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1. 发明授权

US08210823B2 Method and apparatus for creating seal slots for turbine components 有权
标题翻译：用于创建涡轮机部件密封槽的方法和装置
公开(公告)号：US08210823B2
公开(公告)日：2012-07-03
申请号：US12168935
申请日：2008-07-08
申请人： John D. Ward , Srikanth Kottilingam , Daniel Tragesser , Steven Rauch
发明人： John D. Ward , Srikanth Kottilingam , Daniel Tragesser , Steven Rauch
IPC分类号： F01D5/30
CPC分类号： F01D5/3007 , F01D11/006 , Y10T29/49316
摘要： A sealing slot system for a turbine dovetail. The sealing slot system may include a dovetail tab with a first leg and a second leg, an insert positioned between the first leg and the second leg so as to define a sealing slot, and a pin extending through the dovetail tab and the slot insert.
摘要翻译：一种用于涡轮燕尾榫的密封槽系统。密封槽系统可以包括具有第一腿部和第二腿部的燕尾片，插入件位于第一腿部和第二腿部之间，以便限定密封狭槽，以及延伸穿过燕尾舌片和狭槽插入物的针头。

2. 发明申请

US20100008781A1 Method and Apparatus for Creating Seal Slots for Turbine Components 有权
标题翻译：用于创建涡轮机部件密封槽的方法和装置
公开(公告)号：US20100008781A1
公开(公告)日：2010-01-14
申请号：US12168935
申请日：2008-07-08
申请人： John D. Ward , Srikanth Kottilingam , Daniel Tragesser , Steven Rauch
发明人： John D. Ward , Srikanth Kottilingam , Daniel Tragesser , Steven Rauch
IPC分类号： F01D5/30 , B23P15/04
CPC分类号： F01D5/3007 , F01D11/006 , Y10T29/49316
摘要： A sealing slot system for a turbine dovetail. The sealing slot system may include a dovetail tab with a first leg and a second leg, an insert positioned between the first leg and the second leg so as to define a sealing slot, and a pin extending through the dovetail tab and the slot insert.
摘要翻译：一种用于涡轮燕尾榫的密封槽系统。密封槽系统可以包括具有第一腿部和第二腿部的燕尾片，插入件位于第一腿部和第二腿部之间，以便限定密封狭槽，以及延伸穿过燕尾舌片和狭槽插入物的针头。

3. 发明申请

US20120213626A1 EXPLOSION-WELDED GAS TURBINE SHROUD AND A PROCESS OF FORMING AN EXPLOSION-WELDED GAS TURBINE 审中-公开
标题翻译：爆炸焊接气体涡轮机和形成爆炸焊接气体涡轮机的过程
公开(公告)号：US20120213626A1
公开(公告)日：2012-08-23
申请号：US13031925
申请日：2011-02-22
申请人： Daniel Nowak , George Goller , Srikanth Kottilingam , Melbourne Myers , Bill Damon Johnston
发明人： Daniel Nowak , George Goller , Srikanth Kottilingam , Melbourne Myers , Bill Damon Johnston
IPC分类号： F04D29/18 , B21K25/00
CPC分类号： F01D11/08 , B23K20/08 , B23K2101/001 , B23K2103/02 , B23K2103/04 , B23K2103/05 , B23K2103/08 , B23K2103/10 , B23K2103/12 , B23K2103/14 , B23K2103/18 , B23K2103/20 , B23K2103/22 , B23K2103/24 , B23K2103/26 , F05D2230/232 , F05D2240/11 , Y10T29/49321
摘要： An explosion-welded turbine shroud and a process of forming an explosion-welded gas turbine shroud are disclosed. The explosion-welded gas turbine shroud includes a first alloy explosion welded to a second alloy. In the explosion-welded gas turbine shroud, the first alloy forms at least a portion of a hot gas path or an expansion region of the gas turbine shroud includes the first alloy. The process includes explosion welding a first alloy to a second alloy to form the gas turbine shroud.
摘要翻译：公开了一种爆炸焊接的涡轮机罩和形成爆炸焊接的燃气涡轮机罩的工艺。爆炸焊接的燃气涡轮机护罩包括焊接到第二合金的第一合金爆炸。在爆炸焊接的燃气轮机护罩中，第一合金形成热气路径的至少一部分或燃气轮机罩的膨胀区域包括第一合金。该方法包括将第一合金爆炸焊接到第二合金以形成燃气涡轮罩。

