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71. 发明公开

EP2136051A3 Power augmentation system for a gas turbine 有权
标题翻译：一个燃气涡轮机的功率放大系统
公开(公告)号：EP2136051A3
公开(公告)日：2010-12-22
申请号：EP09006909.7
申请日：2009-05-22
申请人： Gas Turbine Efficiency Sweden AB
发明人： Bland, Robert
IPC分类号： F02C7/057 , F02C7/143
CPC分类号： F02C7/057 , F02C3/305 , F02C7/1435
摘要： A fluid delivery skid with a pre-fill system for supplying fluid has one or more stages including a first valve and a second valve, each having an open and closed position. The stages have active and inactive states to provide a desired flow rate of fluid to an apparatus for distribution of the fluid. In an active state, fluid is received in the stage and pressurized with the first valve open and the second valve closed. Further, in an active state, fluid is released with the first valve closed and the second open. In an inactive state, at least the second valve is closed. A control unit is connected to a pump unit and controls operation of the pump to regulate the stages to supply pressure at a level determined to achieve the desired flow rate.

72. 发明公开

EP2211039A2 Methods and device for augmenting power output of a gas turbine plant 审中-公开
标题翻译： Verfahren und Vorrichtung zurErhöhungder Leistung eines Gasturbinenkraftwerks
公开(公告)号：EP2211039A2
公开(公告)日：2010-07-28
申请号：EP10151145.9
申请日：2010-01-20
申请人： General Electric Company
发明人： Wilkes, Kevin Wood , Snider, David August , Hannula, Scott Victor , Rosson, Randy Scott
IPC分类号： F02C3/30 , F02C6/16 , F02C7/143 , F02C7/16
CPC分类号： F02C6/16 , F02C3/24 , F02C3/305 , F02C7/143 , F02C7/16 , H02P9/04 , Y02E60/15
摘要： Systems and methods for augmenting power output of a turbine(10) during a transient event are provided. A cooling substance may be provided and at least a portion of the cooling substance may be directed to a compressor inlet (22) of the turbine (10) for a predefined time in order to augment power output of the turbine.
摘要翻译：提供了用于在瞬态事件期间增加涡轮（10）的功率输出的系统和方法。可以提供冷却物质，并且冷却物质的至少一部分可以被引导到涡轮机（10）的压缩机入口（22）预定的时间，以便增加涡轮的功率输出。

73. 发明公开

EP2196652A2 Gas turbine base load control by chilling modulation 审中-公开
标题翻译： Gasturbine Grundlast Kontrolle durch Modulation derKühlung
公开(公告)号：EP2196652A2
公开(公告)日：2010-06-16
申请号：EP09177606.2
申请日：2009-12-01
申请人： General Electric Company
发明人： Feher, Peter , Motakef, Abbas
IPC分类号： F02C7/057 , F02C7/143 , F02C9/16
CPC分类号： F02C7/057 , F02C7/143 , F02C9/16
摘要： A control system (100) for a base load output of a gas turbine engine. The control system (100) may include an inlet chilling coil system (210) for providing air to the gas turbine engine (110) at a desired temperature, a temperature control valve (260) in communication with the inlet chilling coil system (210), a temperature sensor (290) positioned about the gas turbine engine (110), and a temperature controller (270) in communication with the temperature control valve (260) and the temperature sensor (290). The temperature controller (270) modulates the temperature control valve (260) until the air provided to the gas turbine engine (110) by the inlet chilling coil system (210) reaches the desired temperature as sensed by the temperature sensor (290).
摘要翻译：一种用于燃气涡轮发动机的基本负载输出的控制系统（100）。控制系统（100）可以包括用于在期望温度下向燃气涡轮发动机（110）提供空气的入口冷却盘管系统（210），与入口冷却盘管系统（210）连通的温度控制阀（260），位于燃气涡轮发动机（110）周围的温度传感器（290）和与温度控制阀（260）和温度传感器（290）连通的温度控制器（270）。温度控制器（270）调节温度控制阀（260），直到由入口冷却盘管系统（210）提供到燃气涡轮发动机（110）的空气达到由温度传感器（290）感测到的期望温度。

