-
公开(公告)号：US6145194A
公开(公告)日：2000-11-14
申请号：US321703
申请日：1999-05-28
CPC分类号： B23P6/005 , C21D9/50 , F01D5/005 , Y10T29/49318 , Y10T29/49336
摘要： A method for repairing a shrink-fitted turbine disc without removing the disc from the shaft. The method is composed of two basic steps: (1) depositing one or more weld layers in a vicinity of a defective region of the disc using a temperbead welding process and (2) heat treating the disc using an induction heating process. In a first embodiment of the method, the heat treating step includes heating a heat-affected zone of the disc in a vicinity of the one or more weld layers to a temperature T.sub.h, heating a rim region of the disc to a temperature T.sub.r and heating a bore region of the disc to a temperature T.sub.b, where T.sub.h, T.sub.r >T.sub.b. In a second embodiment of the method, the heat treating step includes heating a region of the disc in a vicinity of the one or more weld layers using the induction heating process and concurrently cooling a bore region of the disc. In a third embodiment of the method, the heat treating step includes heating at least a portion of the disc using the induction heating process and concurrently heating the shaft to maintain a predetermined temperature differential between the bore region of the disc and the shaft. In a fourth embodiment of the method, the heat treating step includes heating at least a portion of the disc using the induction heating process and concurrently heating the shaft to maintain a uniform temperature between the bore region of the disc and the shaft.
摘要翻译： 一种用于修复收缩式涡轮盘而不从轴移除盘的方法。 该方法由两个基本步骤组成：（1）使用调温焊接工艺在盘的缺陷区域附近沉积一个或多个焊接层，以及（2）使用感应加热工艺对所述盘进行热处理。 在该方法的第一实施例中，热处理步骤包括将一个或多个焊接层附近的盘的热影响区域加热到温度Th，将盘的边缘区域加热到温度Tr并加热 盘的钻孔区域到达Tb，其中Th，Tr> Tb。 在该方法的第二实施例中，热处理步骤包括使用感应加热过程在一个或多个焊接层附近加热盘的区域，同时冷却盘的孔区域。 在该方法的第三实施例中，热处理步骤包括使用感应加热过程加热盘的至少一部分，同时加热轴以保持盘的孔区域和轴之间的预定温差。 在该方法的第四实施例中，热处理步骤包括使用感应加热过程加热盘的至少一部分，同时加热轴以在盘的孔区域和轴之间保持均匀的温度。
-
公开(公告)号：US20060138093A1
公开(公告)日：2006-06-29
申请号：US11060937
申请日：2005-02-18
CPC分类号： B23K26/206 , B23K9/00 , B23K9/044 , B23K10/00 , B23K15/00 , B23K20/002 , B23K20/021 , B23K26/32 , B23K26/342 , B23K26/60 , B23K2101/001 , B23K2103/18 , B23K2103/26 , B23P6/007 , C22F1/10 , F01D5/005 , F05D2230/232 , F05D2230/30
摘要： A method of repairing a metallic component, such as a superalloy turbine blade or turbine nozzle, includes the step of preparing the component by stripping the protective coatings from the component. The component is then pre-conditioned for welding by a first hot isostatic process. Once the conditioning sequence is complete, the component is welded using any of a number of welding techniques and by adding weld fillers to the weld area. After the welding step, the component is sealed by a second hot isostatic process treatment performed at conditions similar to the first hot isostatic process. The component is finally prepared for re-entry into service.
摘要翻译： 修复诸如超级合金涡轮机叶片或涡轮喷嘴的金属部件的方法包括通过从组件剥离保护涂层来制备组件的步骤。 然后通过第一个热等静压过程对该部件进行预处理以进行焊接。 一旦调理顺序完成，使用多种焊接技术焊接组件，并通过在焊接区域添加焊接填料。 在焊接步骤之后，通过在类似于第一热等静压工艺的条件下进行的第二次热等静压处理来密封部件。 该组件终于准备重新投入使用。
-
3.发明申请Methods for Extending the Life of Alloy Steel Welded Joints by Elimination and Reduction of the HAZ 失效通过消除和减少HAZ来延长合金钢焊接接头寿命的方法公开(公告)号：US20080156402A1
公开(公告)日：2008-07-03
申请号：US12025827
申请日：2008-02-05
CPC分类号： B23K35/004 , B23K35/3033 , B23K35/3066 , B23K2103/05
摘要： In one embodiment, the present invention provides a method for welding together two metal pieces, comprising buttering a surface of a first metal piece with a first nickel-based filler metal at a thickness sufficient to isolate a heat-affected zone in the first metal piece from subsequent welding; heat-treating at least the heat-affected zone in the first metal piece; buttering a surface of a second metal piece with a second nickel-based filler metal having the same composition as the first nickel-based filler metal and at a thickness sufficient to isolate a heat-affected zone in the second metal piece from subsequent welding; heat-treating at least the heat-affected zone in the second metal piece; and welding the heat-treated first buttered surface to the heat-treated second buttered surface with a third nickel-based filler metal having the same composition as the first and second nickel-based filler metals.
