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1.发明授权公开(公告)号：US08843293B2
公开(公告)日：2014-09-23
申请号：US12330154
申请日：2008-12-08
申请人： Stefan Rofka , Andreas Rueter , Klaus Doebbeling , Martin Nicklas
发明人： Stefan Rofka , Andreas Rueter , Klaus Doebbeling , Martin Nicklas
CPC分类号： F02C9/54 , F05D2270/112 , F05D2270/303
摘要： With a method for controlling a gas turbine in a power plant, a multiplicity of operating lines for the gas turbine for different gas turbine inlet temperatures TIT or gas turbine exhaust temperatures TAT and positions of the compressor inlet guide vane cascade VIGV are specified as a function of the load. For minimizing the electricity production costs during operation switching can be optionally carried out between different operating lines during constant or varying power output of the power plant.
摘要翻译： 利用用于控制发电厂中的燃气轮机的方法，指定用于不同燃气轮机入口温度TIT或燃气轮机排气温度TAT的燃气轮机的多条操作管线和压缩机入口导叶叶栅级联VIGV的位置作为功能 的负载。 为了最小化操作期间的电力生产成本，可以可选地在发电厂的恒定或变化的功率输出期间在不同的操作线之间进行切换。
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2.发明申请METHOD FOR CONTROLLING A GAS TURBINE IN A POWER PLANT AND POWER PLANT FOR CARRYING OUT THE METHOD 有权用于控制发电厂和动力装置中的气体涡轮机的方法公开(公告)号：US20090150040A1
公开(公告)日：2009-06-11
申请号：US12330154
申请日：2008-12-08
申请人： Stefan Rofka , Andreas Rueter , Klaus Doebbeling , Martin Nicklas
发明人： Stefan Rofka , Andreas Rueter , Klaus Doebbeling , Martin Nicklas
IPC分类号： F02C9/00
CPC分类号： F02C9/54 , F05D2270/112 , F05D2270/303
摘要： With a method for controlling a gas turbine in a power plant, a multiplicity of operating lines for the gas turbine for different gas turbine inlet temperatures TIT or gas turbine exhaust temperatures TAT and positions of the compressor inlet guide vane cascade VIGV are specified as a function of the load. For minimizing the electricity production costs during operation switching can be optionally carried out between different operating lines during constant or varying power output of the power plant.
摘要翻译： 利用用于控制发电厂中的燃气轮机的方法，指定用于不同燃气轮机入口温度TIT或燃气轮机排气温度TAT的燃气轮机的多条操作管线和压缩机入口导叶叶栅级联VIGV的位置作为功能 的负载。 为了最小化操作期间的电力生产成本，可以可选地在发电厂的恒定或变化的功率输出期间在不同的操作线之间进行切换。
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公开(公告)号：US20120216546A1
公开(公告)日：2012-08-30
申请号：US13407168
申请日：2012-02-28
IPC分类号： F02C7/18
CPC分类号： F02C7/1435 , F01D15/10 , F01D25/32 , F02C3/30 , F02C3/305 , F02C7/057 , F05D2220/32 , F05D2220/76 , F05D2270/053
摘要： A method and apparatus for the operation of a gas turbine unit with an evaporative intake air cooling system in the intake air pathway, wherein the return water flow of the evaporative intake air cooling system is used for the cooling of components of the gas turbine unit and/or of a generator coupled to the gas turbine unit and/or of another element coupled to the gas turbine unit, and a gas turbine unit adapted to be operated using this method.
摘要翻译： 一种用于在进气通道中具有蒸发进气冷却系统的燃气轮机单元的操作的方法和装置，其中所述蒸发进气冷却系统的回水流被用于冷却所述燃气轮机单元的部件， 耦合到燃气涡轮机单元和/或耦合到燃气涡轮机单元的另一个元件的发电机，以及适于使用该方法操作的燃气轮机单元。
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公开(公告)号：US09803549B2
公开(公告)日：2017-10-31
申请号：US13407168
申请日：2012-02-28
CPC分类号： F02C7/1435 , F01D15/10 , F01D25/32 , F02C3/30 , F02C3/305 , F02C7/057 , F05D2220/32 , F05D2220/76 , F05D2270/053
摘要： A method and apparatus for the operation of a gas turbine unit with an evaporative intake air cooling system in the intake air pathway, wherein the return water flow of the evaporative intake air cooling system is used for the cooling of components of the gas turbine unit and/or of a generator coupled to the gas turbine unit and/or of another element coupled to the gas turbine unit, and a gas turbine unit adapted to be operated using this method.