74. 发明公开

EP2067964A3 Radial staging method and configuration of a liquid injection system for power plants 有权转让
标题翻译：系统和方法，用于燃气涡轮机的流体注射
公开(公告)号：EP2067964A3
公开(公告)日：2010-05-05
申请号：EP08105943.8
申请日：2008-12-05
申请人： Rolls-Royce Power Engineering PLC
发明人： Omielan, Walter Kasimierz , Taraboulsi, Gabriel , Harry, Chris Pin
IPC分类号： F02C7/143 , F04D29/70
CPC分类号： F02C7/1435 , F02C3/30 , F02C3/305 , F04D29/5846 , F04D29/705 , F05D2260/212 , F05D2270/16
摘要： A turbine power plant employs a radial staging of a liquid injection system to provide a uniform fluid distribution, for use in wet compression. The liquid injection system includes a hub to be coupled to an air intake case of a turbine power plant. An annular ring assembly is spaced radially outwardly from the hub. Spray bars are spoked about the hub and the annular ring. The spray bars each include a body portion having an inner end coupled to the hub and an outer end coupled to the ring assembly. The spray bars each have at least two nozzle assemblies along the body portion. The spray bars each define at least two liquid supply manifolds each having an inlet at the annular ring assembly and an outlet at an associated nozzle assembly. The liquid supply manifolds each supply liquid to one or more associated nozzle assemblies.

75. 发明授权

EP1138955B1 Method and apparatus for increasing the efficiency of a multi-stage compressor 无效
标题翻译：方法和装置用于增加多级压缩机的效率
公开(公告)号：EP1138955B1
公开(公告)日：2010-05-05
申请号：EP01302620.8
申请日：2001-03-21
申请人： Watson Cogeneration Company
发明人： Ingistov, Steve
IPC分类号： F04D29/58 , F04D29/70 , F02C7/143 , F01D25/00
CPC分类号： F04D29/701 , F02C7/1435 , F04D29/5846 , F04D29/705 , Y02T50/675

76. 发明公开

EP1903188A3 System and method for augmenting turbine power output 有权
标题翻译：系统和方法，以增加涡轮机的输出
公开(公告)号：EP1903188A3
公开(公告)日：2009-11-25
申请号：EP07017397.6
申请日：2007-09-05
申请人： Gas Turbine Efficiency Sweden AB
发明人： Wagner, Thomas , Cesar, Carlos
IPC分类号： F01D25/00 , F02C3/30 , F02C7/143 , F02C9/16 , F01D5/28 , F02C7/04 , F02C7/232
CPC分类号： F02C7/04 , F01D25/002 , F01D25/007 , F01D25/305 , F02C3/305 , F02C7/1435 , F02C7/232 , F05D2260/602 , F05D2260/607 , Y02T50/675
摘要： A method and system augments shaft output of gas turbine engines that can be used in multiple modes of operation. The system comprises a washing unit capable of injecting atomized water into the gas turbine engine, thereby obtaining a release of fouling material from the at least one compressor blade; and at least one water injection unit capable of injecting atomized water into the air stream of the gas turbine engine's inlet duct or at the gas turbine, under the control of a computational fluid dynamic model, in order to increase a mass flow of said air flow, wherein the power output from said gas turbine engine can be augmented.

77. 发明公开

EP2082959A2 System and method for improving jet aircraft operating efficiency 有权
标题翻译：提高喷气飞机运行效率的系统和方法
公开(公告)号：EP2082959A2
公开(公告)日：2009-07-29
申请号：EP09150886.1
申请日：2009-01-19
申请人： Honeywell International Inc.
发明人： Dwyer, Michael D., Honeywell International Inc. , Wessels, Richard F., Honeywell International Inc. , Hollingsworth, D. R., Honeywell International Inc.
IPC分类号： B64D11/02 , F02C3/30 , F02C7/143 , F02C3/24
CPC分类号： B64D11/02 , F02C3/24 , F02C3/30 , F02C3/305 , F02C7/1435 , F05D2210/13 , F05D2220/60 , F05D2260/602 , Y02T50/46 , Y02T50/671 , Y02T50/675
摘要： A disposal system is provided. In an embodiment, by way of example, the disposal system can include a first tank (22) adapted to be at least partially filled with waste fluid. The disposal system can also include a waste processing device (28) adapted to receive waste fluid and adjust one or more properties of the waste fluid. Additionally, the waste disposal system can include a jet engine (38) comprising a first chamber adapted to contain a fluid undergoing compression. The jet engine can be in fluid communication with the waste processing device to receive the waste fluid from the waste processing device.
摘要翻译：提供处置系统。在一个实施例中，举例来说，处理系统可以包括适于至少部分地填充有废液的第一箱（22）。处理系统还可以包括废物处理装置（28），其适于接收废弃流体并调整废弃流体的一种或多种性质。另外，废物处理系统可以包括喷气发动机（38），该喷气发动机（38）包括适于容纳经受压缩的流体的第一室。喷气发动机可以与废物处理装置流体连通以从废物处理装置接收废物流体。

