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1. 发明授权

EP3192885B1 INTERNALLY COOLED NI-BASE SUPERALLOY COMPONENT WITH SPALLATION-RESISTANT TBC SYSTEM 有权转让
公开(公告)号：EP3192885B1
公开(公告)日：2020-05-06
申请号：EP17150775.9
申请日：2017-01-10
申请人： United Technologies Corporation
发明人： Task, Michael N. , Boeke, Mark A. , Levine, Jeffrey R. , Bergman, Russell J.
IPC分类号： C22C19/05 , C23C28/00 , C23C30/00

2. 发明公开

EP2360350A3 Combined featherseal slot and lightening pocket 有权转让
标题翻译：合并的槽的密封条和节省重量的袋
公开(公告)号：EP2360350A3
公开(公告)日：2014-08-20
申请号：EP11250213.3
申请日：2011-02-24
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Kovach, Scott A.
IPC分类号： F01D9/04 , F01D11/00
CPC分类号： F01D11/005 , F01D9/041 , F01D25/12 , F05D2220/323 , F05D2230/12 , F05D2230/21 , F05D2240/12 , F05D2240/55 , F05D2250/75 , F05D2260/20
摘要： A segmented engine component has multiple segments which are connected to each other via a featherseal (144) arrangement. Each of the components has a combined featherseal slot (146) and lightening pocket (148).

3. 发明公开

EP2372099A2 Turbine sealing system 有权转让
标题翻译： Turbinendichtungssystem
公开(公告)号：EP2372099A2
公开(公告)日：2011-10-05
申请号：EP11159741.5
申请日：2011-03-25
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Chrisikos, James P. , Bach, Leonard A.
IPC分类号： F01D11/00
CPC分类号： F01D11/005 , F01D9/042 , F05D2240/57
摘要： A sealing system (8) for sealing a gap (134) between a first body (110) and a second body (112) includes a first seal (114) having a first portion (136) adapted to be attached to the first body (110) and a second portion (130) extending into the gap (134). The sealing system (8) also includes a second seal (116). The second seal (116) has a first portion adapted to be attached to the second body (112) and a second portion (132) extending across the gap (134). The second portion (130) of the first seal (114) and the second portion (132) of the second seal (116) are adjacent and overlapping with each other to seal the gap (134).
摘要翻译：用于密封第一主体（110）和第二主体（112）之间的间隙（134）的密封系统（8）包括第一密封件（114），其具有适于附接到第一主体（112）的第一部分（136） 110）和延伸到间隙（134）中的第二部分（130）。密封系统（8）还包括第二密封件（116）。第二密封件（116）具有适于附接到第二主体（112）的第一部分和跨过间隙（134）延伸的第二部分（132）。第一密封件（114）的第二部分（130）和第二密封件（116）的第二部分（132）彼此相邻并重叠以密封间隙（134）。

4. 发明授权

EP2636852B1 Hybrid inner air seal for gas turbine engines 有权转让
公开(公告)号：EP2636852B1
公开(公告)日：2019-03-06
申请号：EP13150426.8
申请日：2013-01-07
申请人： United Technologies Corporation
发明人： Caprario, Joseph T. , Bergman, Russell J. , Humphrey, Pamela A. , Sandoval, Jonathan Perry
IPC分类号： F01D11/00

5. 发明公开

EP2366873A3 Cover plate for turbine vane assembly 有权转让
标题翻译：盖板用于涡轮机叶片
公开(公告)号：EP2366873A3
公开(公告)日：2015-01-14
申请号：EP11158341.5
申请日：2011-03-15
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Bridges, Joseph W. , Richter, Kevin R.
IPC分类号： F01D9/04 , F01D25/12
CPC分类号： F01D9/041 , F01D25/12 , F05D2260/201 , Y02T50/676 , Y10T428/24273 , Y10T428/24802
摘要： A cover plate (100) for a turbine vane is formed from a material blank configured to provide the cover plate (100) with a flexible flange area (118) that can be secured to the turbine vane assembly. The flange area (118) may have a range of motion that may be responsive to an installation force, which effectively modifies the configuration of the cover plate (100) to such degree as to seal the cover plate to the turbine vane assembly. The flange area (118) includes flexible wings (132) separated by a gap (130) which contains a weld (138).

