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公开(公告)号：US09849528B2
公开(公告)日：2017-12-26
申请号：US14854476
申请日：2015-09-15
摘要： An electrical discharge machining (EDM) system according to embodiments includes: a guide structure; a plurality of electrode devices positioned at least partially within the guide structure, the plurality of electrode devices aligned to provide a plurality of electrical discharges to a workpiece, each of the plurality of electrode devices including: an electrode for positioning proximate the workpiece; an electrode holder coupled to the electrode for holding the electrode proximate the workpiece; and a driver coupled to the electrode holder, the driver adapted to modify a position of the electrode holder and the electrode; and a control system operably connected with the driver, the control system configured to provide instructions to the driver of at least one of the plurality of electrode devices to modify a position of the at least one of the plurality of electrodes independently of at least one other one of the plurality of electrodes.
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公开(公告)号：US09468991B2
公开(公告)日：2016-10-18
申请号：US14164539
申请日：2014-01-27
CPC分类号： B23K26/03 , B23K26/032 , B23K26/0622 , B23K26/146 , B23K26/16 , B23K26/388 , B23K26/389 , B23K26/40 , B23K2101/001 , B23K2101/34 , B23K2103/08 , B23K2103/50
摘要： The present disclosure provides a method for determining a hole completing in laser drilling of a hole in a near wall of an airfoil. The method includes drilling a hole in the near wall of the airfoil using a laser drill. The laser drill may move in a pattern relative to the airfoil. The method also includes determining when the drilling of the hole is complete based on a calculated time duration between successive breakthroughs of a laser from the laser drill through the near wall of the airfoil, or based on a calculated time duration since the latest breakthrough of the laser from the laser drill through the near wall of the airfoil.
摘要翻译： 本公开提供了一种用于确定在翼型件的近壁中的孔的激光钻孔中完成孔的方法。 该方法包括使用激光钻孔在翼型件的近壁处钻孔。 激光钻可以以相对于翼型的图案移动。 该方法还包括基于来自激光钻头的激光在机翼的近壁之间的连续穿透之间的计算的持续时间来确定孔的钻孔何时完成，或者基于从最近的突破之后计算的持续时间 来自激光钻头的激光穿过机翼的近壁。
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公开(公告)号：US09962792B2
公开(公告)日：2018-05-08
申请号：US14626955
申请日：2015-02-20
发明人： Zhaoli Hu , Abe Denis Darling , Shamgar Elijah McDowell , Douglas Anthony Serieno , Jonathan Matthew Lomas
IPC分类号： B23K26/00 , B21K25/00 , B23K26/382 , B23K26/08 , B23K26/14 , B23K26/40 , F01D5/00 , B23K26/042 , B23K26/03 , F01D5/14 , B23K101/00
CPC分类号： B23K26/382 , B23K26/032 , B23K26/042 , B23K26/0876 , B23K26/14 , B23K26/389 , B23K26/40 , B23K2101/001 , F01D5/005 , F01D5/147 , F05D2230/13 , Y02T50/673
摘要： A method for repairing one or more holes in a near wall of a component is provided. The method includes determining updated hole information, including an updated location, of a first hole in the near wall of the component. The method also includes directing a confined laser beam of the confined laser drill towards the near wall of the component at the updated location of the first hole to drill through a coating of the component extending over and/or positioned in the first hole. The method also includes sensing a characteristic of light reflected from the updated location of the first hole and determining the confined laser beam of the confined laser drill has drilled through a portion of the coating of the component extending over and/or positioned in the first hole based on the sensed characteristic of light.
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公开(公告)号：US20160214208A1
公开(公告)日：2016-07-28
申请号：US14602324
申请日：2015-01-22
IPC分类号： B23K26/146 , B23K26/38 , F01D5/18
CPC分类号： B23K26/146 , B23K26/38 , B23K2101/001 , B23P2700/06 , F01D5/187 , F05D2230/13 , F05D2260/20 , F05D2260/202
摘要： A system for forming a passage in an airfoil includes a liquid-jet guided laser that generates a laser beam confined within a fluid column, and a purge medium supply that is fluidly coupled to an aperture of the airfoil. A purge medium flows from the purge medium supply in a flow direction that is substantially parallel to an inner surface of the inner cavity. A controller is configured to direct the liquid-jet guided laser to cut a first passage through the outer surface. A centerline of the passage forms an acute angle with respect to the purge medium flow direction. The first passage is formed at a first radial position that is radially distal to the aperture. A method for forming passages in an airfoil using the system described herein is also disclosed.