4. 发明授权

US09108266B2 Welded component, a welded gas turbine component, and a process of welding a component 有权
标题翻译：焊接部件，焊接燃气轮机部件以及焊接部件的工序
公开(公告)号：US09108266B2
公开(公告)日：2015-08-18
申请号：US13089719
申请日：2011-04-19
申请人： Yan Cui , Ganjiang Feng , Srikanth Kottilingam , Dechao Lin
发明人： Yan Cui , Ganjiang Feng , Srikanth Kottilingam , Dechao Lin
IPC分类号： B23K15/00 , B23K26/00 , B23K26/20 , B23K26/32
CPC分类号： B23K15/0093 , B23K15/0073 , B23K26/211 , B23K26/323 , B23K2101/001 , B23K2103/18 , B23K2103/26 , Y10T428/12493
摘要： A welded component, a welded gas turbine component, and a process of welding a component are disclosed. The welded component includes a first alloy, a second alloy, and a weld positioned between the first alloy and the second alloy. The weld is formed by a first shim and a second shim being beam welded.
摘要翻译：公开了焊接部件，焊接燃气轮机部件以及焊接部件的工序。焊接部件包括位于第一合金和第二合金之间的第一合金，第二合金和焊接部。焊接由第一垫片和第二垫片形成为梁焊接。

5. 发明申请

US20060208032A1 Manufacture of specialized alloys with specific properties 有权
标题翻译：制造具有特定性能的专业合金
公开(公告)号：US20060208032A1
公开(公告)日：2006-09-21
申请号：US11082103
申请日：2005-03-16
申请人： William Jones , Srikanth Kottilingam
发明人： William Jones , Srikanth Kottilingam
IPC分类号： A47J36/02
CPC分类号： B23K20/1215 , B23K20/122 , B23K35/0244 , C22C26/00 , C22C29/00 , C22C2026/002
摘要： A method of manufacturing specialized alloys having specific properties and an alloy made using this method. The methods involve the use of micro and/or nano-sized particles that are mixed into an alloy using a friction stir welding method. The micro and/or nano-sized particles are used to alter one or more characteristics of the alloy in the locations in which the micro and/or nano-sized particles are added. The micro and/or nano-sized particles may be metal particles, non-metal particles, or a combination thereof.
摘要翻译：制造具有特定性能的专用合金的方法和使用该方法制造的合金。这些方法涉及使用摩擦搅拌焊接方法将微混合和/或纳米尺寸的颗粒混合到合金中。使用微尺寸和/或纳米尺寸的颗粒来改变在添加微米和/或纳米尺寸颗粒的位置中合金的一个或多个特性。微尺寸和/或纳米尺寸的颗粒可以是金属颗粒，非金属颗粒或其组合。

6. 发明申请

US20060157165A1 Weldability of alloys with directionally-solidified grain structure 有权
标题翻译：具有定向凝固的晶粒结构的合金的可焊性
公开(公告)号：US20060157165A1
公开(公告)日：2006-07-20
申请号：US11036991
申请日：2005-01-18
申请人： Srikanth Kottilingam , Peter Ditzel
发明人： Srikanth Kottilingam , Peter Ditzel
IPC分类号： C22F1/10
CPC分类号： C22C21/00 , B23K26/356
摘要： A method of welding alloys having directionally-solidified grain structure. The methods improve the weldability of these alloys by creating a localized region of fine grain structure, wherein the welding occurs in these localized regions. The localized regions are formed by applying strain energy using a variety of different methods, such as by hammer peening, laser peening or sand blasting. Then, a heat treatment step may be used to create recrystallized grains having the fine grain structure. The region of fine grain structure provides better weldability.
摘要翻译：焊接具有定向凝固的晶粒结构的合金的方法。该方法通过产生细晶粒结构的局部区域来改善这些合金的可焊性，其中焊接发生在这些局部区域中。通过使用各种不同的方法施加应变能来形成局部区域，例如通过锤击，激光喷丸或喷砂。然后，可以使用热处理步骤来产生具有细晶粒结构的再结晶晶粒。细晶粒结构区域提供更好的焊接性。

