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1. 发明授权

EP2642076B1 Connecting system for metal components and cmc components, a turbine blade retaining system and a rotating component retaining system 有权转让
标题翻译：用于金属部件和cmc部件的连接系统，涡轮叶片保持系统和旋转部件保持系统
公开(公告)号：EP2642076B1
公开(公告)日：2018-01-17
申请号：EP13158942.6
申请日：2013-03-13
申请人： General Electric Company
发明人： Floyd, Donald Earl
IPC分类号： F01D5/28 , F01D5/30
CPC分类号： F01D5/284 , F01D5/3007 , F01D5/3053 , F01D5/3084 , F05D2260/30 , F05D2300/50212 , F05D2300/6033 , F05D2300/612
摘要： A connecting system (100) for metal components (112) and CMC components (114), a turbine blade retaining system (130) and rotating component retaining system (200) are provided. The connecting system (100) includes a retaining pin (122), a metal foam bushing (116), a first aperture (108) disposed in the metal component (112), and a second aperture (110) disposed in the ceramic matrix composite component (114). The first aperture (108) and the second aperture (110) are configured to form a through-hole (132) when the metal component (112) and the ceramic matrix composite component (114) are engaged. The retaining pin (122) and the metal foam bushing (116) are operably arranged within the through-hole (132) to connect the metal component (112) and the ceramic matrix composite component (114).

2. 发明公开

EP2642076A3 Connecting system for metal components and cmc components, a turbine blade retaining system and a rotating component retaining system 有权转让
标题翻译：为金属组分和CMC部件，涡轮机叶片保持系统和旋转部件保持系统连接系统
公开(公告)号：EP2642076A3
公开(公告)日：2014-01-08
申请号：EP13158942.6
申请日：2013-03-13
申请人： General Electric Company
发明人： Floyd, Donald Earl
IPC分类号： F01D5/28 , F01D5/30
CPC分类号： F01D5/284 , F01D5/3007 , F01D5/3053 , F01D5/3084 , F05D2260/30 , F05D2300/50212 , F05D2300/6033 , F05D2300/612
摘要： A connecting system (100) for metal components (112) and CMC components (114), a turbine blade retaining system (130) and rotating component retaining system (200) are provided. The connecting system (100) includes a retaining pin (122), a metal foam bushing (116), a first aperture (108) disposed in the metal component (112), and a second aperture (110) disposed in the ceramic matrix composite component (114). The first aperture (108) and the second aperture (110) are configured to form a through-hole (132) when the metal component (112) and the ceramic matrix composite component (114) are engaged. The retaining pin (122) and the metal foam bushing (116) are operably arranged within the through-hole (132) to connect the metal component (112) and the ceramic matrix composite component (114).
摘要翻译：提供了用于金属部件（112）和CMC组分A连接系统（100）（114），涡轮机叶片保持系统（130）和旋转构件保持系统（200）。所述连接系统（100）包括在所述陶瓷基体复合布置在保持销（122），金属泡沫衬套（116），在所述金属部件（112）和第二孔（110）布置的第一开口（108）部件（114）。所述第一孔（108）和第二孔（110）被配置为形成在金属部件（112）和陶瓷基质复合材料构件（114）接合的通孔（132）。保持销（122）和所述金属泡沫衬套（116）可操作地内配置所述通孔（132）连接的金属部件（112）和陶瓷基质复合材料构件（114）。

