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1. 发明授权

EP2940258B1 TURBINE DEVICE, AND WASTE HEAT RECOVERY POWER GENERATION SYSTEM INCLUDING SAME 有权转让
公开(公告)号：EP2940258B1
公开(公告)日：2018-11-28
申请号：EP13868327.1
申请日：2013-12-20
申请人： POSCO
发明人： JANG, Tae-In , KWEON, Yong-Hun , JEE, Chang-Woon , KIM, Jung-Kuk
IPC分类号： F01K25/10 , F01D15/10 , F01D25/16 , F16C32/04 , F01K7/16 , F01K13/00 , F22B1/18
CPC分类号： F01K7/16 , F01D15/10 , F01D25/16 , F01K13/00 , F05D2220/62 , F05D2220/64 , F05D2240/515 , F16C32/04 , F16C2360/00 , F22B1/18
摘要： Provided are a turbine device and a waste heat recovery power generation system including same. According to the present invention, a mechanical (contact) type bearing structure is replaced with a contactless electromagnetic bearing so as to extend the lifespan of a turbine and increase power generation efficiency. The use of waste heat can be facilitated, and the operation of the device can be maintained stably through the improvement of a structure of a disk means and an appropriate arrangement of a mechanical bearing means.

2. 发明公开

EP3356230A1 DISPOSITIF DE DÉGIVRAGE POUR LÈVRE D'ENTRÉE D'AIR DE NACELLE DE TURBORÉACTEUR D'AÉRONEF 审中-公开
公开(公告)号：EP3356230A1
公开(公告)日：2018-08-08
申请号：EP16787496.5
申请日：2016-09-29
申请人： Safran Nacelles
发明人： MAALIOUNE, Hakim , GONIDEC, Patrick , RAMI, Jean-Paul
IPC分类号： B64D15/02 , F02C6/18 , F02C7/047 , F02C7/14 , F01D25/02 , B64D15/06
CPC分类号： F02C7/047 , B64D15/02 , B64D15/04 , B64D15/06 , B64D33/02 , B64D2033/0233 , F01D25/02 , F02C6/18 , F02C7/14 , F05D2220/32 , F05D2220/323 , F05D2220/62 , F05D2260/208 , Y02T50/672 , Y02T50/675
摘要： The invention relates to a device (10) for de-icing an air intake lip (12) of an aircraft turbojet engine nacelle (14), the device (10) comprising a de-icing circuit in which a heat transfer fluid (22) circulates, said heat transfer fluid working in a two-phase form, the circuit comprising at least one device (26) for circulating the heat transfer fluid (22) in the de-icing circuit, a system (28) for heating the heat transfer fluid (22) and which is intended to change the phase of said fluid to a vapour phase, and an inlet conduit (30), for the heat transfer fluid (22), which opens into the lip (12) through the rear wall (18) in order to inject the vapour phase fluid (22) into the lip (12), the fluid changing phase when it condenses on the front wall (16) of the lip (12) to de-ice the lip (12).

3. 发明公开

EP3321491A1 ELECTRICALLY BOOSTED REGENERATIVE BLEED AIR SYSTEM 有权转让
标题翻译：电力提升再生式空气净化系统
公开(公告)号：EP3321491A1
公开(公告)日：2018-05-16
申请号：EP17201611.5
申请日：2017-11-14
申请人： Hamilton Sundstrand Corporation
发明人： HIMMELMANN, Richard A. , TONGUE, Stephen E.
IPC分类号： F02C6/08 , F02C7/32
CPC分类号： F02C6/08 , B64D13/06 , B64D15/04 , B64D2013/0618 , B64D2013/0648 , F02C7/32 , F05D2220/323 , F05D2220/62 , F05D2220/76 , F05D2270/06
摘要： An engine bleed air system (60) for providing air to an aircraft system includes a port (62) for extracting bleed air from a compressor section of an engine. The system additionally includes a turbo-generator (64) having a turbine (82) and a generator (84). The generator (84) is driven by rotation of the turbine (82). A boost compressor (66) is fluidly coupled to the port (62). Bleed air from the port (62) is selectively provided to one of the turbo-generator (64) and the boost compressor (66) based on a demand of the aircraft system.
摘要翻译：用于向飞机系统提供空气的发动机引气系统（60）包括用于从引擎的压缩机部分引出引气的端口（62）。该系统还包括具有涡轮机（82）和发电机（84）的涡轮发电机（64）。发电机（84）通过涡轮机（82）的旋转而被驱动。增压压缩机（66）流体联接到端口（62）。基于飞机系统的需求，将来自端口（62）的排气选择性地提供给涡轮发电机（64）和增压压缩机（66）中的一个。