78. 发明授权

EP1740806B1 Verfahren zum kontinuierlichen Betreiben einer Flüssigkeitsfördervorrichtung 失效转让
标题翻译：一种用于连续操作的流体处理设备处理
公开(公告)号：EP1740806B1
公开(公告)日：2009-06-03
申请号：EP05747785.3
申请日：2005-04-06
申请人： Alstom Technology Ltd
发明人： JIMENEZ HÄRTEL, Carlos , OESTERLE, Stefan , REUMSCHÜSSEL, Carsten , SAVIC, Sasha
IPC分类号： F02C3/30 , F02C7/143 , F04B41/06 , F25B5/02 , F04D15/02
CPC分类号： F04D29/5846 , F02C3/30 , F04B23/06
摘要： The invention relates to a method for operating a transport device (120) and to a transport device (120) for continuously transporting a liquid. The method and the transport device (120) are particularly suitable for use in a water injection installation (126) for injecting water into the primary flow (107) of a gas turbine (100). The transport device (120) comprises a plurality of transport units (FE1, FE2, FE3, FE4, FE5) that are connected in parallel. In a first method step (11), the transport units (FE1, FE2, FE3, FE4, FE5) of the transport device (120) are assigned to at least two transport unit groups (FG1, FG2). Said transport unit groups (FG1, FG2) and their assigned respective transport units (FE1, FE2, FE3, FE4, FE5) are then activated in rolling succession at intervals from an idle mode in order to transport the volumetric flow of liquid (method step 13). During each interval at least one transport unit is thus switched to idle mode in rolling succession. The invention enables the service life of the transport units of the transport device (120) to be extended.

79. 发明授权

EP1643575B1 FUEL CELL/CONSTANT PRESSURE TURBINE/HYBRID SYSTEM 有权
标题翻译：燃料电池/恒压涡轮 - / - 混合系统
公开(公告)号：EP1643575B1
公开(公告)日：2009-03-11
申请号：EP04746599.2
申请日：2004-06-29
申请人： KAWASAKI JUKOGYO KABUSHIKI KAISHA
发明人： TANAKA, Kazuo , HARADA, Eiichi; 690-32, , SHOJI, Takatoshi , KITAJIMA, Junichi , YAMASHITA, Seiji
IPC分类号： H01M8/04 , H01M8/00 , F02C6/00 , F02C7/143
CPC分类号： H01M8/04022 , F02C6/00 , F05D2220/60 , H01M8/0662 , H01M16/00

80. 发明公开

EP1566529A4 ATMOSPHERIC PRESSURE COMBUSTION TURBINE SYSTEM 有权
标题翻译：用燃烧的大气压力涡轮系统
公开(公告)号：EP1566529A4
公开(公告)日：2008-05-07
申请号：EP03751336
申请日：2003-10-03
申请人： KAWASAKI HEAVY IND LTD , NAT INST OF ADVANCED IND SCIEN
发明人： TANAKA KAZUO , YAMASHITA SEIJI , HARADA EIICHI , IKI NORIHIKO , TAKAHASHI SANYO , FURUTANI HIROHIDE
IPC分类号： F02C7/00 , F02C3/30 , F02C3/34 , F02C7/08 , F02C7/10 , F02C7/141 , F02C7/143 , F02C6/00
CPC分类号： F02C7/08 , F02C3/30 , F02C3/34 , F02C7/10 , F02C7/143 , F05D2220/60 , F05D2260/212 , Y02E20/14
摘要： An atmospheric pressure combustion turbine system suitable for recovering an energy from atmospheric pressure hot gas, comprising power generating equipment having a combustor (12) disposed on the former stage of the turbine (16) of turbo machinery formed of the turbine (16) and at least one of compressors (20, 24) and producing an axial output by passing the working fluid of the turbo machinery through the combustor (12), the turbine (16), and the compressors (20, 24) in that order, the power generating equipment further comprising a regenerative heat exchanger (14) performing the cooling of the hot working gas leaving the turbine (16) by exchanging heat with the mixed gas generated, mixing the outside air with exhaust gas, heating the mixture, and humidifying the mixture with hot water, at least one of coolers (22, 26) cooling the working gas by exchanging heat with water at the inlets of the compressors (20, 24), and a humidifier (30) mixing the introduced outside air with a part of the exhaust gas leaving the compressor (24), heating the mixture, and humidifying the working gas in the coolers (22, 26) by using the hot water obtained by the heat exchange with the working gas, wherein the mixed gas outputted from the humidifier (30) is led into the regenerative heat exchanger (14), and the hot humid mixed gas preheated by the heat exchange with the hot working gas at the outlet of the turbine (16) is led into the combustor (12).

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