6. 发明公开

EP2366873A2 Cover plate for turbine vane assembly 有权转让
标题翻译： AbdeckplattefürTurbinenschaufeln
公开(公告)号：EP2366873A2
公开(公告)日：2011-09-21
申请号：EP11158341.5
申请日：2011-03-15
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Bridges, Joseph W. , Richter, Kevin R.
IPC分类号： F01D9/04
CPC分类号： F01D9/041 , F01D25/12 , F05D2260/201 , Y02T50/676 , Y10T428/24273 , Y10T428/24802
摘要： A cover plate (100) for a turbine vane is formed from a material blank configured to provide the cover plate (100) with a flexible flange area (118) that can be secured to the turbine vane assembly. The flange area (118) may have a range of motion that may be responsive to an installation force, which effectively modifies the configuration of the cover plate (100) to such degree as to seal the cover plate to the turbine vane assembly. The flange area (118) includes flexible wings (132) separated by a gap (130) which contains a weld (138).
摘要翻译：用于涡轮叶片的盖板（100）由材料坯料形成，所述材料坯料被配置为向所述盖板（100）提供可固定到所述涡轮叶片组件的柔性凸缘区域（118）。凸缘区域（118）可以具有可以响应于安装力的运动范围，该安装力有效地将盖板（100）的构造改变为将盖板密封到涡轮叶片组件的程度。凸缘区域（118）包括由包含焊缝（138）的间隙（130）分开的柔性翼（132）。

7. 发明公开

EP2360350A2 Combined featherseal slot and lightening pocket 有权转让
标题翻译： Kombinierte Nut eines Dichtstreifens sowie gewichtssparende Tasche
公开(公告)号：EP2360350A2
公开(公告)日：2011-08-24
申请号：EP11250213.3
申请日：2011-02-24
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Kovach, Scott A.
IPC分类号： F01D9/04
CPC分类号： F01D11/005 , F01D9/041 , F01D25/12 , F05D2220/323 , F05D2230/12 , F05D2230/21 , F05D2240/12 , F05D2240/55 , F05D2250/75 , F05D2260/20
摘要： A segmented engine component has multiple segments which are connected to each other via a featherseal (144) arrangement. Each of the components has a combined featherseal slot (146) and lightening pocket (148).
摘要翻译：分段发动机部件具有多个通过羽毛（144）布置彼此连接的部分。每个部件具有组合的羽状缝隙（146）和减重口袋（148）。

8. 发明授权

EP2360350B1 Combined featherseal slot and lightening pocket 有权转让
公开(公告)号：EP2360350B1
公开(公告)日：2018-06-06
申请号：EP11250213.3
申请日：2011-02-24
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Kovach, Scott A.
IPC分类号： F01D9/04 , F01D11/00
CPC分类号： F01D11/005 , F01D9/041 , F01D25/12 , F05D2220/323 , F05D2230/12 , F05D2230/21 , F05D2240/12 , F05D2240/55 , F05D2250/75 , F05D2260/20
摘要： A segmented engine component has multiple segments which are connected to each other via a featherseal (144) arrangement. Each of the components has a combined featherseal slot (146) and lightening pocket (148).

9. 发明公开

EP3192885A1 INTERNALLY COOLED NI-BASE SUPERALLOY COMPONENT WITH SPALLATION-RESITANT TBC SYSTEM 有权转让
标题翻译：内部冷却的镍基高温合金元件与分散性TBC系统
公开(公告)号：EP3192885A1
公开(公告)日：2017-07-19
申请号：EP17150775.9
申请日：2017-01-10
申请人： United Technologies Corporation
发明人： Task, Michael N. , Boeke, Mark A. , Levine, Jeffrey R. , Bergman, Russell J.
IPC分类号： C22C19/05 , C23C28/00 , C23C30/00
摘要： A gas turbine engine component comprising a nozzle segment, the nozzle segment comprising at least one substrate having a surface. A metallic bondcoat is coupled to the surface of the substrate. An yttria-stabilized zirconia thermal barrier coating is coupled to the metallic bondcoat opposite the surface.
摘要翻译：一种包括喷嘴段的燃气涡轮发动机部件，所述喷嘴段包括具有表面的至少一个基板。金属粘合涂层被连接到基底的表面。氧化钇稳定的氧化锆热障涂层与表面相对的金属结合涂层偶联。

10. 发明授权

EP2366873B1 Cover plate for turbine vane assembly 有权转让
标题翻译：盖板用于涡轮机叶片
公开(公告)号：EP2366873B1
公开(公告)日：2016-05-11
申请号：EP11158341.5
申请日：2011-03-15
申请人： United Technologies Corporation
发明人： Bergman, Russell J. , Bridges, Joseph W. , Richter, Kevin R.
IPC分类号： F01D9/04 , F01D25/12
CPC分类号： F01D9/041 , F01D25/12 , F05D2260/201 , Y02T50/676 , Y10T428/24273 , Y10T428/24802

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