请日：2006-11-30
申请人： The General Electric Company
发明人： Deaton, John Broddus, Jr. , Azad, Farzin Homayoun , Azer, Magdi Naim , Rockstroh, Todd Jay
IPC分类号： C21D10/00 , F01D5/28 , G01N29/12 , B23K26/00
CPC分类号： C21D10/005 , F01D5/286 , G01N29/12 , G01N2291/0234 , Y02T50/671
摘要： A system (10) and method for monitoring a laser shock peening process includes a sensor (14) connected to a controller (16). The controller (16) includes an input (36, 40) and a processor (38). The input (36, 40) is connected to the sensor (14) to receive a signal indicative of a laser shock event at a workpiece (20). The processor (38) is connected to the input (36, 40) and is configured to determine a time-of-flight (48) of residual energy associated with the laser shock event from the workpiece (20) to the sensor (14) and determine peen quality from the time-of-flight of the residual energy.
摘要翻译：用于监测激光冲击硬化处理的系统（10）和方法包括连接到控制器（16）的传感器（14）。控制器（16）包括输入（36,40）和处理器（38）。输入（36,40）连接到传感器（14）以接收指示工件（20）处的激光冲击事件的信号。处理器（38）连接到输入（36,40），并被配置为确定与从工件（20）到传感器（14）的激光冲击事件相关联的剩余能量的飞行时间（48）并从剩余能量的飞行时间确定喷丸质量。

7. 发明公开

EP1304446A1 Method for replacing a damaged TBC ceramic layer 审中-公开
标题翻译： Methode um einebeschädigteTBC Keramikschicht zu ersetzen
公开(公告)号：EP1304446A1
公开(公告)日：2003-04-23
申请号：EP02255682.3
申请日：2002-08-14
申请人： GENERAL ELECTRIC COMPANY
发明人： Rigney, Joseph David , Azer, Magdi Naim
IPC分类号： F01D5/28 , C23C4/02
CPC分类号： C23C28/321 , C23C4/02 , C23C28/3455 , F01D5/005 , F01D5/288 , F05D2230/13 , F05D2230/80 , F05D2230/90 , F05D2300/611 , Y02T50/67 , Y02T50/673 , Y10T29/49318
摘要： The present invention is a method for repairing a TBC ceramic top coat in local regions that have experienced a mechanical or thermally-induced spallation event leaving the underlying bond coat intact. A novel combination of groove design (i.e. spacing, pattern and depth) and laser-surface incident angles fabricated into the remaining bond coat is used to achieve spallation resistance equal to or greater than baseline after applying and maintaining a TBC ceramic patch to the localized areas of spallation. The method is particularly useful, but not limited to, repair of coating systems comprised of physical vapor deposited (PVD) ceramic top coats. In a preferred embodiment, the method of the present invention comprises (1) cleaning the exposed spalled region, (2) treating a limited portion of the bond coat by a grooving process with two linear arrays of equally spaced grooves intersecting at a preselected angle so as to texture the surface, and (3) depositing a ceramic material on the surface of the spalled / textured portion of the bond layer. The grooving process is accomplished with a high energy beam.
摘要翻译：本发明是一种在局部区域修复TBC陶瓷面漆的方法，其经历机械或热诱导的剥落事件，使得底层粘结涂层完好无损。使用制造到剩余粘结涂层中的槽设计（即间距，图案和深度）和激光表面入射角的新颖组合来实现在将TBC陶瓷贴片应用并保持在局部区域之后等于或大于基线的剥离阻力的剥落。该方法特别有用，但不限于，修复由物理气相沉积（PVD）陶瓷顶涂层组成的涂层体系。在一个优选实施例中，本发明的方法包括（1）清洁暴露的剥落区域，（2）通过切槽工艺处理有限部分的粘结涂层，其中两个线性阵列具有以预选角度相交的等间距凹槽，以便（3）在接合层的剥离/纹理化部分的表面上沉积陶瓷材料。开槽过程是用高能束实现的。