7. 发明申请

US20050050705A1 Repair of nickel-based alloy turbine disk 有权
标题翻译：镍基合金涡轮盘修复
公开(公告)号：US20050050705A1
公开(公告)日：2005-03-10
申请号：US10938713
申请日：2004-09-10
申请人： David Segletes , Brij Seth , Srikanth Kottilingam , Peter Ditzel
发明人： David Segletes , Brij Seth , Srikanth Kottilingam , Peter Ditzel
IPC分类号： B63H1/16 , F01D5/00 , F03B3/12
CPC分类号： F01D5/005 , F05D2230/232 , F05D2230/30 , F05D2300/606 , F05D2300/607 , Y10T29/49318 , Y10T29/49726 , Y10T29/4973 , Y10T29/49732 , Y10T29/49734 , Y10T29/49737 , Y10T29/49742 , Y10T29/49746
摘要： A method of adding material to a nickel-based superalloy component, such as a gas turbine rotor disk, without damaging the underlying material and without creating an unacceptable level of cracking. The method is advantageously applied in the repair of Alloy 706 turbine rotors having experienced operating failures in the steeple region of the disk. Once the damaged material is removed, replacement nickel-based superalloy material is added using a welding process that protects both the underlying material and the replacement material. The replacement material may be added by welding, with the preheat temperature maintained no lower than 100° C. below the aging temperature of the deposited alloy and with the interpass temperature maintained below the solution annealing temperature of the alloy. Alternatively, the replacement material may be preformed and welded to the original material using a friction welding process. In one embodiment, a replacement steeple of directionally solidified or single crystal material is installed onto a disk hub using a linear friction welding technique.
摘要翻译：将材料添加到镍基超级合金部件（例如燃气轮机转子盘）上而不损坏下面的材料并且不产生不可接受的开裂水平的方法。该方法有利地应用于在盘的尖顶区域中经历操作故障的合金706涡轮转子的修复中。一旦损坏的材料被去除，使用保护底层材料和替换材料的焊接工艺来添加替代的镍基超级合金材料。替代材料可以通过焊接加入，预热温度保持在低于沉积合金的老化温度以下的100℃以下，层间温度保持在合金的固溶退火温度以下。或者，可以使用摩擦焊接方法将更换材料预成型并焊接到原始材料。在一个实施例中，使用线性摩擦焊接技术将定向凝固或单晶材料的替换尖顶安装到盘毂上。