4. 发明公开

EP3315735A1 SYSTEM FOR HIGHER PLANT EFFICIENCY 有权
标题翻译：系统提高工厂效率
公开(公告)号：EP3315735A1
公开(公告)日：2018-05-02
申请号：EP17194390.5
申请日：2017-10-02
申请人： General Electric Company
发明人： ZHANG, Hua , HU, Iris
IPC分类号： F01K9/02 , F01K13/02 , F01K9/00
CPC分类号： F01K23/101 , F01K3/185 , F01K7/16 , F01K9/003 , F01K9/023 , F01K13/02 , F01N5/02 , F02C6/18 , F05D2220/31 , F05D2220/32 , F05D2220/62 , F05D2220/72 , F05D2270/3061 , Y02E20/16
摘要： A steam cycle system 44 includes a heat recovery steam generator HRSG 46 which receives exhaust gases, a steam turbine coupled to the HRSG 46 which receives a first steam flow generated by the HRSG, and a condenser 50 which condenses a second steam flow output by the steam turbine. The condenser 50 includes a plurality of heat exchanger tubes 62, a fan 52, and a steam collection header 60. The system includes one or more sensors 54 which measure one or more properties of the steam flow. The system includes a closed-loop controller 58 communicatively coupled to the one or more sensors 54. The controller 58 receives data from the one or more sensors 54, determines a flow rate of the second steam flow through the steam header using the one or more sensors 54, calculates whether the flow rate of the steam is within a threshold, and adjusts one or more operating parameters of the fan 52.
摘要翻译：蒸汽循环系统44包括接收排气的热回收蒸汽发生器HRSG 46，联接到HRSG 46的蒸汽涡轮，该蒸汽涡轮接收由HRSG产生的第一蒸汽流，以及冷凝器50，其冷凝由第二蒸汽流输出的第二蒸汽流汽轮机。冷凝器50包括多个热交换器管62，风扇52和蒸汽收集集管60.该系统包括一个或多个传感器54，其测量蒸汽流的一个或多个特性。该系统包括通信地耦合到一个或多个传感器54的闭环控制器58.控制器58从一个或多个传感器54接收数据，使用一个或多个传感器54确定通过蒸汽集管的第二蒸汽流量传感器54计算蒸汽的流量是否在阈值内，并且调整风扇52的一个或多个操作参数。

5. 发明公开

EP3249196A1 AN ENERGY FLOW OF AN ADVANCED ENVIRONMENTAL CONTROL SYSTEM 有权转让
标题翻译：先进的环境控制系统的能量流动
公开(公告)号：EP3249196A1
公开(公告)日：2017-11-29
申请号：EP17172830.6
申请日：2017-05-24
申请人： Hamilton Sundstrand Corporation
发明人： Bruno, Louis J. , Hipsky, Harold W.
IPC分类号： F02C1/02 , F02C6/08 , B64D13/06
CPC分类号： B64D13/02 , B64D13/08 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , F02C1/02 , F02C6/08 , F05D2220/323 , F05D2220/62
摘要： An airplane is provided. The airplane includes a compressing device including a turbine (213) and a compressor (212). The turbine includes first and second inlets and provides energy by expanding one or more mediums. The first inlet is receives a first medium of the one or more mediums. The second inlet receives a second medium of the one or more mediums. The compressor receives a first energy derived from the first and second mediums being expanded across the turbine during a first mode of the compressing device, receives a second energy derived from the first medium being expanded across the turbine during a second mode of the compressing device, and compresses the second medium in accordance with the first mode or the second mode.
摘要翻译：提供飞机。该飞机包括包括涡轮机（213）和压缩机（212）的压缩装置。涡轮机包括第一和第二入口并通过扩展一个或多个介质来提供能量。第一入口接收一种或多种介质中的第一介质。第二入口接收一种或多种介质中的第二介质。在压缩装置的第一模式期间，压缩机接收从在涡轮机上扩张的第一和第二介质获得的第一能量，在压缩装置的第二模式期间接收从在涡轮机上膨胀的第一介质获得的第二能量，并按照第一模式或第二模式压缩第二媒体。