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公开(公告)号：US07093450B2
公开(公告)日：2006-08-22
申请号：US10999990
申请日：2004-12-01
IPC分类号： F25D17/06
CPC分类号： F02C7/1435 , F04D29/5846 , F05D2260/212
摘要： In a method of operating a compressor, a gaseous medium is compressed in a first compressor stage. The partially compressed medium is sent from the first compressor stage into an intermediate cooler where it is cooled before being directed into the second compressor stage where it is compressed further. A liquid medium is sprayed into the gaseous medium in the intermediate cooler so that a two-phase mixture with a liquid phase and a gaseous phase is formed in the intermediate cooler. The liquid phase is separated again before adding it to the second compressor stage.
摘要翻译： 在操作压缩机的方法中，气态介质在第一压缩机级中被压缩。 部分压缩的介质从第一压缩机级被输送到中间冷却器中，在中间冷却器进入第二压缩机级之前将其冷却，在第二压缩机级中进一步被压缩。 将液体介质喷射到中间冷却器中的气体介质中，使得在中间冷却器中形成具有液相和气相的两相混合物。 将液相再次分离，然后再将其添加到第二压缩机级。
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公开(公告)号：US06708497B2
公开(公告)日：2004-03-23
申请号：US10183871
申请日：2002-06-28
IPC分类号： F02C330
CPC分类号： F01K21/047
摘要： The invention relates to a method of operating a gas turbine installation (1), compressed fresh air (6, 19, 38) is branched off after a compressor (2) and supplied to an evaporator device (14), in the evaporator device (14) feed water (17, 26, 28) is evaporated, while heat is supplied, and is mixed with the fresh air (6, 19, 38) in order to generate a steam/air mixture (22, 37), the steam/air mixture (22, 37) is fed back upstream of a gas turbine (10), the heat required for the evaporation of the feed water (17, 26, 28) is at least partially extracted from an exhaust gas (12) of the gas turbine (10). In order to improve the efficiency of the gas turbine installation (1), the feed water (17, 26, 28) runs down along a wall arrangement (39) heated by the exhaust gas (12) and is subjected to the fresh air (6, 19, 38). The feed water (17, 26, 28) evaporates and mixes with the fresh air (6, 19, 38), by which means the steam/air mixture (22, 37) forms for the recirculation.
摘要翻译： 本发明涉及一种操作燃气轮机装置（1）的方法，压缩的新鲜空气（6,39,38）在压缩机（2）之后被分流并供应到蒸发装置（14），在蒸发器装置 14）供水（17,26,28）蒸发，同时供应热量，并与新鲜空气（6,19,38）混合以产生蒸汽/空气混合物（22,37），蒸汽 /空气混合物（22,37）被馈送到燃气轮机（10）的上游，用于蒸发给水（17,26,28）所需的热量至少部分地从排气（12）排出 燃气轮机（10）。 为了提高燃气轮机装置（1）的效率，供水（17,26,28）沿着由排气（12）加热的壁装置（39）向下延伸并且经受新鲜空气（ 6，19，38）。 给水（17,26,28）蒸发并与新鲜空气（6,19,38）混合，由此形成用于再循环的蒸汽/空气混合物（22,37）。
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公开(公告)号：US06672863B2
公开(公告)日：2004-01-06
申请号：US10145780
申请日：2002-05-16
IPC分类号： F23D1446
CPC分类号： F23C9/00 , F23C7/002 , F23C2900/07002 , F23D11/402 , F23D17/002
摘要： In a premixing burner (1) for a gas turbine or hot-gas generation for the combustion of liquid or gaseous fuel, in which fuel is mixed with combustion air (9a, 9b) in a burner interior (14), is fed to a combustion chamber (3) and is burnt in this combustion chamber (3), stabilization in the part-load model is achieved in a simple and efficient way in that means (15) are provided which make it possible to recirculate hot exhaust gas (17) out of the combustion chamber (3) into the burner interior (14) and to stabilize the flame by means of selfignition processes. The means (15) are preferably a recirculation line which picks up hot exhaust gas (17) from the outer backflow zone (10) and feeds it to the burner interior (14) in the region of a burner tip (2) facing away from the combustion chamber (3), additional fuel (pilot fuel 21) being admixed with the exhaust gas (17) in the recirculation line upstream of the feed to the burner interior (14).
摘要翻译： 在用于燃气轮机或用于燃烧液体或气体燃料的燃气的预混合燃烧器（1）中，其中燃料与燃烧器内部（14）中的燃烧空气（9a，9b）混合，被供给到 燃烧室（3），并且在该燃烧室（3）中燃烧，部件负荷模型中的稳定性以简单有效的方式实现，因为提供了使得可以再循环热废气（17）的装置（15） ）从燃烧室（3）进入燃烧器内部（14）并通过自燃过程来稳定火焰。 装置（15）优选地是从外部回流区（10）拾取热废气（17）并在燃烧器尖端（2）的远离燃烧器端部（2）的区域中将其供给到燃烧器内部（14）的再循环管线。 燃烧室（3），附加燃料（引燃燃料21）与在燃烧器内部（14）的进料上游的再循环管线中的废气（17）混合。
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公开(公告)号：US20050252231A1
公开(公告)日：2005-11-17
申请号：US10999990
申请日：2004-12-01
CPC分类号： F02C7/1435 , F04D29/5846 , F05D2260/212
摘要： In a method of operating a compressor, a gaseous medium is compressed in a first compressor stage. The partially compressed medium is sent from the first compressor stage into an intermediate cooler where it is cooled before being directed into the second compressor stage where it is compressed further. A liquid medium is sprayed into the gaseous medium in the intermediate cooler so that a two-phase mixture with a liquid phase and a gaseous phase is formed in the intermediate cooler. The liquid phase is separated again before adding it to the second compressor stage.