摘要翻译： 用于在翼型件中形成通道的系统包括产生限制在流体柱内的激光束的液体喷射引导激光器和流体地联接到翼型孔的吹扫介质供应。 吹扫介质从基本上平行于内腔的内表面的流动方向从吹扫介质供给流动。 控制器构造成引导液体喷射引导激光器切割穿过外表面的第一通道。 通道的中心线相对于吹扫介质流动方向形成锐角。 第一通道形成在径向远离孔的第一径向位置处。 还公开了使用本文所述的系统在翼型件中形成通道的方法。
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公开(公告)号：US20160199942A1
公开(公告)日：2016-07-14
申请号：US14592232
申请日：2015-01-08
CPC分类号： B23K26/032 , B23K26/146 , B23K26/389 , F01D5/186 , F05D2230/13 , F05D2260/202
摘要： A method for drilling a hole in a component is provided. The method includes directing a confined laser beam of a confined laser drill towards a near wall of the component and sensing a first characteristic of light from the hole in the near wall of the component with a first sensor positioned outside the component. The method also includes sensing a second characteristic of light from the hole in the near wall the component with a second sensor. The second characteristic of light is different from the first characteristic of light. Additionally, the method includes determining a hole progress based on the sensed first characteristic of light and the sensed second characteristic of light.
摘要翻译： 提供了一种用于在组件中钻孔的方法。 该方法包括将受限激光钻的受限激光束引向部件的近壁，并且利用位于部件外部的第一传感器感测来自组件的近壁中的孔的光的第一特性。 该方法还包括利用第二传感器感测来自近壁中的孔的光的第二特性。 光的第二特性与光的第一特性不同。 另外，该方法包括基于感测的光的第一特性和感测到的光的第二特性来确定孔进展。
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公开(公告)号：US20160138405A1
公开(公告)日：2016-05-19
申请号：US14546357
申请日：2014-11-18
IPC分类号： F01D5/18 , B23K26/384
CPC分类号： B23K26/389 , B23K26/142 , B23K2101/001 , F05D2230/13
摘要： A system for forming a cooling hole in an airfoil includes a liquid-jet guided laser. The liquid-jet guided laser generates a laser beam confined within a fluid column. The fluid column/laser beam is directed at an outer surface of the airfoil. The system also includes a purge medium supply that is fluidly coupled to an aperture of the airfoil. The purge medium supply provides a purge medium into an inner cavity of the airfoil. The purge medium flow is oriented to flow in a flow direction that is substantially parallel to an inner surface of the cavity. A cooling hole is formed in the airfoil and extends through the outer surface and penetrates the inner surface of the cavity. A centerline of the cooling hole forms an acute angle with respect to the purge medium flow direction. The system described herein provides a method for manufacturing an airfoil.
摘要翻译： 用于在翼型件中形成冷却孔的系统包括液体喷射引导激光器。 液体喷射引导激光器产生限制在流体柱内的激光束。 流体柱/激光束指向翼型件的外表面。 该系统还包括流体耦合到翼型的孔的清洗介质供应。 吹扫介质供应器将吹扫介质提供到翼型件的内腔中。 吹扫介质流被定向成在基本上平行于空腔的内表面的流动方向上流动。 在翼型件中形成冷却孔，并且延伸穿过外表面并穿过腔体的内表面。 冷却孔的中心线相对于吹扫介质流动方向形成锐角。 本文所述的系统提供了一种制造翼型的方法。
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公开(公告)号：US10589385B2
公开(公告)日：2020-03-17
申请号：US14592217
申请日：2015-01-08
IPC分类号： B23K26/70 , B23K26/146 , B23K26/40 , B23K26/382 , B23K26/03 , B23K26/0622 , B23K26/402 , F01D5/18 , B23K103/16 , B23K101/00 , B23K103/18
摘要： A method for drilling a hole in a component is provided. The method includes directing a confined laser beam of the confined laser drill towards a near wall of the component and sensing a characteristic of light directed along a beam axis of the confined laser beam away from the component with a sensor. The method also includes determining one or more operational conditions based on the characteristic of the light sensed with the sensor. The one or more operational conditions includes at least one of a depth of the hole being drilled by the confined laser drill and a material into which the confined laser beam of the confined laser drill is being directed. Such a method may allow for more appropriate control of the confined laser drill.