6. 发明公开

EP3219940A1 COMBINED CYCLE POWER PLANT AND METHOD FOR OPERATING SUCH A COMBINED CYCLE POWER PLANT 有权转让
标题翻译：联合循环发电厂和操作这种联合循环发电厂的方法
公开(公告)号：EP3219940A1
公开(公告)日：2017-09-20
申请号：EP16161150.4
申请日：2016-03-18
申请人： General Electric Technology GmbH
发明人： Couzzi-Carneiro, Mariah , Dietzmann, Joerg
IPC分类号： F01K17/02 , F01K23/10
CPC分类号： F01K23/106 , F01D15/10 , F01K7/16 , F01K17/025 , F01K23/10 , F02C3/04 , F05D2220/32 , F05D2220/62 , H02K7/1823 , Y02E20/16
摘要： The invention relates to a water/steam system (1) for a combined cycle power plant, comprising a heat recovery steam generator (4) providing a flue gas stream path (6) for extracting heat from a flue gas stream (9) exhausted from a gas turbine, the heat recovery steam generator (4) having a low pressure section (3) including a low pressure evaporator (13) arranged along the flue gas stream path (6) for generating low pressure steam at a low pressure input level (p 10 ) for a main input (54) of a low pressure steam turbine (51). Furthermore, the invention relates to a method for operating such a water/steam system (1). In order to use heat a low temperatures, the present invention provides that in the low pressure section () additionally sub low pressure steam at a sub low pressure level (p 11 ) below the low pressure level (p 10 ) is generated by means of a sub low pressure evaporator (23) in the flue gas stream path (6).
摘要翻译：本发明涉及用于联合循环动力装置的水/蒸汽系统（1），其包括热回收蒸汽发生器（4），该热回收蒸汽发生器提供烟气流路径（6），用于从烟气流（9）燃气轮机，所述热回收蒸汽发生器（4）具有低压部分（3），所述低压部分包括沿所述烟气流路径（6）布置的低压蒸发器（13），用于产生低压输入水平的低压蒸汽 p10）用于低压蒸汽轮机（51）的主输入（54）。此外，本发明涉及一种用于操作这种水/蒸汽系统（1）的方法。为了在低温下使用热量，本发明规定，在低压段（P10）中，另外通过副产生低于低压水平（p10）的次低压水平（p11）的低压低压蒸汽低压蒸发器（23）在烟气流路径（6）中。

7. 发明公开

EP3177565A1 KRAFTWERK ZUR HERSTELLUNG VON ENERGIE UND AMMONIAK 审中-公开
公开(公告)号：EP3177565A1
公开(公告)日：2017-06-14
申请号：EP15767449.0
申请日：2015-09-11
申请人： Siemens Aktiengesellschaft
发明人： SCHMID, Günter , ECKERT, Helmut , TAROATA, Dan
IPC分类号： C01C1/04 , B01J19/24 , B01J19/26 , B01J4/00 , B01J8/00 , B05B17/00 , C01C1/02 , C01B21/06
CPC分类号： C01C1/026 , B01J19/245 , B01J19/26 , B01J2208/00902 , C01B21/061 , C01B21/0612 , C01C1/02 , F01D15/10 , F02C6/10 , F05D2220/31 , F05D2220/62 , Y02E20/14 , Y02P20/129
摘要： The invention relates to a method for producing ammonia and energy, in which an electropositive metal that is selected from the alkali metals, the alkaline earth metals, aluminium and zinc, as well as mixtures and/or alloys of same, is atomised and/or sprayed and is combusted with a reaction gas that comprises nitrogen, the reacted mixture of reaction gas and electropositive metal being mixed with water and/or an aqueous solution and/or suspension of a hydroxide of said electropositive metal. The invention also relates to a device for carrying out said method.
摘要翻译：本发明涉及一种生产氨和能量的方法，其中选自碱金属，碱土金属，铝和锌以及其混合物和/或合金的正电性金属被雾化和/或喷涂并用包含氮的反应气体燃烧，反应气体和正电性金属的反应混合物与水和/或所述正电金属的氢氧化物的水溶液和/或悬浮液混合。本发明还涉及用于执行所述方法的设备。

8. 发明公开

EP3123003A4 COMBINED CYCLE GAS TURBINE PLANT 有权
标题翻译： GAS-UND-DAMPF-KOMBIKRAFTWERK
公开(公告)号：EP3123003A4
公开(公告)日：2017-05-03
申请号：EP15768271
申请日：2015-03-27
申请人： MITSUBISHI HITACHI POWER SYS , MITSUBISHI HITACHI POWER SYSTEMS EUROPE LTD
发明人： YOKOYAMA YOSHIYUKI , MARTINEZ JOSE MANUEL , RUBIO ELVIO , RATIA PABLO
IPC分类号： F01K23/10 , F01K23/12 , F01K23/16
CPC分类号： F01K23/10 , F01K5/02 , F01K7/345 , F01K23/101 , F01K23/16 , F02C3/04 , F02C9/42 , F05D2210/13 , F05D2220/31 , F05D2220/32 , F05D2220/62 , H02K7/1823 , Y02E20/16
摘要： This combined cycle gas turbine plant has a gas turbine (104) and a steam turbine (106) mounted on the same shaft. A control system is configured for switching the plant from a rated mode of operation, in which the plant is operated on gas turbine output and steam turbine output, to a reduced load mode of operation, in which the plant is operated on gas turbine output alone. The switch from the rated mode of operation to the reduced load mode of operation occurs if plant demand decreases below a predetermined threshold. The steam turbine is run under full speed no load conditions in the reduced load mode of operation, and is heated using controlled steam admission, to maintain the steam turbine in a heated ‘stand-by’ state.
摘要翻译：该联合循环燃气轮机装置具有安装在同一轴上的燃气轮机（104）和蒸汽轮机（106）。控制系统被配置用于将设备从其中设备在燃气轮机输出和蒸汽轮机输出上操作的额定操作模式切换到减负载操作模式，其中设备仅在燃气轮机输出上操作。如果工厂需求降低到预定阈值以下，则从额定运行模式切换到减负荷运行模式。蒸汽轮机在减负荷运行模式下在全速无负荷条件下运行，并且使用受控的蒸汽进入来加热蒸汽轮机，以使蒸汽轮机保持处于加热“备用”状态。

