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1. 发明授权

EP2876289B1 Fan containment system for a gas turbine engine 有权转让
标题翻译：燃气涡轮发动机风扇安全系统
公开(公告)号：EP2876289B1
公开(公告)日：2016-03-30
申请号：EP14191261.8
申请日：2014-10-31
申请人： Rolls-Royce plc
发明人： Harper, Cedric Brett , Care, Ian Colin Deuchar , Reed, Julian Mark
IPC分类号： F02K3/06 , F01D21/04 , F01D11/12 , F01D21/10 , F01D25/24 , F02C7/05
CPC分类号： F02C7/05 , F01D11/122 , F01D21/04 , F01D21/045 , F01D21/10 , F01D25/246 , F02K3/06 , F05D2220/36

2. 发明公开

EP2787195A4 INTERNAL COMBUSTION ENGINE WITH SUPERCHARGER 审中-公开
标题翻译：与装载机内燃发动机
公开(公告)号：EP2787195A4
公开(公告)日：2015-12-30
申请号：EP12854363
申请日：2012-07-06
申请人： TOYOTA MOTOR CO LTD
发明人： SHIODA JUMPEI , KAKUTA YUSHI , SUGIYAMA MATSUYOSHI
IPC分类号： F02B39/16 , B60T17/02 , F01M13/00 , F02B39/14 , F02B67/04 , F04C18/344 , F04C29/00
CPC分类号： F01M3/00 , B60T17/02 , F01D21/10 , F01D25/002 , F01D25/18 , F01M13/00 , F01M13/028 , F01M13/0405 , F02B29/0406 , F02B39/14 , F02B39/16 , F02B67/04 , F02C6/12 , F02D41/0007 , F02D41/18 , F02D2250/08 , F02M25/06 , F02M26/05 , F02M26/06 , F02M26/10 , F02M26/15 , F02M26/23 , F04C18/3442 , F04C23/006 , F04C2210/1005 , F04C2210/14 , F04C2210/24 , F04C2220/10 , F05D2220/40

3. 发明公开

EP2848776A3 Compressor blade monitoring system 审中-公开
标题翻译：压缩机叶片监控系统
公开(公告)号：EP2848776A3
公开(公告)日：2015-03-25
申请号：EP14184199.9
申请日：2014-09-10
申请人： General Electric Company
发明人： Yu, Lijie , Ansari, Adil , Badami, Vivek Venugopal , Bliss, John Thomas , Chadha, Rahul , Gupta, Rajan
IPC分类号： F01D21/00 , F01D21/14 , F01D17/00 , F01D17/02 , F01D17/04 , F01D17/06 , F01D17/08 , F01D21/10 , F02C9/00 , G05B23/02
CPC分类号： F04D27/001 , F01D21/00 , F01D21/003 , F01D21/04 , F01D21/10 , F01D21/14 , F02C9/00 , F03D17/00 , F04D29/324 , F05D2260/80 , F05D2260/81 , G01B7/14 , G01B11/14 , G01B21/16 , G01D21/00 , G06F17/40 , G06F19/00
摘要： A system 2 including: at least one computing device 120 configured to monitor a compressor blade 10 in a turbomachine 5 by: extracting time of arrival (TOA) data about the compressor blade 10 at a defined interval; correlating turbomachine operating conditions with the TOA data; extracting resonance data about the compressor blade 10 during startup or shutdown of the turbomachine 5, and extracting static deflection and tip clearance data about the compressor blade 10 during steady state operation of the turbomachine 5; creating a baseline compressor blade comparison level based upon the extracted resonance data, extracted static deflection and tip clearance data, and correlation between the turbomachine operating conditions and the TOA data; and iteratively extracting updated TOA data and performing the correlating, the extracting of the resonance data, static deflection and tip clearance data using the updated TOA data at the defined interval to create an updated baseline compressor blade comparison level.
Corresponding computer program product with a program code executed by such a computing device.
摘要翻译：系统2包括：至少一个计算装置120，配置成通过以下步骤监测涡轮机5中的压缩机叶片10：以限定的时间间隔提取关于压缩机叶片10的到达时间（TOA）数据; 将涡轮机操作条件与TOA数据相关联; 在涡轮机械5的启动或关闭期间提取关于压缩机叶片10的共振数据，并且在涡轮机械5的稳态操作期间提取关于压缩机叶片10的静态偏转和尖端间隙数据; 基于提取的共振数据，提取的静态偏转和尖端间隙数据以及涡轮机操作条件与TOA数据之间的相关性来创建基线压缩机叶片比较水平; 以及在所定义的时间间隔处使用更新的TOA数据迭代地提取更新的TOA数据并且执行关联，共振数据的提取，静态偏转和尖端间隙数据以创建更新的基线压缩机叶片比较水平。具有由这种计算设备执行的程序代码的相应的计算机程序产品。

