公开(公告)号：WO1997015407A1

公开(公告)日：1997-05-01

申请号：PCT/US1996016746

申请日：1996-10-18

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  BUONGIORNO, Angelo

IPC: B08B09/093

CPC classification number: F01D25/002 ,  B08B3/02 ,  B08B9/00 ,  B08B2230/01 ,  F05D2260/607

Abstract: A process and apparatus is provided for cleaning deposits (9) from gas turbine engine components, particularly turbine blades (1), by locating or drilling a hole into the cavity of the component, inserting a cleaning tube (7) into the cavity and cleaning the deposits (9) from the cavity with a cleaning material inserted into the cavity through the tube (7), followed by sealing any hole drilled in the component.

Abstract translation: 提供了一种工艺和设备，用于通过在组件的空腔中定位或钻孔，将燃气涡轮发动机部件，特别是涡轮叶片（1）清除沉积物（9），将清洁管（7）插入腔体和清洁 来自腔体的沉积物（9）具有通过管（7）插入空腔中的清洁材料，随后密封在部件中钻出的任何孔。

公开(公告)号：WO1998026158A1

公开(公告)日：1998-06-18

申请号：PCT/IB1997001645

申请日：1997-12-05

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  WOLFLA, Thomas, A. ,  FERGUSON, James, J.

IPC: F01D05/14

CPC classification number: F16J15/445 ,  B23K26/40 ,  B23K2103/02 ,  B23K2103/08 ,  B23K2103/10 ,  B23K2103/14 ,  B23K2103/26 ,  B23K2103/50 ,  C23C4/18 ,  C23C30/00 ,  F01D11/122 ,  F04D29/164 ,  F05D2230/13 ,  F05D2230/90 ,  Y02T50/672

Abstract: An abradable seal is provided utilizing a laser to cut a pattern into the surface effective to improve abradability in the area of the pattern.

Abstract translation: 利用激光器将可磨损密封件切割成表面，有效地改善图案区域的磨损性。

公开(公告)号：WO1994023890A1

公开(公告)日：1994-10-27

申请号：PCT/US1994004263

申请日：1994-04-20

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  TEETS, J., Michael ,  BURNHAM, Douglas, R.

IPC: B23P15/00

CPC classification number: B21D53/78 ,  B21K3/04 ,  B23P15/04 ,  F01D5/288 ,  F04D29/324 ,  F05D2240/303 ,  Y10T29/49336 ,  Y10T29/49341

Abstract: A process is provided for forming a metallic edge (1) having a three dimensional internal configuration by preparing a metallic edge blank having a two dimensional internal configuration; attaching a flange (7) to the sides (3) of the blank; preheating the blank, forming mandrel (a) and receiver dies (11) to a temperature at which the metal is in a malleable state, with the forming mandrel (a) having an external surface which corresponds to the three dimensional internal configuration of the formed metallic edge; and hot forming the metallic edge (1) by securing the blank within the receiver dies (11) and advancing the mandrel into the inner cavity of the blank through use of a drive means which rotates the mandrel as it advances into the blank while maintaining the blank, mandrel (9) and receiver dies (11) at the malleable temperature.

Abstract translation: 提供一种通过制备具有二维内部构造的金属边缘坯料来形成具有三维内部构造的金属边缘（1）的工艺; 将凸缘（7）附接到坯料的侧面（3）; 预热坯料，将芯棒（a）和接收器模具（11）成形到金属处于可延展状态的温度，成型心轴（a）具有对应于所形成的三维内部构造的外表面 金属边缘 以及通过将所述坯件固定在所述接收器模具（11）内并使所述心轴进入所述坯料的内腔中而使所述金属边缘（1）热成型，所述驱动装置使得所述心轴在进入所述坯料时旋转，同时保持所述 空白，心轴（9）和接收器模具（11）。

公开(公告)号：WO1995030512A1

公开(公告)日：1995-11-16

申请号：PCT/US1995003388

申请日：1995-03-20

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  GOODWATER, Frank ,  HUYNH, Lang ,  KANG, David

IPC: B23P15/00

CPC classification number: B23K1/0018 ,  B23K1/018 ,  B23K2101/001 ,  B23P6/002 ,  B23P11/025 ,  Y10T29/49318 ,  Y10T29/49336 ,  Y10T29/53096

Abstract: A process and apparatus are provided for separating components of a brazed vane assembly (1) by preheating the assembly to a temperature below the solidus of the base metal of the vane assembly and above the liquids of the braze, then maintaining such temperature while separating the airfoil (23) from the platform (45) by pulling/pushing the airfoil (23) and platform apart (45).

Abstract translation: 提供了一种工艺和设备，用于通过将组件预热到低于叶片组件的基底金属的固相线的温度并在钎焊液的上方分离钎焊叶片组件（1）的部件，然后在分离 通过拉动/推动翼型件（23）和平台（45），从平台（45）获得翼型件（23）。

公开(公告)号：WO1998013585A1

公开(公告)日：1998-04-02

申请号：PCT/US1997013851

申请日：1997-08-06

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  WEISS, Carl

IPC: F01D09/04

CPC classification number: B23P6/005 ,  F01D9/042 ,  F05D2230/80 ,  Y02T50/672 ,  Y10T29/49318 ,  Y10T29/49323

Abstract: Field replacement of a damaged outlet guide vane in a turbofan engine is facilitated by utilizing a replacement vane assembly (30) that includes an elongated replacement vane (31) having a first inner (32) and a second outer (33) mounting platform mounted at opposite ends of the vane. The first mounting platform is fixedly secured to the inner end of the vane and second mounting platform is mounted so as to be movable from the outer end of the vane toward the inner end thereof. By moving the outer mounting platform toward the inner end of the vane, it is easier to maneuver the vane in a confined space and facilitate entry of the outer platform over the lip of and into the outer annular casing groove (61) that retains the replacement vane.

