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1. 发明申请

US20090060735A1 TURBINE ROTOR APPARATUS AND SYSTEM 审中-公开
标题翻译：涡轮转子装置和系统
公开(公告)号：US20090060735A1
公开(公告)日：2009-03-05
申请号：US11848645
申请日：2007-08-31
申请人： Swami Ganesh , Robin Carl Schwant , Lyle B. Spiegel
发明人： Swami Ganesh , Robin Carl Schwant , Lyle B. Spiegel
IPC分类号： F01D1/00 , F01D5/02 , F04D3/00
CPC分类号： F01D5/063 , F05D2230/233 , F05D2230/235 , Y02T50/671
摘要： A segmented turbine rotor is disclosed. The segmented turbine rotor has a plurality of rows of a plurality of turbine blades. At least one rotor segment of a plurality of rotor segments of the segmented turbine rotor includes a ring disposed circumferentially about and having an axis substantially parallel to a central axis of the rotor, the ring defining a cavity disposed at a center thereof and having an outer surface supporting at least one row of the plurality of rows of turbine blades.
摘要翻译：公开了一种分段涡轮转子。分段涡轮转子具有多排多个涡轮叶片。分段式涡轮机转子的多个转子段中的至少一个转子段包括围绕并且具有基本上平行于转子的中心轴线的轴线设置的环，该环限定了设置在其中心处的空腔，表面支撑多排涡轮叶片的至少一排。

2. 发明申请

US20110198318A1 HORIZONTAL WELDING METHOD AND JOINT STRUCTURE THEREFOR 审中-公开
标题翻译：水平焊接方法及其结构
公开(公告)号：US20110198318A1
公开(公告)日：2011-08-18
申请号：US12704866
申请日：2010-02-12
申请人： Alan Joseph Silvia , William Edward Babcock , Swami Ganesh , Jonathan T. Salkin , Robin Carl Schwant , Lyle B. Spiegel
发明人： Alan Joseph Silvia , William Edward Babcock , Swami Ganesh , Jonathan T. Salkin , Robin Carl Schwant , Lyle B. Spiegel
IPC分类号： B23K9/16
CPC分类号： B23K9/0026 , B23K9/0206 , B23K9/167 , B23K9/173 , B23K9/232 , B23K31/02 , B23K33/004 , B23K2101/001 , F01D5/063
摘要： Embodiments of the invention relate generally to welding methods and, more particularly, to methods for welding in a horizontal position and a joint structure suitable for such methods. In one embodiment, the invention provides a method of forming a welded joint between two components, the method comprising: aligning a first and second component to form a joint therebetween, the joint comprising: a protrusion of the first component, and a recess of the second component, wherein the protrusion and recess have complimentary shapes; orienting the first and second components such that a major axis of each is oriented vertically; and welding the first and second components at a substantially horizontally-oriented root opening, the substantially horizontally-oriented root opening positioned along the joint.
摘要翻译：本发明的实施方案一般涉及焊接方法，更具体地，涉及在水平位置焊接的方法和适于这种方法的接头结构。在一个实施例中，本发明提供了一种在两个部件之间形成焊接接头的方法，所述方法包括：对准第一和第二部件以在其间形成接头，所述接头包括：第一部件的突出部分和第二部件，其中所述突起和凹部具有互补形状; 使第一和第二部件定向成使得每个部件的长轴垂直取向; 并且将第一和第二部件以基本上水平定向的根部开口焊接，所述大致水平定向的根部开口沿着接头定位。

3. 发明申请

US20090057287A1 METHOD AND APPARATUS RELATED TO JOINING DISSIMILAR METAL 审中-公开
标题翻译：与接合金属相关的方法和装置
公开(公告)号：US20090057287A1
公开(公告)日：2009-03-05
申请号：US11848584
申请日：2007-08-31
申请人： Swami Ganesh , Robin Carl Schwant , Lyle B. Spiegel
发明人： Swami Ganesh , Robin Carl Schwant , Lyle B. Spiegel
IPC分类号： B23K11/00
CPC分类号： B23P15/04 , B23K9/232 , B23K20/129 , B23K2101/001 , B23P15/006
摘要： A method to join a first and second item that are made from different materials is disclosed. The method includes using a dual alloy member disposed between the first item and the second item, the dual alloy member comprising a first material, a second material different from the first material, and a wrought region between the first material and the second material. The method further includes melting together a localized area of material of the first item and the first material, thereby creating a first weld joint substantially absent intermixing of the first material with the second material, and melting together a localized area of material of the second item and the second material, thereby creating a second weld joint substantially absent intermixing of the second material with the first material, and thereby joining the first item to the second item.
摘要翻译：公开了一种连接由不同材料制成的第一和第二物品的方法。该方法包括使用设置在第一物品和第二物品之间的双重合金元件，所述双合金元件包括第一材料，与第一材料不同的第二材料，以及第一材料和第二材料之间的锻造区域。该方法还包括将第一物品的材料的局部区域和第一材料熔合在一起，从而产生基本上不使第一材料与第二材料混合的第一焊接接头，并将第二物料的局部区域的材料熔化在一起和第二材料，从而产生基本上不使第二材料与第一材料混合的第二焊接接头，从而将第一物品与第二物品接合。