4. 发明公开

EP2069200A2 INSTRUMENTED COMPONENT FOR USE IN AN OPERATING ENVIRONMENT 审中-公开
标题翻译： INSTRUMENTIERTE KOMPONENTE ZUR VERWENDUNG IN EINER BETRIEBSUMGEBUNG
公开(公告)号：EP2069200A2
公开(公告)日：2009-06-17
申请号：EP07872572.8
申请日：2007-07-24
申请人： Siemens Energy, Inc. , Roesch, Edward, R.
发明人： MITCHELL, David, J. , KULKARNI, Anand, A. , SUBRAMANIAN, Ramesh
IPC分类号： B64C27/00 , C23C28/04 , F01D17/02 , G01D3/08 , C04B35/00 , F01D21/00 , F23R3/00 , G01H11/08 , G08C17/02 , H01L41/187
CPC分类号： C23C28/321 , B33Y70/00 , C23C28/3215 , C23C28/34 , C23C28/341 , C23C28/345 , C23C28/3455 , F01D5/288 , F01D17/02 , F01D21/003 , F01D21/10 , F05D2230/90 , F05D2300/611 , F23R3/007 , G01D3/08 , H04Q9/00 , H04Q2209/40 , H04Q2209/50 , Y02T50/673
摘要： An instrumented component (18, 19) for use in various operating environments such as the hot gas path section of a combustion turbine engine (10). The component (18, 19) may have a substrate, a sensor (50, 204, 210) connected with the substrate for sensing a condition of the component (18, 19) within the casing during operation of the combustion turbine (10) and a connector (52, 202) attached to the substrate and in communication with the sensor (50, 204, 210) for routing a data signal from the sensor (50, 204, 210) to a termination location (53). The component (18, 19) may include a wireless telemetry device (54, 202) in communication with the connector (52, 202) for wirelessly transmitting the data signal outside the casing. A transceiver (56) may be located outside the casing for receiving the data signal and transmitting it to a processing module (30) for developing information with respect to a condition of the component (18, 19) or a coating (26) deposited on the component (18, 19).
摘要翻译：一种用于各种操作环境（例如燃气涡轮发动机（10）的热气路径部分））的仪表部件（18,19）。组件（18,19）可以具有衬底，与衬底连接的传感器（50,204,210），用于在燃气轮机（10）的操作期间感测壳体内部件（18,19）的状态，以及连接器（52,202），其连接到所述基板并与所述传感器（50,204,210）通信，用于将数据信号从所述传感器（50,204,210）路由到终止位置（53）。组件（18,19）可以包括与连接器（52,202）通信的无线遥测设备（54,202），用于在壳体外部无线地传输数据信号。收发器（56）可以位于外壳外部，用于接收数据信号并将其发送到处理模块（30），用于相对于组件（18,19）或沉积在其上的涂层（26）的状态显影信息组件（18,19）。