Abstract translation: 通过利用替换叶片组件（30）来促进涡轮风扇发动机中损坏的出口导向叶片的现场更换，该替换叶片组件（30）包括具有第一内部（32）和第二外部（33）安装平台的细长的替换叶片（31） 叶片的两端。 第一安装平台固定在叶片的内端，第二安装平台被安装成可从叶片的外端向其内端移动。 通过将外部安装平台移动到叶片的内端，更容易在密闭的空间中操纵叶片，并且便于外部平台进入外部环形壳体凹槽（61）的唇缘，从而保持更换 叶片。

公开(公告)号：WO1996022842A1

公开(公告)日：1996-08-01

申请号：PCT/US1995016754

申请日：1995-12-21

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  HINSON, David

IPC: B05D05/02

CPC classification number: H05K3/383 ,  C23F1/02 ,  C23F1/26 ,  H05K2201/0116 ,  H05K2201/0166 ,  H05K2201/0373 ,  H05K2203/0769

Abstract: A process for roughening a metal surface is provided comprising applying a coating to the metal surface wherein the coating is a temporary barrier to an etchant attacking the metal surface and the coating is susceptible to the etchant gradually removing the coating, and then etching the coated metal surface with an aqueous bath containing the etchant effective to produce a roughened metal surface.

Abstract translation: 提供了一种使金属表面粗糙化的方法，包括将涂层涂覆到金属表面上，其中涂层是临时阻挡侵蚀金属表面的蚀刻剂，并且涂层易于蚀刻剂逐渐去除涂层，然后蚀刻涂覆的金属 具有含有蚀刻剂的水浴的表面有效地产生粗糙的金属表面。

公开(公告)号：WO1995020458A1

公开(公告)日：1995-08-03

申请号：PCT/US1994014063

申请日：1994-12-08

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  BUONGIORNO, Angelo

IPC: B23K26/14

CPC classification number: B23K26/144

Abstract: A laser powdered metal cladding apparatus (10) includes a removable conical nozzle (15) having a central opening (23) through which the laser beam and powdered metal exit the apparatus. The opening (23) extends to the front surface (53) of the nozzle that is in close proximity to the workpiece (25). Axial passageways (51) in the tapered wall of the nozzle extend rearward from the front surface (53) and are arranged in an array that is centered around the opening (23). Inert gas flows through these axial passageways (51) to cool the nozzle and to form an oxidation shield at the puddle of liquid metal (26). Water or other cooling fluid is circulated through a water jacket (40) between apertures (41) to cool the apparatus (10). Powdered metal for cladding is delivered to a conical passage (35) at its inlets (36), and exits through the opening (23).

Abstract translation: 激光粉末金属包层设备（10）包括具有中心开口（23）的可移除的锥形喷嘴（15），激光束和粉末金属通过该中心开口离开设备。 开口（23）延伸到紧邻工件（25）的喷嘴的前表面（53）。 喷嘴的锥形壁中的轴向通道（51）从前表面（53）向后延伸并且以围绕开口（23）为中心的阵列布置。 惰性气体流过这些轴向通道（51）以冷却喷嘴并在液态金属（26）的熔池处形成氧化屏蔽。 水或其它冷却流体通过孔（41）之间的水套（40）循环以冷却装置（10）。 用于包层的粉状金属在其入口（36）处被输送到锥形通道（35），并且通过开口（23）离开。

公开(公告)号：WO1995006540A1

公开(公告)日：1995-03-09

申请号：PCT/US1994009933

申请日：1994-08-31

Applicant: CHROMALLOY GAS TURBINE CORPORATION

Inventor： CHROMALLOY GAS TURBINE CORPORATION ,  GOODWATER, Frank ,  HUYNH, Lang ,  KANG, David ,  LI, Hon ,  LIZOTTE, James ,  DOYLE, Brian

IPC: B23K26/00

CPC classification number: B23K26/034 ,  B23K26/123 ,  B23K26/32 ,  B23K26/60 ,  B23K2101/001 ,  B23K2103/26 ,  F05B2220/302

Abstract: A process is provided for laser welding a superalloy article (20) by preheating the entire weld area and region adjacent to the weld area of the article to a ductile temperature within the range of 1400-2100 degrees F with an induction heat coil (14) and maintaining such temperature during welding and solidification of the weld; and welding the preheated article using a laser (11) with a powder alloy feed (12), with a control system which controls the laser powder feed (12) and a motion system on which the article is fixtured, wherein the control system includes a vision system which digitizes the weld area of the article (20) providing a path for the laser to follow.

Abstract translation: 提供了一种用于通过用感应加热线圈（14）预热整个焊接区域和与焊接区域相邻的区域到1400-2100°F范围内的延展性温度来激光焊接超级合金制品（20）的工艺， 并在焊接和凝固期间保持这种温度; 以及使用激光器（11）与粉末合金进料（12）焊接预热制品，其中控制系统控制激光粉末进料（12）和其上固定有物品的运动系统，其中控制系统包括： 数字化物品（20）的焊接区域的视觉系统，提供激光跟随的路径。