8. 发明授权

EP1637616B1 System and method for monitoring laser shock processing 有权
标题翻译：装置和方法用于监测激光震动喷丸处理
公开(公告)号：EP1637616B1
公开(公告)日：2012-08-15
申请号：EP05255498.7
申请日：2005-09-08
申请人： GENERAL ELECTRIC COMPANY
发明人： Pingfan, Peter Wu , Azer, Magdi Naim , Benicewicz, Pamela King
IPC分类号： B23K26/03 , C21D10/00 , G01N21/71 , B23K26/00
CPC分类号： G01N21/718 , B23K26/00 , B23K26/0066 , B23K26/0069 , B23K26/032 , C21D1/09 , C21D10/00 , C21D10/005 , C21D11/00 , G01J5/60 , G01N21/63

9. 发明公开

EP2015022A1 Profilometry apparatus and method of operation 审中-公开
标题翻译： Profilometrie-Vorrichtung und Betriebsverfahrendafür
公开(公告)号：EP2015022A1
公开(公告)日：2009-01-14
申请号：EP07112216.2
申请日：2007-07-11
申请人： GENERAL ELECTRIC COMPANY
发明人： Hu, Qingying , Azer, Magdi Naim , Harding, Kevin George , Deaton, JR., John Broddus , Tewari, Sudhir Kumar
IPC分类号： G01B11/25
CPC分类号： G01B11/25
摘要： A profilometry apparatus (12) is provided. The profilometry apparatus (12) includes a fringe projection device (32) configured to project a fringe pattern on an object (22) and an optical unit (34) configured to capture an image of a distorted fringe pattern modulated by the object (22). The profilometry apparatus (12) also includes a signal processing unit (60) configured to process the captured image from the optical unit (34) to filter noise from the image and to obtain real-time estimation of parameters associated with manufacture or repair of the object (22).
摘要翻译：提供轮廓测量装置（12）。轮廓测量装置（12）包括边缘投影装置（32），其被配置为将物体（22）上的条纹图案投影和被配置为捕获被物体（22）调制的失真条纹图案的图像的光学单元（34）。轮廓测量装置（12）还包括信号处理单元（60），被配置为处理来自光学单元（34）的捕获图像，以过滤来自图像的噪声，并获得与制造或维修相关的参数的实时估计物体（22）。

10. 发明公开

EP1637616A2 System and method for monitoring laser shock processing 有权
标题翻译： Vorrichtung und Verfahren zurÜberwachungeines Laserschockstrahlprozesses
公开(公告)号：EP1637616A2
公开(公告)日：2006-03-22
申请号：EP05255498.7
申请日：2005-09-08
申请人： GENERAL ELECTRIC COMPANY
发明人： Pingfan, Peter Wu , Azer, Magdi Naim , Benicewicz, Pamela King
IPC分类号： C21D10/00 , B23K26/00
CPC分类号： G01N21/718 , B23K26/00 , B23K26/0066 , B23K26/0069 , B23K26/032 , C21D1/09 , C21D10/00 , C21D10/005 , C21D11/00 , G01J5/60 , G01N21/63
摘要： A method and system (14) for monitoring laser shock peening of a work piece (18). A line spectrum is obtained from radiation emitted by a plasma (32) produced by a laser shock peening process. The shape of the line spectrum about its emission peak is compared to a defined line shape to verify proper operation of the laser shock peening process. The line shape may be a Lorentzian line shape corresponding to a desired line shape. The line shape may a Gaussian line shape corresponding to an undesired line shape. The system (14) can also detect the failure mode that occurs when the opaque layer (22) is broken through by detecting the plasma spectral component produced by the work piece material, along with the plasma produced by the opaque layer.
摘要翻译：一种用于监测工件（18）的激光冲击硬化的方法和系统（14）。由通过激光冲击硬化处理产生的等离子体（32）发射的辐射获得线谱。将其关于其发射峰的线谱的形状与定义的线形状进行比较，以验证激光冲击喷丸处理的正确操作。线形状可以是对应于所需线形状的洛伦兹线形状。线形状可以是对应于不期望的线形状的高斯线形状。系统（14）还可以通过检测由工件材料产生的等离子体光谱分量以及不透明层产生的等离子体来检测当不透明层（22）破裂时发生的故障模式。

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