8. 发明申请

US20050015980A1 Repair of combustion turbine components 有权
标题翻译：燃气轮机组件修理
公开(公告)号：US20050015980A1
公开(公告)日：2005-01-27
申请号：US10669867
申请日：2003-09-24
申请人： Srikanth Kottilingam , Peter Ditzel
发明人： Srikanth Kottilingam , Peter Ditzel
IPC分类号： B23K10/02 , B23K35/02 , B23K35/32 , B23P6/00 , F01D5/00 , F01D5/18 , F01D9/02
CPC分类号： B23P6/007 , B23K10/027 , B23K35/0227 , B23K35/0244 , B23K35/32 , B23K2101/001 , B23P2700/06 , F01D5/005 , F01D5/187 , F01D9/023 , Y02T50/67 , Y02T50/676 , Y10T29/49233 , Y10T29/49318 , Y10T29/49734 , Y10T29/49737 , Y10T29/49742
摘要： A method of repairing a combustion turbine component having damage located at or near a cooling hole or hollow or geometrically complex portion of the component is provided. The method comprises forming a preparatory groove that extends from a surface of the component to the damaged area but does not extend to the cooling hole or hollow or geometrically complex portion of the component, the groove extending 40-90% the distance from the component to the damaged area; spraying a filler material into the groove with a micro-plasma torch at a current of less than 50 amperes; and filling the groove with the filler material such that the heated filler material substantially extends from the cooling hole or hollow or geometrically complex portion of the component to a surface of the component.
摘要翻译：提供了一种修复具有位于组件的冷却孔或中空或几何复杂部分处或附近的损伤的燃气涡轮机部件的方法。该方法包括形成从部件的表面延伸到损坏区域但不延伸到部件的冷却孔或中空或几何复杂部分的准备槽，该槽延伸40-90％的距离，从该部件到受损区域; 使用小于50安培的电流的微等离子体焰炬将填充材料喷射到凹槽中; 并且用填充材料填充凹槽，使得加热的填充材料基本上从组件的冷却孔或中空或几何复杂的部分延伸到部件的表面。

9. 发明授权

US07775414B2 Consumable insert and method of using the same 有权
标题翻译：消耗品插入物及其使用方法
公开(公告)号：US07775414B2
公开(公告)日：2010-08-17
申请号：US10679080
申请日：2003-10-04
申请人： Peter J. Ditzel , Srikanth Kottilingam
发明人： Peter J. Ditzel , Srikanth Kottilingam
IPC分类号： B23K35/14
CPC分类号： B23K35/0266 , B23K35/0272 , B23K35/3033
摘要： A consumable insert (10) formed of material particles (14) contained within a sheath (12). The particles may be a melting point depressant that has a concentration that is greater in a center region (16) of the insert than in the surface region (18) of the insert, thereby facilitating complete melting of the insert during a transient liquid phase bonding process. Alternatively, the particles may be a low-ductility material, such as a superalloy or an MCrAlY alloy, contained within a high ductility sheath material formed into a ribbon shape, thereby allowing the low-ductility material to be delivered in ribbon form during a coating process.
摘要翻译：由包含在护套（12）内的材料颗粒（14）形成的可消耗插入件（10）。颗粒可以是在插入件的中心区域（16）中具有比在插入件的表面区域（18）中大的浓度的熔点抑制剂，从而有助于在瞬态液相粘合期间插入物的完全熔化处理。或者，颗粒可以是包含在形成为带状的高延展性护套材料中的低延展性材料，例如超合金或MCrAlY合金，从而允许低延展性材料在涂层期间以带状输送处理。

10. 发明申请

US20060042729A1 Heat treatment of superalloy components 有权
标题翻译：超级合金部件的热处理
公开(公告)号：US20060042729A1
公开(公告)日：2006-03-02
申请号：US10932718
申请日：2004-09-02
申请人： Srikanth Kottilingam , Peter Ditzel
发明人： Srikanth Kottilingam , Peter Ditzel
IPC分类号： C22F1/10
CPC分类号： C22F1/10 , Y10T29/49336
摘要： An improved method of heat treating superalloys prior to welding includes subjecting only the portion of the component to be repaired to a localized heat treatment, leaving the remainder of the component untreated. The localized heat treatment permits the use of higher hold temperatures that are near, at, or above the Ni3(Al,Ti) solution temperature of the alloy. Such heat treatment prevents strain age cracking and also prevents recrystallization in areas that are not heat treated. Such localized heat treatment can be applied before and/or after welding, for material rejuvenation, pre-brazing, and post-brazing.
摘要翻译：在焊接之前对高温合金进行热处理的改进方法包括只对待修复的部件的一部分进行局部热处理，使组分的其余部分未经处理。局部热处理允许使用比合金的Ni 3（Al，Ti）溶液温度接近，等于或高于更高的保持温度。这种热处理可防止应变时效开裂，并且防止在未被热处理的区域中的再结晶。这种局部热处理可以在焊接之前和/或之后施加，用于材料复原，预钎焊和后钎焊。

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