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91. 发明专利

JP2014139436A Turbomachine having swirl-inhibiting seal 有权
标题翻译：具有SWIRL-INHIBITIC SEAL的涡轮发酵
公开(公告)号：JP2014139436A
公开(公告)日：2014-07-31
申请号：JP2014005537
申请日：2014-01-16
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： ZHENG XIAOQING , JASON W JEWETT , MILLER RICHARD JAMES
IPC分类号： F01D11/02 , F01D25/00 , F01D25/24 , F16J15/447
CPC分类号： F01D11/04 , F01D11/001 , F01D11/08 , F05D2240/11 , F05D2240/80
摘要： PROBLEM TO BE SOLVED: To provide a swirl-inhibiting seal which is adapted to rubbing and does not require a large space.SOLUTION: Various embodiments include a turbomachine including a swirl-inhibiting seal. In various particular embodiments, a turbomachine includes: a rotor section having sets of axially disposed blades; and a diaphragm section at least partially surrounding the rotor section, the diaphragm section including a set of nozzles positioned between adjacent sets of axially disposed blades. The set of nozzles includes at least one nozzle having: a base section coupled to the diaphragm section; a blade coupled to the base section; and a radial tip section coupled to a radial end of the blade, the radial tip section including an axially extending flange having a slot extending therethrough for controlling a fluid flow in the turbomachine.
摘要翻译：要解决的问题：提供适于摩擦并且不需要大的空间的旋转抑制密封。解决方案：各种实施例包括涡流机，其包括涡流抑制密封件。在各种具体实施例中，涡轮机包括：具有一组轴向设置的叶片的转子部分; 以及至少部分地围绕所述转子部分的隔膜部分，所述隔膜部分包括位于相邻的轴向设置的叶片组之间的一组喷嘴。所述喷嘴组包括至少一个喷嘴，所述喷嘴具有：与所述隔膜部分联接的基部; 叶片，其联接到所述基部; 以及联接到所述叶片的径向端部的径向末端部分，所述径向末端部分包括轴向延伸的凸缘，所述凸缘具有延伸穿过其中的槽，用于控制所述涡轮机中的流体流动。

92. 发明专利

JP2014135051A Accommodation of different types of sensors in vibration monitoring system using external input or daughter board with interchangeable operating hardware 审中-公开
标题翻译：使用具有可互换操作硬件的外部输入或DAUGHTER板的振动监测系统中不同类型的传感器的存储
公开(公告)号：JP2014135051A
公开(公告)日：2014-07-24
申请号：JP2014000030
申请日：2014-01-06
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： PARAG VISHWANATH ACHARYA , SHRINIWAS ANANDA NEJE , ABHIJEET WARALE
IPC分类号： G05B19/05
CPC分类号： G01H11/00
摘要： PROBLEM TO BE SOLVED: To facilitate sensor change of a controller of a monitoring system.SOLUTION: In the monitoring system, a first printed circuit board includes an electrical circuit and signal processing hardware. A first sensor has first operating parameters and is in electrical communication with a second printed circuit board, and the second printed circuit board includes signal processing hardware configured to process a signal. The second printed circuit board is in electrical communication with the first printed circuit board through a connector. The connector is configured to permit insertion and removal of a third printed circuit board to operate a second sensor having second operating parameters that differ from the first operating parameters of the first sensor.
摘要翻译：要解决的问题：为了便于监控系统的控制器的传感器更换。解决方案：在监控系统中，第一印刷电路板包括电路和信号处理硬件。第一传感器具有第一操作参数并且与第二印刷电路板电连通，并且第二印刷电路板包括被配置为处理信号的信号处理硬件。第二印刷电路板通过连接器与第一印刷电路板电连通。连接器被配置为允许插入和移除第三印刷电路板以操作具有与第一传感器的第一操作参数不同的第二操作参数的第二传感器。

93. 发明专利

JP2014132258A Electrometer current injection by high voltage ramp 审中-公开
标题翻译：电子电流注入高电压RAMP
公开(公告)号：JP2014132258A
公开(公告)日：2014-07-17
申请号：JP2013228915
申请日：2013-11-05
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： DAN JAY MCCORMICK
IPC分类号： G01T1/185 , G01T1/16 , G21C17/00
CPC分类号： G01T1/185 , G01L21/34 , G01N27/62 , G01N27/66 , G01N27/68 , G01N27/70
摘要： PROBLEM TO BE SOLVED: To provide an apparatus and method for conducting a test cycle for an electrometer of an environmental radiation monitor by current injection.SOLUTION: An environmental radiation monitor 10 includes a high pressure ionization chamber 46, a power supply 60 electrically connected to the high pressure ionization chamber, and an electrometer 66 electrically connected to the high pressure ionization chamber. A controller 50 controls a power supply voltage signal provided to the high pressure ionization chamber to create a constant current to be injected into the electrometer. The method includes varying the voltage signal provided to the high pressure ionization chamber, measuring a current signal, processing the current signal with the electrometer, and comparing the voltage signal to an expected result, indicating proper operation of the electrometer. Further examples of the method include initiating and discontinuing a test function.
摘要翻译：要解决的问题：提供一种通过电流注入对环境辐射监测器的静电计进行测试循环的装置和方法。解决方案：环境辐射监测器10包括高压电离室46，电源60电连接到高压电离室和电连接到高压电离室的静电计66。控制器50控制提供给高压电离室的电源电压信号，以产生要注入静电计的恒定电流。该方法包括改变提供给高压电离室的电压信号，测量电流信号，用静电计处理电流信号，以及将电压信号与预期结果进行比较，指示静电计的适当操作。该方法的其他实例包括启动和中断测试功能。