摘要翻译： 在一个实施例中，本发明提供了一种用于将两个金属片焊接在一起的方法，包括将第一金属片的表面与第一镍基填充金属进行焊接，其厚度足以隔离第一金属片中的热影响区 从后续焊接; 至少对第一金属片中的热影响区域进行热处理; 用具有与第一镍基填充金属具有相同组成的第二镍基填料金属涂覆第二金属片的表面，并且具有足以将第二金属片中的热影响区隔离以后的焊接的厚度; 至少对第二金属片中的热影响区域进行热处理; 以及与第一和第二镍基填充金属具有相同组成的第三镍基填料金属将经热处理的第一加工表面焊接到经热处理的第二加工表面。
-
公开(公告)号：US06364971B1
公开(公告)日：2002-04-02
申请号：US09487931
申请日：2000-01-20
申请人： Artie Gene Peterson, Jr. , David Wayne Gandy , Gregory Frederick , Jan T. Stover , Ramaswamy Viswanathan
发明人： Artie Gene Peterson, Jr. , David Wayne Gandy , Gregory Frederick , Jan T. Stover , Ramaswamy Viswanathan
IPC分类号： B23K2634
CPC分类号： B23K26/206 , B23K9/00 , B23K9/044 , B23K10/00 , B23K15/00 , B23K20/002 , B23K20/021 , B23K26/32 , B23K26/342 , B23K26/60 , B23K2101/001 , B23K2103/18 , B23K2103/26 , B23P6/007 , C22F1/10 , F01D5/005 , F05D2230/232 , F05D2230/30
摘要： A method of repairing a metallic member, such as a superalloy turbine blade, includes the step of preparing the blade by stripping the protective coatings from the blade. The blade is then pre-conditioned for welding by a first hot isostatic process. Once the blade conditioning sequence is complete, the blade is welded using a laser welding technique and by adding weld fillers to the weld area. After the welding step, the blade is sealed by a second hot isostatic process treatment performed at conditions similar to the first hot isostatic process. The blade is finally prepared for re-entry into service.
摘要翻译： 修复诸如超级合金涡轮机叶片的金属构件的方法包括通过从刀片剥离保护涂层来制备刀片的步骤。 然后通过第一个热等静压过程对刀片进行预处理以进行焊接。 一旦刀片调理顺序完成，刀片将使用激光焊接技术进行焊接，并通过在焊接区域添加焊接填料。 在焊接步骤之后，通过在与第一热等静压过程类似的条件下进行的第二次热等静压处理来对刀片进行密封。 刀片最终准备重新投入使用。
-
5.发明授权Methods for extending the life of alloy steel welded joints by elimination and reduction of the HAZ 失效通过消除和减少HAZ来延长合金钢焊接接头寿命的方法公开(公告)号：US07591410B2
公开(公告)日：2009-09-22
申请号：US12025827
申请日：2008-02-05
IPC分类号： B23K35/24
CPC分类号： B23K35/004 , B23K35/3033 , B23K35/3066 , B23K2103/05
摘要： In one embodiment, the present invention provides a method for welding together two metal pieces, comprising buttering a surface of a first metal piece with a first nickel-based filler metal at a thickness sufficient to isolate a heat-affected zone in the first metal piece from subsequent welding; heat-treating at least the heat-affected zone in the first metal piece; buttering a surface of a second metal piece with a second nickel-based filler metal having the same composition as the first nickel-based filler metal and at a thickness sufficient to isolate a heat-affected zone in the second metal piece from subsequent welding; heat-treating at least the heat-affected zone in the second metal piece; and welding the heat-treated first buttered surface to the heat-treated second buttered surface with a third nickel-based filler metal having the same composition as the first and second nickel-based filler metals.