4. 发明授权

US08414267B2 Multiple alloy turbine rotor section, welded turbine rotor incorporating the same and methods of their manufacture 有权
标题翻译：多合金涡轮转子部分，包含其的焊接涡轮转子及其制造方法
公开(公告)号：US08414267B2
公开(公告)日：2013-04-09
申请号：US12570566
申请日：2009-09-30
申请人： Swami Ganesh , Robin Carl Schwant
发明人： Swami Ganesh , Robin Carl Schwant
IPC分类号： F01D5/02
CPC分类号： F01D5/063 , B21J5/002 , B21K1/28 , B22F5/009 , B22F7/062 , B23K35/0261 , B23K2101/001 , B23P15/006 , C22C19/00 , F01D5/28 , F05D2230/23 , F05D2230/25 , Y02E10/721 , Y10T29/49316 , Y10T29/4932
摘要： A method of making a multiple alloy, multi-section welded turbine rotor includes providing a forged multiple alloy rotor section having an integral microstructure, the rotor section comprising a first alloy having a first alloy composition and second alloy having a second alloy composition, a first weld face comprising the first alloy on a first end and an a second weld face comprising the second alloy on an opposed second end. The method also includes providing a first rotor section comprising the first alloy composition and a second rotor section comprising the second alloy composition. The method also includes welding the first rotor section to the first weld face and welding the second rotor section to the second weld face.
摘要翻译：制造多合金，多段焊接涡轮转子的方法包括提供具有整体微结构的锻造多合金转子部分，所述转子部分包括具有第一合金组成的第一合金和具有第二合金组成的第二合金，第一合金在第一端上包括第一合金的焊接面和在相对的第二端上包括第二合金的第二焊接面。该方法还包括提供包括第一合金组合物的第一转子部分和包括第二合金组合物的第二转子部分。该方法还包括将第一转子部分焊接到第一焊接面并将第二转子部分焊接到第二焊接面。

5. 发明申请

US20130004317A1 TURBINE DISK PREFORM, WELDED TURBINE ROTOR MADE THEREWITH AND METHODS OF MAKING THE SAME 有权
标题翻译：涡轮盘预制件，焊接式涡轮转子及其制造方法
公开(公告)号：US20130004317A1
公开(公告)日：2013-01-03
申请号：US13172943
申请日：2011-06-30
申请人： Swami Ganesh , Steven Louis Breitenbach , Robin Carl Schwant
发明人： Swami Ganesh , Steven Louis Breitenbach , Robin Carl Schwant
IPC分类号： F01D5/02 , C21D7/08 , B23P15/04 , C21D7/06
CPC分类号： F01D5/063 , B23K2101/001 , Y10T29/479 , Y10T29/49321 , Y10T29/49325
摘要： A method of making a turbine rotor is disclosed. The method includes forming a last stage disk preform having a disk axis, the preform having a rotor face and an opposed shaft face, the rotor face having a circumferential, axially-extending rotor rib protruding therefrom, the shaft face having a circumferential, axially-extending shaft rib protruding therefrom, the disk preform comprising a disk preform material. The method also includes joining the rotor rib to a rotor preform to form a rotor joint, the rotor preform comprising a rotor preform material. The method further includes joining the shaft rib to a shaft to form a shaft joint, the shaft comprising a shaft material, wherein the disk preform material is different than the rotor preform material and the shaft material.
摘要翻译：公开了一种制造涡轮转子的方法。该方法包括形成具有盘轴的最后级盘预制件，预型件具有转子面和相对的轴面，转子面具有从其突出的圆周方向轴向延伸的转子肋，该轴面具有周向的，延伸的轴肋从其突出，盘预制件包括盘预制件材料。该方法还包括将转子肋连接到转子预制件以形成转子接头，转子预制件包括转子预制件材料。该方法还包括将轴肋连接到轴以形成轴接头，该轴包括轴材料，其中盘预制件材料与转子预制件材料和轴材料不同。