5. 发明公开

EP1418312A2 Turbine blade oxidation monitoring and life prediction using neural network based diagnostic techniques in conjunction with pyrometer signals 有权
标题翻译： Verfahren zurOxidationsüberwachungeiner Turbinenschaufel，das Pyestersignale verwendet
公开(公告)号：EP1418312A2
公开(公告)日：2004-05-12
申请号：EP03257005.3
申请日：2003-11-05
申请人： GENERAL ELECTRIC COMPANY
发明人： Choi, Sukhwan
IPC分类号： F01D21/00 , F01D21/10 , F01D21/12 , G01J5/00
CPC分类号： F01D21/003 , F01D21/10 , F01D21/12 , F01D21/14 , G01J5/0022
摘要： Oxidation of turbine buckets may cause unexpected and expensive turbine failures. Turbine bucket oxidation condition may be estimated to predict remaining useful bucket life during operation of a turbine by processing time-varying temperature distributions measured with a pyrometer of at least one rotating turbine bucket.
摘要翻译：涡轮机桶的氧化可能导致意外和昂贵的涡轮机故障。可以估计涡轮机桶氧化条件，以通过处理用至少一个旋转涡轮机桶的高温计测量的随时间变化的温度分布来预测涡轮运行期间的剩余有用的桶寿命。

6. 发明公开

EP3351327A1 PORTABLE JIG AND FIXTURE FOR PRECISION MACHINING 有权转让
公开(公告)号：EP3351327A1
公开(公告)日：2018-07-25
申请号：EP18151782.2
申请日：2018-01-16
申请人： General Electric Company
发明人： HUTH, Robert Edward , CLARK, Jason Matthew
IPC分类号： B23B47/28 , B23Q9/00
CPC分类号： B23B47/28 , B23B2215/76 , B23P2700/13 , B23Q9/0042 , F01D5/025 , F01D5/026 , F01D21/04 , F01D21/045 , F01D21/06 , F01D21/10 , F01D21/14 , F01D25/285 , F02C3/04 , F02C3/14 , F02C6/12 , F02C7/22 , F04D29/522 , F04D29/644 , F05D2220/32 , F05D2220/40 , F05D2230/10 , F05D2230/14 , F05D2230/237 , F05D2230/238 , F05D2240/35 , F05D2260/311 , F23R2900/00018 , F23R2900/00019
摘要： A portable jig and fixture (80) having at least one base plate (82), a column assembly (83) removably coupled to the at least one base plate (82), a slide assembly (100) removably coupled to the column assembly (83), a power feed head (104) removably coupled to the slide assembly (100), and a spindle unit (108) removably coupled with the slide assembly (100) having a motor (112) removably engaged it. At least one cutter assembly (120) is removably engaged with the spindle unit (108) and at least one drill jig (130) is also removably engaged with the spindle unit (108). Also, a turbomachine (10) having complementary structure (70) on the compressor discharge casing (21) can engage with the at least one base plate alignment mounting structure (72) on the portable jig and fixture (80).

7. 发明公开

EP3102886A1 METHOD FOR MONITORING A COMBUSTOR 审中-公开
标题翻译： VERFAHREN ZURÜBERWACHUNGEINER BRENNKAMMER
公开(公告)号：EP3102886A1
公开(公告)日：2016-12-14
申请号：EP15700533.1
申请日：2015-01-06
申请人： Siemens Aktiengesellschaft
发明人： BULAT, Ghenadie , HEADLAND, Paul
IPC分类号： F23N5/16 , F23N5/24 , F23R3/00 , F01D21/00 , F01D21/10 , F01D21/12 , G01N29/07
CPC分类号： F01D21/10 , F02C7/30 , F23D2208/10 , F23D2900/00016 , F23N5/16 , F23N5/242 , F23R3/00 , F23R2900/00004 , G01N29/04 , G01N29/07 , G01N2291/0258 , G01N2291/044 , G01N2291/102
摘要： A method for monitoring a combustor (30) comprising the steps: - measuring several times a distance between a first wall of the combustor (30) and either a second wall of the combustor (30) or a sensor of the combustor (30) by means of the sensor, and - concluding from a variation in the distances - a formation of deposit (84) on the first and/or second wall and/or sensor, and/or - a temperature change within the combustor (30), and/or - a pressure change within the combustor (30).
摘要翻译：一种用于监测燃烧器（30）的方法，包括以下步骤： - 通过以下步骤测量所述燃烧器（30）的第一壁与所述燃烧器（30）的第二壁或所述燃烧器（30）的传感器之间的距离传感器的装置，以及 - 从距离的变化得出 - 在第一和/或第二壁和/或传感器上形成沉积物（84）和/或 - 在燃烧器（30）内的温度变化，以及 /或 - 在燃烧器（30）内的压力变化。

