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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
发明人： SCHMID, Günter , ECKERT, Helmut , TAROATA, Dan
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。
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2.发明公开GENERATING POWER USING AN ION TRANSPORT MEMBRANE 审中-公开STROMERZEUGUNG MIT EINER IONENTRANSPORTMEMBRAN
公开(公告)号：EP2593647A4
公开(公告)日：2017-05-17
申请号：EP11807536
申请日：2011-07-14
申请人： GTLPETROL LLC
发明人： ALLAM RODNEY J
IPC分类号： F02C3/20 , B01D59/30 , B01D61/38 , C01B13/02 , F02C3/30 , F02C6/06 , F02C6/10 , F02C6/18 , F02C7/00 , F02C7/22
CPC分类号： F02C7/22 , C01B13/0251 , C01B2203/84 , F02C3/28 , F02C3/30 , F02C6/06 , F02C6/10 , F02C6/18 , F02C7/00 , F05D2220/722 , F05D2220/75 , F05D2260/213 , F05D2270/20 , Y02E20/16 , Y02E20/18 , Y02E50/11 , Y02E50/12
摘要： A system may include a compressor, a heat exchanger and an ITM. The compressor is configured to receive an air stream and compress the air stream to generate a pressurized stream. The heat exchanger is configured to receive the pressured stream and indirectly heat the pressurized stream using heat from an oxygen stream from an Ion Transport Membrane (ITM). The ITM is configured to receive the heated pressurized stream and generate an oxygen stream and the non-permeate stream, wherein the non-permeate stream is passed to a gas turbine burner and the oxygen stream is passed to the heat exchanger.
摘要翻译： 系统可以包括压缩机，热交换器和ITM。 压缩机被构造成接收气流并压缩气流以产生加压流。 热交换器构造成接收加压流并利用来自离子迁移膜（ITM）的氧流的热量间接加热加压流。 ITM被配置为接收经加热的加压流并产生氧气流和非渗透物流，其中非渗透物流被传送到燃气涡轮机燃烧器并且氧气流被传送到热交换器。
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公开(公告)号：EP1717420B1
公开(公告)日：2014-10-22
申请号：EP05009519.9
申请日：2005-04-29
发明人： Renz, Ulrich Prof.
CPC分类号： F02C6/18 , F01K23/064 , F01K23/068 , F01K23/10 , F01K23/108 , F02C3/20 , F02C6/10 , F05D2220/72 , Y02E20/18 , Y02E20/344
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4.发明授权METHOD FOR OPERATION OF A COMBINED-CYCLE POWER PLANT WITH COGENERATION, AND A COMBINED-CYCLE POWER PLANT FOR CARRYING OUT THE METHOD 有权方法与热电联产和GUD电厂运行的GUD RAFTWERKS用于实施过程
公开(公告)号：EP2630342B1
公开(公告)日：2014-09-17
申请号：EP11763951.8
申请日：2011-10-03
CPC分类号： F01K23/101 , B01D1/26 , C02F1/041 , C02F1/16 , C02F2103/08 , F01K7/165 , F01K17/04 , F01K23/10 , F01K23/103 , F01K23/18 , F02C6/04 , F02C6/10 , F02C6/18 , Y02E20/14 , Y02E20/16 , Y02P70/34
摘要： The invention relates to a method for operation of a combined-cycle power plant with cogeneration, in which method combustion air is inducted in at least one gas turbine, is compressed and is supplied to at least one combustion chamber for combustion of a fuel, and the resultant exhaust gas is expanded in at least one turbine, producing work, and in which method the exhaust gas emerging from the at least one turbine is passed through a heat recovery steam generator in order to generate steam, which generator is part of a water-steam circuit with at least one steam turbine, a condenser, a feedwater tank and a feedwater pump, wherein heat is provided by extracting steam from the at least one steam turbine. In a method such as this, the electricity production is decoupled from the steam production in that in order to restrict the electricity production while the heat provided by means of steam extraction remains at a constant level, a portion of the inducted combustion air is passed through the at least one turbine to the heat recovery steam generator without being involved in the combustion of the fuel in the gas turbine, and in that this portion of the combustion air is used to operate at least one supplementary firing in the heat recovery steam generator.
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公开(公告)号：EP2483544A1
公开(公告)日：2012-08-08
申请号：EP10793305.3
申请日：2010-09-24
申请人： Sermenghi, Bruno
发明人： Sermenghi, Bruno
摘要： A thermal motor system comprises a combustion chamber connected to an accumulating chamber of the fluid produced by combustion by a control valve. A fluid actuator is driven by an operating fluid coming from the accumulating chamber. The combustion chamber has a fixed volume and does not contain elements moved by the fluid produced by combustion.
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公开(公告)号：EP1992811A3
公开(公告)日：2010-11-24
申请号：EP08251712.9
申请日：2008-05-15
IPC分类号： F02C6/08
CPC分类号： F02K5/02 , F02B61/00 , F02B65/00 , F02B73/00 , F02C3/13 , F02C5/00 , F02C6/10 , F02C6/12 , F05D2220/50 , F05D2220/76
摘要： A gas turbine engine (14) with a turbine (25) with an exhaust manifold (48) thereabout from which fluids can be transferred to the turbine and an air compressor (23) having an air transfer duct (30) extending therefrom so as to be capable to provide compressed air in that air transfer duct at one end thereof to the air intake (32) of an internal combustion engine (34) provided as an intermittent combustion engine. The air intake and an exhaust outlet (39) are each coupled to combustion chambers (35) therein and a rotatable output shaft (40) is also coupled to those combustion chambers for generating force. The exhaust outlet has an exhaust transfer duct (46) extending therefrom so as to have the intermittent combustion engine be capable to provide exhaust therefrom in that exhaust transfer duct at one end thereof, and the exhaust transfer duct being connected at an opposite end thereof to the exhaust manifold (48) to be capable of transferring intermittent combustion engine exhaust thereto. A method of generating force and electrical power uses such an engine combination.