6. 发明授权

US07546685B2 Process for producing a rotor 有权
标题翻译：制造转子的方法
公开(公告)号：US07546685B2
公开(公告)日：2009-06-16
申请号：US11070467
申请日：2005-03-01
申请人： Swami Ganesh , Robin Carl Schwant , Ling Yang , John Zhiqiang Wang , Francis Alexander Reed , Robert V. Falsetti
发明人： Swami Ganesh , Robin Carl Schwant , Ling Yang , John Zhiqiang Wang , Francis Alexander Reed , Robert V. Falsetti
IPC分类号： B23P15/02
CPC分类号： G01N29/0618 , B21K1/10 , B23P15/006 , F01D5/02 , F01D5/28 , G01N9/24 , G01N29/11 , G01N29/265 , G01N2291/02854 , G01N2291/044 , G01N2291/2693 , Y10T29/49316 , Y10T29/4932 , Y10T29/49336 , Y10T29/49337
摘要： A process for producing a rotor, the rotor formed thereby, as well as turbines in which such a rotor is installed. The rotor is formed by casting an ingot to have first and second regions formed of different alloys that intermix during casting to define a transition zone therebetween. The ingot is forged to yield a rotor forging that contains axially-aligned first and second alloy regions and a transition zone therebetween. The effects of the transition zone can be mitigated by modeling the transition zone and then off-center machining the forging so that the axis of rotation of the machined monolithic rotor is more centrally located with respect to the transition zone.
摘要翻译：用于制造转子的方法，由其形成的转子以及其中安装有这样的转子的涡轮机。转子通过铸造锭形成以具有由不同合金形成的第一和第二区域，其在铸造期间混合以在其间限定过渡区域。锻造铸锭以产生包含轴向对齐的第一和第二合金区域以及它们之间的过渡区域的转子锻造。通过对过渡区域进行建模，然后对锻造进行偏心加工，可以减轻过渡区域的影响，使得加工的整体式转子的旋转轴线相对于过渡区域更位于中心。

7. 发明授权

US08961144B2 Turbine disk preform, welded turbine rotor made therewith and methods of making the same 有权
标题翻译：涡轮盘预制件，由其制成的焊接涡轮转子及其制造方法
公开(公告)号：US08961144B2
公开(公告)日：2015-02-24
申请号：US13172943
申请日：2011-06-30
申请人： Swami Ganesh , Steven Louis Breitenbach , Robin Carl Schwant
发明人： Swami Ganesh , Steven Louis Breitenbach , Robin Carl Schwant
IPC分类号： F01D5/06
CPC分类号： F01D5/063 , B23K2101/001 , Y10T29/479 , Y10T29/49321 , Y10T29/49325
摘要： A method of making a turbine rotor is disclosed. The method includes forming a last stage disk preform having a disk axis, the preform having a rotor face and an opposed shaft face, the rotor face having a circumferential, axially-extending rotor rib protruding therefrom, the shaft face having a circumferential, axially-extending shaft rib protruding therefrom, the disk preform comprising a disk preform material. The method also includes joining the rotor rib to a rotor preform to form a rotor joint, the rotor preform comprising a rotor preform material. The method further includes joining the shaft rib to a shaft to form a shaft joint, the shaft comprising a shaft material, wherein the disk preform material is different than the rotor preform material and the shaft material.
摘要翻译：公开了一种制造涡轮转子的方法。该方法包括形成具有盘轴的最后级盘预制件，预型件具有转子面和相对的轴面，转子面具有从其突出的圆周方向轴向延伸的转子肋，该轴面具有周向的，延伸的轴肋从其突出，盘预制件包括盘预制件材料。该方法还包括将转子肋连接到转子预制件以形成转子接头，转子预制件包括转子预制件材料。该方法还包括将轴肋连接到轴以形成轴接头，该轴包括轴材料，其中盘预制件材料与转子预制件材料和轴材料不同。

8. 发明申请

US20110076147A1 Multiple Alloy Turbine Rotor Section, Welded Turbine Rotor Incorporating the Same and Methods of Their Manufacture 有权
标题翻译：多合金涡轮转子段，焊接涡轮转子及其制造方法
公开(公告)号：US20110076147A1
公开(公告)日：2011-03-31
申请号：US12570566
申请日：2009-09-30
申请人： Swami Ganesh , Robin Carl Schwant
发明人： Swami Ganesh , Robin Carl Schwant
IPC分类号： F03D1/06 , B23P15/00 , F03D3/06 , B21D22/00
CPC分类号： F01D5/063 , B21J5/002 , B21K1/28 , B22F5/009 , B22F7/062 , B23K35/0261 , B23K2101/001 , B23P15/006 , C22C19/00 , F01D5/28 , F05D2230/23 , F05D2230/25 , Y02E10/721 , Y10T29/49316 , Y10T29/4932
摘要： A method of making a multiple alloy, multi-section welded turbine rotor includes providing a forged multiple alloy rotor section having an integral microstructure, the rotor section comprising a first alloy having a first alloy composition and second alloy having a second alloy composition, a first weld face comprising the first alloy on a first end and an a second weld face comprising the second alloy on an opposed second end. The method also includes providing a first rotor section comprising the first alloy composition and a second rotor section comprising the second alloy composition. The method also includes welding the first rotor section to the first weld face and welding the second rotor section to the second weld face.
摘要翻译：制造多合金，多段焊接涡轮转子的方法包括提供具有整体微结构的锻造多合金转子部分，所述转子部分包括具有第一合金组成的第一合金和具有第二合金组成的第二合金，第一合金在第一端上包括第一合金的焊接面和在相对的第二端上包括第二合金的第二焊接面。该方法还包括提供包括第一合金组合物的第一转子部分和包括第二合金组合物的第二转子部分。该方法还包括将第一转子部分焊接到第一焊接面并将第二转子部分焊接到第二焊接面。