3. 发明公开

EP2642076A2 Connecting system for metal components and cmc components, a turbine blade retaining system and a rotating component retaining system 有权转让
标题翻译：为金属组分和CMC部件，涡轮机叶片保持系统和旋转部件保持系统连接系统
公开(公告)号：EP2642076A2
公开(公告)日：2013-09-25
申请号：EP13158942.6
申请日：2013-03-13
申请人： General Electric Company
发明人： Floyd, Donald Earl
IPC分类号： F01D5/28 , F01D5/30
CPC分类号： F01D5/284 , F01D5/3007 , F01D5/3053 , F01D5/3084 , F05D2260/30 , F05D2300/50212 , F05D2300/6033 , F05D2300/612
摘要： A connecting system (100) for metal components (112) and CMC components (114), a turbine blade retaining system (130) and rotating component retaining system (200) are provided. The connecting system (100) includes a retaining pin (122), a metal foam bushing (116), a first aperture (108) disposed in the metal component (112), and a second aperture (110) disposed in the ceramic matrix composite component (114). The first aperture (108) and the second aperture (110) are configured to form a through-hole (132) when the metal component (112) and the ceramic matrix composite component (114) are engaged. The retaining pin (122) and the metal foam bushing (116) are operably arranged within the through-hole (132) to connect the metal component (112) and the ceramic matrix composite component (114).

4. 发明公开

EP2626520A2 Turbine shell having a plate frame heat exchanger 审中-公开
标题翻译： Turbinengehäusemit einemPlattenrahmenwärmetauscher
公开(公告)号：EP2626520A2
公开(公告)日：2013-08-14
申请号：EP13154238.3
申请日：2013-02-06
申请人： General Electric Company
发明人： Floyd, Donald Earl
IPC分类号： F01D11/24 , F01D25/14 , F01D25/26
CPC分类号： F01D11/24 , F01D25/14 , F01D25/26 , F05D2260/213
摘要： A turbine shell (40) is provided, and includes a body portion (42) and at least one plate (50). The body portion (42) has a forward end portion (44) and an aft end portion (46). The plate (50) is located between the forward end portion (44) and the aft end portion (46). The plate (50) is part of a plate frame heat exchanger (54), which is part of the body portion (42) of the turbine shell (40).
摘要翻译：提供涡轮壳体（40），并且包括主体部分（42）和至少一个板（50）。主体部分（42）具有前端部分（44）和后端部分（46）。板（50）位于前端部（44）和后端部（46）之间。板（50）是板架热交换器（54）的一部分，其是涡轮机壳体（40）的主体部分（42）的一部分。

5. 发明授权

EP2642082B1 Thermal isolation apparatus 有权转让
标题翻译：隔热装置
公开(公告)号：EP2642082B1
公开(公告)日：2015-05-13
申请号：EP13159007.7
申请日：2013-03-13
申请人： General Electric Company
发明人： Floyd, Donald Earl , Johnson, David Martin
IPC分类号： F01D9/04
CPC分类号： F01D11/18 , F01D9/04 , F05D2300/502

6. 发明公开

EP2642082A1 Thermal isolation apparatus 有权转让
标题翻译：隔热装置
公开(公告)号：EP2642082A1
公开(公告)日：2013-09-25
申请号：EP13159007.7
申请日：2013-03-13
申请人： General Electric Company
发明人： Floyd, Donald Earl , Johnson, David Martin
IPC分类号： F01D11/18
CPC分类号： F01D11/18 , F01D9/04 , F05D2300/502
摘要： A thermal isolation apparatus 10 is provided and includes an annular casing 20 surrounding a turbine bucket stage and defining an annular recess 21 from an interior facing surface 22 thereof, an annular shroud 30 disposed within the casing to provide for a predefined clearance about rotating bucket tips of the turbine bucket stage, the shroud 30 including an annular main member 31 and an annular flange 33 extending from an outwardly facing surface 32 of the main member and being sized to fit within the recess and a thermal barrier 40 formed of porous material, which is interposed between opposing surfaces of the casing 20 and the flange 33 within the recess 21.
摘要翻译：提供隔热装置10，其包括围绕涡轮轮叶级并且从其内部面向表面22限定环形凹部21的环形壳体20，布置在壳体内以提供关于旋转铲斗尖端的预定间隙的环形护罩30 ，护罩30包括环形主构件31和环形凸缘33，环形凸缘33从主构件的面向外的表面32延伸并且尺寸被设计成配合在凹部内并由多孔材料形成的热屏障40 插入凹槽21内的壳体20和凸缘33的相对表面之间。

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