摘要翻译： 在操作压缩机的方法中，气态介质在第一压缩机级中被压缩。 部分压缩的介质从第一压缩机级被输送到中间冷却器中，在中间冷却器进入第二压缩机级之前将其冷却，在第二压缩机级中进一步被压缩。 将液体介质喷射到中间冷却器中的气体介质中，使得在中间冷却器中形成具有液相和气相的两相混合物。 将液相再次分离，然后再将其添加到第二压缩机级。
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公开(公告)号：US20050028530A1
公开(公告)日：2005-02-10
申请号：US10894031
申请日：2004-07-20
IPC分类号： F02C9/34 , C10L3/00 , F02C3/22 , F02C7/228 , F02C9/40 , F23N5/00 , F23R3/28 , G01N33/00 , F02C9/00
CPC分类号： G01N21/359 , F02C3/22 , F02C9/40 , F23N5/003 , F23N2021/10 , G01N21/3504 , G01N33/225
摘要： Relevant fuel-gas properties (XG) are measured on an ongoing basis while a gas turbine group is operating. The C2+alkane content of the fuel gas is of particular interest in this context, since it has a significant influence on the ignitability of the fuel gas in the combustion chamber. The operating parameters of the gas turbine group are acted on directly as a function of the measured fuel-gas properties. In particular, in the case of the example of a gas turbine group with sequential combustion, the distribution of the fuel mass flows ({dot over (m)}EV, {dot over (m)}SEV) between the combustion chambers (4, 8) of the gas turbine group is varied. Furthermore, if there is provision for inert media, such as water or steam, to be introduced, it is possible for the mass flow of inert media ({dot over (m)}ST) to be controlled as a function of the measured fuel properties.
摘要翻译： 燃气轮机组正在运行时，持续测量相关的燃气特性（XG）。 在这种情况下，燃料气体的C2 +烷烃含量是特别有意义的，因为它对燃烧室中的燃料气体的可燃性具有显着的影响。 燃气轮机组的操作参数作为测量的燃料 - 气体性质的函数直接作用。 特别地，在具有顺序燃烧的燃气轮机组的实例的情况下，燃料质量的分布流动（{气点（mEV），气体燃烧室（4,8）之间的点（mSEV） 涡轮机组是不同的，此外，如果要提供诸如水或蒸汽的惰性介质，要引入惰性介质的质量流（{dot over（mST））作为 测量燃料性能。
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公开(公告)号：US07216486B2
公开(公告)日：2007-05-15
申请号：US10894031
申请日：2004-07-20
CPC分类号： G01N21/359 , F02C3/22 , F02C9/40 , F23N5/003 , F23N2021/10 , G01N21/3504 , G01N33/225
摘要： Relevant fuel-gas properties (XG) are measured on an ongoing basis while a gas turbine group is operating. The C2+alkane content of the fuel gas is of particular interest in this context, since it has a significant influence on the ignitability of the fuel gas in the combustion chamber. The operating parameters of the gas turbine group are acted on directly as a function of the measured fuel-gas properties. In particular, in the case of the example of a gas turbine group with sequential combustion, the distribution of the fuel mass flows ({dot over (m)}EV, {dot over (m)}SEV) between the combustion chambers (4, 8) of the gas turbine group is varied. Furthermore, if there is provision for inert media, such as water or steam, to be introduced, it is possible for the mass flow of inert media ({dot over (m)}ST) to be controlled as a function of the measured fuel properties.
摘要翻译： 在燃气轮机组运行的同时，持续地测量相关的燃料气体性质（X N G）。 在这种情况下，燃料气体的C 2 + C 2烷烃含量是特别有意义的，因为它对燃烧室中的燃料气体的可燃性具有显着的影响。 燃气轮机组的操作参数作为测量的燃料 - 气体性质的函数直接作用。 特别地，在具有顺序燃烧的燃气轮机组的示例的情况下，燃料质量的分布流动（{dot over（m）EV，{dot over（m SEV < 燃气轮机组的燃烧室（4,8）之间的距离变化，此外，如果设置要引入的惰性介质，例如水或蒸汽，则惰性物质流可能 作为测量的燃料性质的函数来控制介质（{dot over（m ST ST ））。
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