94. 发明专利

JP2014132211A Articulated transition duct in turbomachine, where this invention was made with government support under contract number de-fc26-05nt42643 awarded by department of energy and government has certain rights in this invention 审中-公开
标题翻译：涡轮发电机中的转换导管，根据合同编号由政府提供的支持DE-FC26-05NT42643由能源和政府部门授予本发明的某些权利
公开(公告)号：JP2014132211A
公开(公告)日：2014-07-17
申请号：JP2013226104
申请日：2013-10-31
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： JAMES SCOTT FLANAGAN , MCMAHAN KEVIN W , JEFFREY SCOTT LEBEGUE , RONNIE RAY PENTECOST
IPC分类号： F23R3/42 , F02C7/28
CPC分类号： F01D9/023 , F05D2230/642 , F05D2250/43 , F05D2250/713
摘要： PROBLEM TO BE SOLVED: To provide combustor sections and transition ducts thereof which allow and accommodate thermal growth of the ducts.SOLUTION: Turbine systems 10 are provided. A turbine system comprises a transition duct comprising an inlet, an outlet, and a duct passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The duct passage includes an upstream portion and a downstream portion. The upstream portion extends from the inlet between an inlet end and an aft end. The downstream portion extends from the outlet between an outlet end and a head end. The turbine system further includes a joint coupling the aft end of the upstream portion and the head end of the downstream portion together. The joint is configured to allow movement of the upstream portion and the downstream portion relative to each other about or along at least one axis.
摘要翻译：要解决的问题：提供允许和适应管道的热生长的燃烧器部分和过渡管道。解决方案：提供涡轮机系统10。涡轮机系统包括过渡管道，该过渡管道包括入口，出口和在入口和出口之间延伸并且限定纵向轴线，径向轴线和切线轴线的管道通道。过渡管道的出口沿着纵向轴线和切线轴线从入口偏移。管道通道包括上游部分和下游部分。上游部分在入口端和后端之间从入口延伸。下游部分在出口端和头端之间从出口延伸。涡轮机系统还包括将上游部分的后端和下游部分的头端连接在一起的接头。所述接头构造成允许所述上游部分和所述下游部分围绕或沿着至少一个轴线相对于彼此移动。

95. 发明专利

JP2014122784A System for supplying fuel to combustor 审中-公开
标题翻译：燃料供应系统
公开(公告)号：JP2014122784A
公开(公告)日：2014-07-03
申请号：JP2013260722
申请日：2013-12-18
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： CHEN WEI , RICHARD MARTIN DICINTIO , KARIM HASAN , ILYA ALEXANDROVICH SLOBODYANSKIY
IPC分类号： F23R3/34 , F23R3/14 , F23R3/28
CPC分类号： F23R3/28 , F23R3/14 , F23R3/286 , F23R3/346
摘要： PROBLEM TO BE SOLVED: To provide a system for supplying fuel to a combustor, the system having a combustion chamber and a liner that circumferentially surrounds at least a portion of the combustion chamber.SOLUTION: A plurality of fuel nozzles are radially arranged across the combustor upstream from the combustion chamber to supply a swirling flow of the fuel into the combustion chamber. A first fuel injector downstream from the plurality of fuel nozzles provides fluid communication for the fuel to flow through the liner and into the combustion chamber. The first fuel injector is circumferentially clocked with respect to the swirling flow of the fuel in the combustion chamber.
摘要翻译：要解决的问题：为了提供一种用于向燃烧器供应燃料的系统，该系统具有周向围绕燃烧室的至少一部分的燃烧室和衬套。解决方案：多个燃料喷嘴沿着燃烧室径向布置在燃烧室的上游，以将燃料的旋流供应到燃烧室中。多个燃料喷嘴下游的第一燃料喷射器提供流体连通以使燃料流过衬套并进入燃烧室。第一燃料喷射器相对于燃烧室中的燃料的旋转流沿周向计时。