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公开(公告)号：US20170320163A1
公开(公告)日：2017-11-09
申请号：US15145053
申请日：2016-05-03
IPC分类号： B23K26/00 , B23K26/146 , B23H1/00 , B23H1/04
CPC分类号： B23K26/0093 , B23H1/00 , B23H1/04 , B23H5/00 , B23H9/14 , B23K26/146
摘要： This disclosure provides a system, method, and resulting workpiece combining liquid guided laser and electrical discharge machining to create a common feature. The workpiece is positioned in a liquid guided laser cutting path and machined by the liquid guided laser device to create an intermediate feature in the workpiece. The work piece is then positioned in an electrical discharge machining (EDM) device so that an electrode of the EDM device is operatively positioned proximate the intermediate feature and machined using the EDM device to modify the intermediate feature in the workpiece to create the finished common feature in the workpiece.
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公开(公告)号：US09662743B2
公开(公告)日：2017-05-30
申请号：US14164506
申请日：2014-01-27
IPC分类号： B23K26/00 , B23K26/04 , B23K26/03 , B23K26/388 , B23K26/146 , B23K26/382 , B23K101/00 , B23K103/16
CPC分类号： B23K26/03 , B23K26/0006 , B23K26/146 , B23K26/388 , B23K26/389 , B23K2101/001 , B23K2103/172
摘要： A method for manufacturing an airfoil is provided, the method including drilling a hole in a near wall of the airfoil using a laser drill and activating a back strike protection in a cavity of the airfoil. The method additionally includes detecting a breakthrough of a laser from the laser drill through the near wall of the airfoil and subsequently initiating a drilling subroutine, with the drilling subroutine including a continued operation of the laser drill. Such a method may provide for an improved hole, such as a cooling passage, in the airfoil.
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公开(公告)号：US20170072487A1
公开(公告)日：2017-03-16
申请号：US14854476
申请日：2015-09-15
摘要： An electrical discharge machining (EDM) system according to embodiments includes: a guide structure; a plurality of electrode devices positioned at least partially within the guide structure, the plurality of electrode devices aligned to provide a plurality of electrical discharges to a workpiece, each of the plurality of electrode devices including: an electrode for positioning proximate the workpiece; an electrode holder coupled to the electrode for holding the electrode proximate the workpiece; and a driver coupled to the electrode holder, the driver adapted to modify a position of the electrode holder and the electrode; and a control system operably connected with the driver, the control system configured to provide instructions to the driver of at least one of the plurality of electrode devices to modify a position of the at least one of the plurality of electrodes independently of at least one other one of the plurality of electrodes.
摘要翻译： 根据实施例的放电加工（EDM）系统包括：导向结构; 多个电极装置，其至少部分地定位在所述引导结构内，所述多个电极装置对准以向工件提供多个放电，所述多个电极装置中的每一个包括：用于在所述工件附近定位的电极; 耦合到所述电极用于将所述电极保持靠近所述工件的电极保持器; 以及耦合到所述电极保持器的驱动器，所述驱动器适于修改所述电极保持器和所述电极的位置; 以及与所述驱动器可操作地连接的控制系统，所述控制系统被配置为向所述驱动器提供所述多个电极装置中的至少一个的指令，以独立于至少一个其他电极来修改所述多个电极中的所述至少一个的所述至少一个的位置 多个电极中的一个。
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