摘要翻译： 在一个实施例中，本发明提供了一种用于将两个金属片焊接在一起的方法，包括将第一金属片的表面与第一镍基填充金属进行焊接，其厚度足以隔离第一金属片中的热影响区 从后续焊接; 至少对第一金属片中的热影响区域进行热处理; 用具有与第一镍基填充金属具有相同组成的第二镍基填料金属涂覆第二金属片的表面，并且具有足以将第二金属片中的热影响区隔离以后的焊接的厚度; 至少对第二金属片中的热影响区域进行热处理; 以及与第一和第二镍基填充金属具有相同组成的第三镍基填料金属将经热处理的第一加工表面焊接到经热处理的第二加工表面。
-
6.发明授权Methods for extending the life of alloy steel welded joints by elimination and reduction of the HAZ 失效通过消除和减少HAZ来延长合金钢焊接接头寿命的方法公开(公告)号：US07371988B2
公开(公告)日：2008-05-13
申请号：US10972249
申请日：2004-10-22
IPC分类号： B23K9/067
CPC分类号： B23K35/004 , B23K35/3033 , B23K35/3066 , B23K2103/05
摘要： In one embodiment, the present invention provides a method for welding together two metal pieces, comprising buttering a surface of a first metal piece with a first nickel-based filler metal at a thickness sufficient to isolate a heat-affected zone in the first metal piece from subsequent welding; heat-treating at least the heat-affected zone in the first metal piece; buttering a surface of a second metal piece with a second nickel-based filler metal having the same composition as the first nickel-based filler metal and at a thickness sufficient to isolate a heat-affected zone in the second metal piece from subsequent welding; heat-treating at least the heat-affected zone in the second metal piece; and welding the heat-treated first buttered surface to the heat-treated second buttered surface with a third nickel-based filler metal having the same composition as the first and second nickel-based filler metals.
摘要翻译： 在一个实施例中，本发明提供了一种用于将两个金属片焊接在一起的方法，包括将第一金属片的表面与第一镍基填充金属进行焊接，其厚度足以隔离第一金属片中的热影响区 从后续焊接; 至少对第一金属片中的热影响区域进行热处理; 用具有与第一镍基填充金属具有相同组成的第二镍基填料金属涂覆第二金属片的表面，并且具有足以将第二金属片中的热影响区隔离以后的焊接的厚度; 至少对第二金属片中的热影响区域进行热处理; 以及与第一和第二镍基填充金属具有相同组成的第三镍基填料金属将经热处理的第一加工表面焊接到经热处理的第二加工表面。
-
7.发明授权公开(公告)号：US07562807B2
公开(公告)日：2009-07-21
申请号：US10839863
申请日：2004-05-05
CPC分类号： C22C19/057 , B22F2998/00 , B23K35/3033 , C22C1/0433
摘要： Accordingly, the present invention provides a weld filler composition for joining different alloy steel pieces with substantially different chromium content, such as joining low alloy ferritic steel to high alloy ferritic steel, low alloy ferritic steel to austenitic stainless steel, or high alloy ferritic steel to austenitic stainless steel, and a method using the same. In one embodiment, the present invention provides a composition for a weld filler comprising nickel, iron, and chromium, which collectively comprise at least 50% by weight of the weld filler; niobium, carbon, manganese, molybdenum, and silicon, which collectively comprise no more than 50% by weight of the weld filler, and a niobium to carbon ratio of approximately 20 or less.
摘要翻译： 因此，本发明提供了一种焊接填料组合物，用于将不同的铬含量的不同合金钢片接合，例如将低合金铁素体钢接合到高合金铁素体钢，低合金铁素体钢到奥氏体不锈钢或高合金铁素体钢， 奥氏体不锈钢及其使用方法。 在一个实施方案中，本发明提供了一种用于焊接填料的组合物，其包含镍，铁和铬，它们共同包含至少50重量％的焊接填料; 铌，碳，锰，钼和硅，其总共不超过焊接填料的50重量％，铌与碳的比例为约20以下。
-
8.发明申请公开(公告)号：US20050247763A1
公开(公告)日：2005-11-10
申请号：US10839863
申请日：2004-05-05
CPC分类号： C22C19/057 , B22F2998/00 , B23K35/3033 , C22C1/0433
摘要： Accordingly, the present invention provides a weld filler composition for joining different alloy steel pieces with substantially different chromium content, such as joining low alloy ferritic steel to high alloy ferritic steel, low alloy ferritic steel to austenitic stainless steel, or high alloy ferritic steel to austenitic stainless steel, and a method using the same. In one embodiment, the present invention provides a composition for a weld filler comprising nickel, iron, and chromium, which collectively comprise at least 50% by weight of the weld filler; niobium, carbon, manganese, molybdenum, and silicon, which collectively comprise no more than 50% by weight of the weld filler, and a niobium to carbon ratio of approximately 20 or less.