9. 发明公开

EP3002431A1 ENGINE BLEED AIR SYSTEM 有权转让
标题翻译： ZAPFLUFTSYSTEM EINES TRIEBWERKS
公开(公告)号：EP3002431A1
公开(公告)日：2016-04-06
申请号：EP15187401.3
申请日：2015-09-29
申请人： Hamilton Sundstrand Corporation
发明人： BRUNO, Louis J. , DEFRANCESCO, Gregory L. , ZYWIAK, Thomas M. , DREW, Diane G. , HIPSKY, Harold W. , HUGHES, Daniel L.
IPC分类号： F02C6/08 , B64D13/04 , B64D13/06 , B64D13/08 , F01C1/02 , F02C9/18
CPC分类号： F02C9/18 , B64D13/06 , B64D2013/0618 , B64D2013/0648 , F02C6/08 , F02C6/12 , F05D2220/62 , F05D2260/213 , F05D2260/606 , Y02T50/56 , Y02T50/675
摘要： An engine bleed air system (3) has one or more taps in the compressor section of an aircraft engine, for example a low pressure tap (19) and a high pressure tap (20). The low pressure tap (19) is fluidly connected to the compressor (21) of a turbo-compressor and the high pressure tap (20) is fluidly connected to the turbine (22) of the turbo-compressor. A bypass line (30) connects the high pressure air to the outlet (32) of the compressor (21), with a heat exchanger (31) used to remove excess heat from the bypass line (30). An additional heat exchanger (37) is used to remove any excess heat from the compressed air, dumping the heat to a fan stream (33) or to the expanded air exiting the turbine (22). The system is controlled to minimize the amount of high pressure air extracted from the engine.
摘要翻译：发动机排气系统（3）在飞行器发动机的压缩机部分中具有一个或多个抽头，例如低压抽头（19）和高压抽头（20）。低压龙头（19）流体地连接到涡轮压缩机的压缩机（21），并且高压龙头（20）流体地连接到涡轮压缩机的涡轮机（22）。旁通管路（30）将高压空气连接到压缩机（21）的出口（32），其中热交换器（31）用于从旁路管线（30）去除多余的热量。使用另外的热交换器（37）来从压缩空气中除去多余的热量，将热量倾倒到风扇流（33）或离开涡轮机（22）的膨胀空气中。控制系统以最小化从发动机提取的高压空气的量。

10. 发明公开

EP2940258A4 TURBINE DEVICE, AND WASTE HEAT RECOVERY POWER GENERATION SYSTEM INCLUDING SAME 有权转让
标题翻译：涡轮机设备和系统的发电，以余热回收
公开(公告)号：EP2940258A4
公开(公告)日：2016-01-13
申请号：EP13868327
申请日：2013-12-20
申请人： POSCO
发明人： JANG TAE-IN , KWEON YONG-HUN , JEE CHANG-WOON , KIM JUNG-KUK
IPC分类号： F01K25/10 , F01D15/10 , F01D25/16 , F01K7/16 , F01K13/00 , F16C32/04
CPC分类号： F01K7/16 , F01D15/10 , F01D25/16 , F01K13/00 , F05D2220/62 , F05D2220/64 , F05D2240/515 , F16C32/04 , F16C2360/00 , F22B1/18
摘要： Provided are a turbine device and a waste heat recovery power generation system including same. According to the present invention, a mechanical (contact) type bearing structure is replaced with a contactless electromagnetic bearing so as to extend the lifespan of a turbine and increase power generation efficiency. The use of waste heat can be facilitated, and the operation of the device can be maintained stably through the improvement of a structure of a disk means and an appropriate arrangement of a mechanical bearing means.

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