9. 发明授权

US06971850B2 Multiple alloy rotor and method therefor 有权
公开(公告)号：US06971850B2
公开(公告)日：2005-12-06
申请号：US10707306
申请日：2003-12-04
申请人： Swami Ganesh , Robin Carl Schwant , Ling Yang , John Zhiqiang Wang
发明人： Swami Ganesh , Robin Carl Schwant , Ling Yang , John Zhiqiang Wang
IPC分类号： B21K1/10 , B23P15/00 , B63H1/26 , F01D5/02 , F01D5/28 , G01N9/24 , G01N29/06 , G01N29/11 , G01N29/265 , F01D5/06
CPC分类号： G01N29/0618 , B21K1/10 , B23P15/006 , F01D5/02 , F01D5/28 , G01N9/24 , G01N29/11 , G01N29/265 , G01N2291/02854 , G01N2291/044 , G01N2291/2693 , Y10T29/49316 , Y10T29/4932 , Y10T29/49336 , Y10T29/49337
摘要： A process for producing a rotor, the rotor formed thereby, as well as turbines in which such a rotor is installed. The rotor is formed by casting an ingot to have first and second regions formed of different alloys that intermix during casting to define a transition zone therebetween. The ingot is forged to yield a rotor forging that contains axially-aligned first and second alloy regions and a transition zone therebetween. The effects of the transition zone can be mitigated by modeling the transition zone and then off-center machining the forging so that the axis of rotation of the machined monolithic rotor is more centrally located with respect to the transition zone.

10. 发明授权

US06962483B2 Multiple alloy rotor 有权
标题翻译：多合金转子
公开(公告)号：US06962483B2
公开(公告)日：2005-11-08
申请号：US10707308
申请日：2003-12-04
申请人： Swami Ganesh , Robin Carl Schwant , Peter William Schilke , Ling Yang , John Zhiqiang Wang , Robert B. Falsetti , Francis Alexander Reed
发明人： Swami Ganesh , Robin Carl Schwant , Peter William Schilke , Ling Yang , John Zhiqiang Wang , Robert B. Falsetti , Francis Alexander Reed
IPC分类号： B21K1/10 , B23P15/00 , G01N9/24 , G01N29/06 , G01N29/11 , G01N29/265 , F01D25/00
CPC分类号： B21K1/10 , B23P15/006 , F01D5/06 , F01D25/005 , G01N9/24 , G01N29/0618 , G01N29/11 , G01N29/265 , G01N2291/02854 , G01N2291/044 , G01N2291/2693
摘要： A monolithic rotor comprising first and second rotor regions axially aligned within the monolithic rotor and a transition zone therebetween. The first and second rotor regions are formed of different alloys and the transition zone having a composition that differs from and varies between the first and second rotor regions. The first rotor region is located within a high pressure region of the monolithic rotor and is formed from an alloy chosen from the group consisting of CrMoV low alloy steels, martensitic stainless steels containing about 11 to about 14 weight percent chromium, Fe—Ni alloys, and nickel-base alloys. The second rotor region is located within a low pressure region of the monolithic rotor and is formed from an alloy chosen from the group consisting of NiCrMoV low alloy steels and martensitic stainless steels containing about 11 to about 14 weight percent chromium.
摘要翻译：整体式转子包括在单片转子内轴向对准的第一和第二转子区域以及它们之间的过渡区域。第一和第二转子区域由不同的合金形成，并且过渡区域具有不同于第一和第二转子区域之间的变化。第一转子区域位于单片转子的高压区域内，并且由选自CrMoV低合金钢，含有约11至约14重量％铬的马氏体不锈钢，Fe-Ni合金，和镍基合金。第二转子区域位于单片转子的低压区域内，并且由选自NiCrMoV低合金钢和含有约11至约14重量％铬的马氏体不锈钢的合金形成。

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