8. 发明授权

EP2224379B1 Turbine blade monitoring 有权转让
标题翻译： Turbinenschaufelüberwachung
公开(公告)号：EP2224379B1
公开(公告)日：2015-04-08
申请号：EP10154090.4
申请日：2010-02-19
申请人： General Electric Company
发明人： Lee, Dongjai
IPC分类号： G06K19/077 , G01N29/22 , F01D25/00
CPC分类号： G06K19/07749 , F01D17/02 , F01D21/003 , F01D21/04 , F01D21/10 , F01D21/14 , F05D2220/31 , F05D2260/80 , G01N29/14 , G01N2291/2693

9. 发明公开

EP2818908A1 Endoscope system 有权转让
标题翻译：内窥镜系统
公开(公告)号：EP2818908A1
公开(公告)日：2014-12-31
申请号：EP13183761.9
申请日：2013-09-10
申请人： Olympus Corporation
发明人： Konomura, Yutaka , Kobayashi, Eiichi , Hori, Fumio
IPC分类号： G02B23/24 , F01D5/00 , F01D25/00 , G01N21/954
CPC分类号： G02B23/2476 , F01D5/12 , F01D21/10 , F01D25/285 , G01M15/14 , G01N21/954 , G02B23/2492 , Y02T50/671
摘要： An endoscope system 1 includes an endoscope 2 having an insertion portion 11 provided with an observation optical system that inspects a plurality of blades RB and SV that are periodically disposed at a periphery of a rotary shaft AR of a rotor of an engine E, and rotate around the rotary shaft AR, a guide tube 21 that is introduced into the engine E, and guides the insertion portion 11, a first fixing portion 23 or 25 that is provided at the guide tube 21 and fixes the guide tube 21 in an inside of the engine E, and a second fixing portion 24 that is provided in a position separated by having a predetermined distance from the first fixing portion 23 or 25 in the guide tube 21, and fixes the guide tube 21 with an outer jacketing cover S of the engine E.
摘要翻译：内窥镜系统1具备内窥镜2，该内窥镜2具有插入部11，该插入部11具备观察光学系统，该观察光学系统对周期性地配置在发动机E的转子的旋转轴AR周围的多个叶片RB，SV进行旋转在旋转轴AR的周围配置有导入管21，该导入管21导入到发动机E内并引导插入部11;第1固定部23或25，其设置在导向管21上，将导向管21固定在内部发动机E以及第二固定部24，该第二固定部24设置在与引导管21中的第一固定部23或25隔开预定距离的位置处，并且将引导管21固定在引导管21的外护套盖S上引擎E.

10. 发明授权

EP1388656B1 Steam turbine with an extraneous matter removing system 有权
标题翻译：汽轮机与系统去除异物
公开(公告)号：EP1388656B1
公开(公告)日：2013-12-25
申请号：EP03017470.0
申请日：2003-08-01
申请人： Mitsubishi Heavy Industries Compressor Corporation
发明人： Hata, Satoshi
IPC分类号： F01D21/10 , F01D25/00 , F02C7/30 , F01D9/06
CPC分类号： F01D25/002 , F01D21/10

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