96. 发明专利

JP2014122624A Compressor casing assembly providing access to compressor blade sealing assembly 审中-公开
标题翻译：压缩机壳体组件提供压缩机叶片密封组件
公开(公告)号：JP2014122624A
公开(公告)日：2014-07-03
申请号：JP2013259697
申请日：2013-12-17
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： SANJI EKANAYAKE , SCIPIO ALSTON ILFORD , JOSEPH P RIZZO
IPC分类号： F04D29/52 , F01D25/24 , F02C7/28 , F04D19/02 , F04D29/16 , F04D29/64
CPC分类号： F04D29/60 , F01D11/08 , F01D11/14 , F01D11/24 , F01D25/24
摘要： PROBLEM TO BE SOLVED: To solve the problem of having to remove a midcompressor casing of a turbine engine in order to access a zero stage seal assembly of a compressor.SOLUTION: A compressor casing assembly 31 includes a forward compressor casing 22, a midcompressor casing 17, a removable cover 43 and a seal assembly 39. The midcompressor casing 17 is provided with a cavity adapted to receive the seal assembly 39, and a cover groove adapted to receive the removable cover 43. The removable cover secures the seal assembly 39.
摘要翻译：要解决的问题：为了解决必须移除涡轮发动机的中压缩机壳体以便进入压缩机的零级密封组件的问题。解决方案：压缩机壳体组件31包括正压缩机壳体22，中压缩机壳体中间压缩机壳体17设置有适于容纳密封组件39的空腔和适于容纳可移除盖43的盖槽。可移除盖固定密封组件39。

97. 发明专利

JP2014122623A Supercharged combined cycle system with air flow bypass to hrsg and fan 有权
标题翻译：超级联合循环系统与空气流旁路到HRSG和风扇
公开(公告)号：JP2014122623A
公开(公告)日：2014-07-03
申请号：JP2013259695
申请日：2013-12-17
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： SANJI EKANAYAKE , SCIPIO ALSTON ILFORD , TIMOTHY TAH-TEH YANG , JULIO ENRIQUE MESTRONI , KURT WALDNER , TEDD SELLERS
IPC分类号： F01D17/00 , F01K23/10 , F02C6/18 , F02C7/00
CPC分类号： F02C6/18 , F01D17/00 , F01K23/101 , F02C9/18 , F22B1/1815 , Y02E20/14 , Y02E20/16
摘要： PROBLEM TO BE SOLVED: To provide customers with a supercharged combined cycle system having sufficient system flexibility, output and efficiency over the system life cycle.SOLUTION: A supercharging system includes a forced draft fan 30 providing an air flow, and a prime mover 31 that drives the forced draft fan 30. A duct directs a first portion of the air flow to a gas turbine system, a main bypass subsystem diverts a second portion of the air flow to a heat recovery steam generator; and a drive bypass subsystem diverts a third portion of the air flow to the prime mover 31. The prime mover 31 may be one of an aeroderivative gas turbine, a gas turbine, a reciprocating engine, a steam turbine and an induction motor and a variable frequency drive.
摘要翻译：要解决的问题：为客户提供在系统寿命周期内具有足够的系统灵活性，输出和效率的增压联合循环系统。解决方案：增压系统包括提供气流的强制通风机30和原动机31，驱动强制通风扇30.管道将空气流的第一部分引导到燃气轮机系统，主旁通子系统将空气流的第二部分转移到热回收蒸汽发生器; 驱动旁路子系统将空气流的第三部分转移到原动机31.原动机31可以是航空燃气轮机，燃气轮机，往复式发动机，蒸汽涡轮机和感应电动机和变量变频器

98. 发明专利

JP2014122346A High thermal conductivity composite for electric insulation, and articles thereof 审中-公开
标题翻译：用于电绝缘的高导电性复合材料及其制品
公开(公告)号：JP2014122346A
公开(公告)日：2014-07-03
申请号：JP2013260720
申请日：2013-12-18
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： WEI TSANG
IPC分类号： C08L63/00 , C08K3/00 , C08L25/02 , C09D5/25 , C09D7/12 , C09D125/02 , C09D163/00
CPC分类号： H01B3/40 , Y10T428/31511
摘要： PROBLEM TO BE SOLVED: To provide a thermally conductive and electrically insulating composite composition.SOLUTION: The composite composition includes an epoxy resin and a filler. The epoxy resin has at least two epoxide groups per molecule, and a reactive diluent. The composite composition includes about 5 vol.% to about 20 vol.% of the filler, based on the total volume of the composite composition. An electrical component having a coating of the composite composition is also provided.
摘要翻译：要解决的问题：提供导热和电绝缘的复合组合物。解决方案：复合组合物包括环氧树脂和填料。环氧树脂每分子具有至少两个环氧基团和反应性稀释剂。基于复合组合物的总体积，复合组合物包含约5体积％至约20体积％的填料。还提供了具有复合组合物涂层的电气部件。

