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1. 发明授权

EP1018405B1 Concentric wrench for blind access opening in a turbine 有权
标题翻译：同心扳手用于涡轮盲人通道开口
公开(公告)号：EP1018405B1
公开(公告)日：2007-02-14
申请号：EP99308438.3
申请日：1999-10-26
申请人： GENERAL ELECTRIC COMPANY
发明人： Laurer, Kurt Neal , Drlik, Gary Joseph , Gibler, Edward Eugene
IPC分类号： B25B13/48 , F01D21/00
CPC分类号： B25B13/481 , B25B13/48 , Y10T29/49318 , Y10T29/49963

2. 发明公开

EP1018405A2 Concentric wrench for blind access opening in a turbine 有权
标题翻译： KonzentrischerSchraubenschlüsselfürBlindzugangöffnungvon Turbinen
公开(公告)号：EP1018405A2
公开(公告)日：2000-07-12
申请号：EP99308438.3
申请日：1999-10-26
申请人： GENERAL ELECTRIC COMPANY
发明人： Laurer, Kurt Neal , Drlik, Gary Joseph , Gibler, Edward Eugene
IPC分类号： B25B13/48
CPC分类号： B25B13/481 , B25B13/48 , Y10T29/49318 , Y10T29/49963
摘要： The concentric wrench includes an outer tube (60) having flats (62) at one end and a gripping surface (64) at an opposite end. An inner tube (66) has interior flats (68) at one end and a gripping surface (70) at its opposite end. With the inner and outer tubes (60, 66) disposed about a pressure transmitting conduit, the tubes may be inserted into a blind access opening in the outer turbine casing to engage the flats (62, 68) of the tubes (60, 66) against hex nuts of an internal fitting. By relatively rotating the tubes (60, 66) using the externally exposed gripping surfaces (64, 70), the threaded connection between the parts of the fitting bearing the respective hex nuts can be tightened or loosened.
摘要翻译：同心扳手包括在一端具有平面（62）的外管（60）和在相对端的抓握表面（64）。内管（66）在一端具有内部平面（68）和在其相对端的夹持表面（70）。通过设置在压力传递导管周围的内管和外管（60,66），管可以插入到外涡轮机壳体中的盲进入开口中以接合管（60,66）的平面（62,68）针对内部配件的六角螺母。通过使用外露的夹持表面（64,70）相对地旋转管（60,66），可以拧紧或缩小轴承相应的六角螺母的配件的螺纹连接。

3. 发明公开

EP1018405A3 Concentric wrench for blind access opening in a turbine 有权
标题翻译：同心扳手用于涡轮盲人通道开口
公开(公告)号：EP1018405A3
公开(公告)日：2003-01-22
申请号：EP99308438.3
申请日：1999-10-26
申请人： GENERAL ELECTRIC COMPANY
发明人： Laurer, Kurt Neal , Drlik, Gary Joseph , Gibler, Edward Eugene
IPC分类号： B25B13/48 , F01D21/00
CPC分类号： B25B13/481 , B25B13/48 , Y10T29/49318 , Y10T29/49963
摘要： The concentric wrench includes an outer tube (60) having flats (62) at one end and a gripping surface (64) at an opposite end. An inner tube (66) has interior flats (68) at one end and a gripping surface (70) at its opposite end. With the inner and outer tubes (60, 66) disposed about a pressure transmitting conduit, the tubes may be inserted into a blind access opening in the outer turbine casing to engage the flats (62, 68) of the tubes (60, 66) against hex nuts of an internal fitting. By relatively rotating the tubes (60, 66) using the externally exposed gripping surfaces (64, 70), the threaded connection between the parts of the fitting bearing the respective hex nuts can be tightened or loosened.

4. 发明公开

EP1045114A3 Cooling supply system for stage 3 bucket of a gas turbine 有权
标题翻译：供给管延伸，用于冷却燃气涡轮叶片的第三阶段
公开(公告)号：EP1045114A3
公开(公告)日：2002-10-30
申请号：EP00303123.4
申请日：2000-04-13
申请人： GENERAL ELECTRIC COMPANY
发明人： Eldrid, Sacheverel Quetin , Leone, Sal Albert , Burns, James Lee , Drlik, Gary Joseph , Palmer, Gene David , Gibler, Edward Eugene
IPC分类号： F01D5/08 , F01D25/12 , F01D9/06 , F02C7/18
CPC分类号： F01D9/065 , F01D5/088 , Y02T50/673 , Y02T50/676
摘要： A gas turbine includes a compressor (55), a combustor and turbine section including at least three stages, and a cooling circuit including an inlet (56) into a third stage nozzle (N3) from the compressor (55) for feeding cooling air from the compressor (55) to the third stage nozzle (N3); at least one passageway (60, 62, 64, 70) running substantially radially through each airfoil (50, 52) of the third stage nozzle (N3) and an associated diaphragm (64), into an annular space (74) between the rotor (R) and the diaphragm (64); and passageways (76, 82) communicating between the annular space (74) and individual buckets (B3) of the third stage.

5. 发明授权

EP1045114B1 Land based gas turbine cooling system and method of cooling 有权
标题翻译：具有用于冷却的冷却系统和方法，陆基燃气轮机
公开(公告)号：EP1045114B1
公开(公告)日：2009-10-14
申请号：EP00303123.4
申请日：2000-04-13
申请人： GENERAL ELECTRIC COMPANY
发明人： Eldrid, Sacheverel Quetin , Leone, Sal Albert , Burns, James Lee , Drlik, Gary Joseph , Palmer, Gene David , Gibler, Edward Eugene
IPC分类号： F01D5/08 , F01D25/12 , F01D9/06 , F02C7/18
CPC分类号： F01D9/065 , F01D5/088 , Y02T50/673 , Y02T50/676

6. 发明公开

EP1045114A2 Cooling supply system for stage 3 bucket of a gas turbine 有权
标题翻译：发动机汽油发电机组（Kühlsystemund Verfahren zurKühlung）
公开(公告)号：EP1045114A2
公开(公告)日：2000-10-18
申请号：EP00303123.4
申请日：2000-04-13
申请人： GENERAL ELECTRIC COMPANY
发明人： Eldrid, Sacheverel Quetin , Leone, Sal Albert , Burns, James Lee , Drlik, Gary Joseph , Palmer, Gene David , Gibler, Edward Eugene
IPC分类号： F01D5/08 , F01D25/12
CPC分类号： F01D9/065 , F01D5/088 , Y02T50/673 , Y02T50/676
摘要： A gas turbine includes a compressor (55), a combustor and turbine section including at least three stages, and a cooling circuit including an inlet (56) into a third stage nozzle (N3) from the compressor (55) for feeding cooling air from the compressor (55) to the third stage nozzle (N3); at least one passageway (60, 62, 64, 70) running substantially radially through each airfoil (50, 52) of the third stage nozzle (N3) and an associated diaphragm (64), into an annular space (74) between the rotor (R) and the diaphragm (64); and passageways (76, 82) communicating between the annular space (74) and individual buckets (B3) of the third stage.
摘要翻译：一种燃气轮机包括压缩机（55），燃烧器和包括至少三级的涡轮部分，以及包括从压缩机（55）进入第三级喷嘴（N3）的入口（56）的冷却回路，用于将冷却空气压缩机（55）到第三级喷嘴（N3）; 至少一个通过第三级喷嘴（N3）的每个翼型件（50,52）径向延伸的通道（60,62,64,70）和相关联的隔膜（64），进入到转子之间的环形空间（R）和隔膜（64）; 以及在所述环形空间（74）和所述第三级的各个桶（B3）之间连通的通道（76,82）。

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