摘要翻译： 因此，本发明提供了一种焊接填料组合物，用于将不同的铬含量的不同合金钢片接合，例如将低合金铁素体钢接合到高合金铁素体钢，低合金铁素体钢到奥氏体不锈钢或高合金铁素体钢， 奥氏体不锈钢及其使用方法。 在一个实施方案中，本发明提供了一种用于焊接填料的组合物，其包含镍，铁和铬，它们共同包含至少50重量％的焊接填料; 铌，碳，锰，钼和硅，其总共不超过焊接填料的50重量％，铌与碳的比例为约20以下。
-
公开(公告)号：US06673169B1
公开(公告)日：2004-01-06
申请号：US10115204
申请日：2002-04-01
申请人： Artie Gene Peterson, Jr. , David Wayne Gandy , Gregory J. Frederick , Jan T. Stover , Ramaswamy Viswanathan
发明人： Artie Gene Peterson, Jr. , David Wayne Gandy , Gregory J. Frederick , Jan T. Stover , Ramaswamy Viswanathan
IPC分类号： B23K1002
CPC分类号： B23K26/206 , B23K9/00 , B23K9/044 , B23K10/00 , B23K15/00 , B23K20/002 , B23K20/021 , B23K26/32 , B23K26/342 , B23K26/60 , B23K2101/001 , B23K2103/18 , B23K2103/26 , B23P6/007 , C22F1/10 , F01D5/005 , F05D2230/232 , F05D2230/30
摘要： A method of repairing a metallic component, such as a superalloy turbine blade or turbine nozzle, includes the step of preparing the component by stripping the protective coatings from the component. The component is then pre-conditioned for welding by a first hot isostatic process. Once the conditioning sequence is complete, the component is welded using any of a number of welding techniques and by adding weld fillers to the weld area. After the welding step, the component is sealed by a second hot isostatic process treatment performed at conditions similar to the first hot isostatic process. The component is finally prepared for re-entry into service.
摘要翻译： 修复诸如超级合金涡轮机叶片或涡轮喷嘴的金属部件的方法包括通过从组件剥离保护涂层来制备组件的步骤。 然后通过第一个热等静压过程对该部件进行预处理以进行焊接。 一旦调理顺序完成，使用多种焊接技术焊接组件，并通过在焊接区域添加焊接填料。 在焊接步骤之后，通过在类似于第一热等静压工艺的条件下进行的第二次热等静压处理来密封部件。 该组件终于准备重新投入使用。
-
10.发明申请公开(公告)号：US20060086708A1
公开(公告)日：2006-04-27
申请号：US10972249
申请日：2004-10-22
申请人： Kent Coleman , David Gandy , Ramaswamy Viswanathan
发明人： Kent Coleman , David Gandy , Ramaswamy Viswanathan
IPC分类号： B23K9/23
CPC分类号： B23K35/004 , B23K35/3033 , B23K35/3066 , B23K2103/05
摘要： In one embodiment, the present invention provides a method for welding together two metal pieces, comprising buttering a surface of a first metal piece with a first nickel-based filler metal at a thickness sufficient to isolate a heat-affected zone in the first metal piece from subsequent welding; heat-treating at least the heat-affected zone in the first metal piece; buttering a surface of a second metal piece with a second nickel-based filler metal having the same composition as the first nickel-based filler metal and at a thickness sufficient to isolate a heat-affected zone in the second metal piece from subsequent welding; heat-treating at least the heat-affected zone in the second metal piece; and welding the heat-treated first buttered surface to the heat-treated second buttered surface with a third nickel-based filler metal having the same composition as the first and second nickel-based filler metals.
-
-
-
-
-
-
-
-
-
搜索结果
12 条记录 (耗时 0.027 秒)