99. 发明专利

JP2014118973A Fuel routing system of gas turbine engine and method of routing fuel 有权
标题翻译：燃油涡轮发动机燃油路由系统及燃油燃料方法
公开(公告)号：JP2014118973A
公开(公告)日：2014-06-30
申请号：JP2013258769
申请日：2013-12-16
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： JAMES ARTHUR SIMMONS , SHINKLE WILLIAM RANDOLPH
IPC分类号： F02C9/46 , F02C9/00 , F23R3/00 , F23R3/28
CPC分类号： F02C9/263 , F02C7/22 , F02C7/222 , F02C7/228 , F02C9/28 , F02C9/34 , F05D2220/76
摘要： PROBLEM TO BE SOLVED: To provide a fuel routing system of a gas turbine engine and a method of routing fuel.SOLUTION: A fuel routing system 30 of a gas turbine engine includes a primary fuel circuit 32 in communication with a fuel source 22 and a fuel distribution manifold 34. The fuel routing system 30 also includes a secondary fuel circuit extending from the primary fuel circuit 32 to a plurality of fuel nozzles 20 configured to direct fuel to a plurality of combustor chambers. The fuel routing system 30 further includes a main fuel flow control valve 43 disposed in the primary fuel circuit 32 for restricting the amount of fuel flowing to the fuel distribution manifold 34 upon removal of an electrical load operably coupled to the gas turbine. The fuel routing system 30 further includes a plurality of check valves 60 disposed between the secondary fuel circuit 50 and the primary fuel circuit 32 for restricting the amount of fuel flowing between the secondary fuel circuit 50 and the primary fuel circuit 32.
摘要翻译：要解决的问题：提供一种燃气涡轮发动机的燃料路由系统和一种路由燃料的方法。解决方案：燃气涡轮发动机的燃料路由系统30包括与燃料源22连通的主燃料回路32和燃料分配歧管34.燃料路由系统30还包括从主燃料回路32延伸到构造成将燃料引导到多个燃烧室的多个燃料喷嘴20的二次燃料回路。燃料路由系统30还包括设置在主燃料回路32中的主燃料流量控制阀43，用于在去除可操作地连接到燃气轮机的电负载时限制流向燃料分配歧管34的燃料量。燃料路由系统30还包括设置在二次燃料回路50和主燃料回路32之间的多个止回阀60，用于限制在二次燃料回路50和一次燃料回路32之间流动的燃料量。

100. 发明专利

JP2014115072A Fuel nozzle for combustor of gas turbine engine 有权
标题翻译：燃气涡轮发动机燃油喷嘴
公开(公告)号：JP2014115072A
公开(公告)日：2014-06-26
申请号：JP2013206019
申请日：2013-10-01
申请人： General Electric Co , ゼネラル・エレクトリック・カンパニイ
发明人： BELSOM KEITH CLETUS , MCMAHAN KEVIN WESTON , THOMAS LARRY LOU
IPC分类号： F23R3/28 , F02C7/22 , F23R3/32
CPC分类号： F02C7/222 , F23R3/286 , F23R3/32
摘要： PROBLEM TO BE SOLVED: To provide an improved fuel nozzle for a gas turbine, which is less complex and/or less expensive to manufacture than current designs while promoting flame stability, and/or while reducing undesirable emissions over a wide range of combustor operating levels.SOLUTION: A main body 72 of a fuel nozzle 70 for a gas turbine has an upstream end 78 axially separated from a downstream end 80, and at least partially defines a fuel supply passage 86 that extends through the upstream end 78 and at least partially through the main body 72. A fuel distribution manifold 74 is disposed at the downstream end 80 of the main body 78. The fuel distribution manifold 74 includes a plurality of axially extending passages 92 that extend through the fuel distribution manifold 74. A plurality of fuel injection ports 96 defines a flow path 98 between the fuel supply passage 86 and each of the plurality of axially extending passages 92.
摘要翻译：要解决的问题：提供一种用于燃气轮机的改进的燃料喷嘴，其在制造时比当前设计更不复杂和/或更便宜，同时提高火焰稳定性，和/或同时在较宽范围的燃烧器操作水平减少不期望的排放物解决方案：用于燃气轮机的燃料喷嘴70的主体72具有与下游端80轴向分离的上游端78，并且至少部分限定了延伸穿过上游端78并且至少部分地延伸的燃料供应通道86 燃料分配歧管74设置在主体78的下游端80处。燃料分配歧管74包括延伸穿过燃料分配歧管74的多个轴向延伸通道92.多个燃料注入口96限定了燃料供给通道86和多个轴向延伸通道92中的每一个之间的流动路径98。

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