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公开(公告)号：EP2203680A2
公开(公告)日：2010-07-07
申请号：EP08783280.4
申请日：2008-07-25
申请人： Wojak, Bodgan
发明人： Wojak, Bodgan
IPC分类号： F23C99/00 , B01D53/50 , B01D53/86 , B01D53/96 , F01K21/00 , F02C3/00 , F17D1/04 , F23G7/00 , F23K5/08 , F25J3/06
CPC分类号： C01B17/54 , C01B17/0473 , C01B17/74 , F02C6/10 , F02C6/18 , Y02A50/2327 , Y02A50/2328 , Y02E20/12 , Y02P20/129 , Y02P20/13 , Y02P20/131 , Y10T137/0318
摘要： A gas turbine topping device, which is disposed upstream of a steam-raising section, is used for generating power in the manufacture of sulphuric acid. A sulfur-burning combustor generates hot sulfur dioxide while a pressure-exchanging ejector mixes the hot combustion gases with a cooler gas (e.g. pressurized air, pressurized N 2 or recycled sulfur dioxide (SO 2 ) to form a mixed working gas having a temperature below the maximum allowable temperature (metallurgical limit) of the blades of the turbine. The turbine drives an oxygen compressor which supplies oxygen to a bubbling chamber which also receives S 8 to produce sulfur vapor for combustion. By using stoichiometric quantities, sulfur dioxide is delivered in requisite quantities to a sulfuric acid plant without any harmful emissions. Useful amounts of electrical power can thus be generated by the gas turbine topping device as well as the downstream steam turbine by harnessing the enormous amount of waste heat involved in the manufacture of sulfuric acid.
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公开(公告)号：EP2126316A2
公开(公告)日：2009-12-02
申请号：EP08870742.7
申请日：2008-03-27
申请人： Siemens AG
发明人： NILSSON, Ulf
IPC分类号： F02C7/224
摘要： A gas turbine engine (100) with - a compressor section (105), - a combustor section (106) comprising at least one combustor (107, 110), - a turbine section (112), - at least one gaseous fuel supply conduit (22) with an upstream section (23) and a downstream section (25) the downstream section (25) being connected to the combustor (107, 110) for delivering gaseous fuel and - a fuel booster located in the gaseous fuel supply conduit, the fuel booster (1) having a driving expander (9) with a driving fluid inlet (11) that is in flow connection with a compressed air outlet (116) of the gas turbine engine's compressor, for receiving compressed air and a driving fluid outlet (13) for discharging expanded air and a fuel compressor (17) with a low pressure fuel inlet (19) connected to the upstream section (23) of the gaseous fuel supply conduit (22) and a high pressure fuel outlet (21) connected to the downstream section (25) of the gaseous fuel supply conduit (22), characterised in that a heat exchanger (3) is present which is located such between the unexpanded driving fluid or the expanded driving fluid on the one side and the low pressure gaseous fuel or the high pressure gaseous fuel on the other side that a heat transfer between the air and the gaseous fuel is possible.
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10.发明公开Aircraft combination engines exhaust thrust recovery 有权Abgasschubrückgewinnung在Flugzeugkombinationstriebwerken
公开(公告)号：EP1992811A2
公开(公告)日：2008-11-19
申请号：EP08251712.9
申请日：2008-05-15
CPC分类号： F02K5/02 , F02B61/00 , F02B65/00 , F02B73/00 , F02C3/13 , F02C5/00 , F02C6/10 , F02C6/12 , F05D2220/50 , F05D2220/76
摘要： A gas turbine engine (14) with a turbine (25) with an exhaust manifold (48) thereabout from which fluids can be transferred to the turbine and an air compressor (23) having an air transfer duct (30) extending therefrom so as to be capable to provide compressed air in that air transfer duct at one end thereof to the air intake (32) of an internal combustion engine (34) provided as an intermittent combustion engine. The air intake and an exhaust outlet (39) are each coupled to combustion chambers (35) therein and a rotatable output shaft (40) is also coupled to those combustion chambers for generating force. The exhaust outlet has an exhaust transfer duct (46) extending therefrom so as to have the intermittent combustion engine be capable to provide exhaust therefrom in that exhaust transfer duct at one end thereof, and the exhaust transfer duct being connected at an opposite end thereof to the exhaust manifold (48) to be capable of transferring intermittent combustion engine exhaust thereto. A method of generating force and electrical power uses such an engine combination.
摘要翻译： 一种具有涡轮机（25）的燃气涡轮发动机（14），其具有排气歧管（48），流体可从该排气歧管传送到涡轮机;以及空气压缩机（23），其具有从其延伸的空气传送管道（30），以便 能够将该空气传输管道的一端处的压缩空气提供给设置为间歇式内燃机的内燃机（34）的进气口（32）。 空气入口和排气出口（39）各自联接到其中的燃烧室（35），并且可旋转的输出轴（40）也联接到那些燃烧室以产生力。 排气出口具有从其延伸的排气传送管道（46），以使得间歇式内燃机能够在其一端的那个排气传送管道中提供排气，并且排气传送管道在其另一端连接到 排气歧管（48）能够将间歇的内燃机排气传送到其上。 一种产生力和电力的方法使用这种发动机组合。
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