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公开(公告)号：US20120090331A1
公开(公告)日：2012-04-19
申请号：US12906558
申请日：2010-10-18
IPC分类号： F02C7/22
CPC分类号： F02C7/22 , F02C3/22 , F02C9/40 , F05D2270/301 , F05D2270/303 , F23K5/00 , F23K2401/201 , F23N1/002 , F23N2021/10
摘要： Systems and methods for supplying fuel to a gas turbine are described. A fuel may be received, and one or more parameters associated with the received fuel may be determined. Based at least in part upon the determined one or more parameters, a desired pressure for removing one or more liquids from the fuel utilizing a separator may be calculated. The operation of a pressure changing device may then be controlled in order to achieve the desired pressure. In certain embodiments, the operations of the method may be performed by a controller that includes one or more computers.
摘要翻译： 描述了向燃气轮机供应燃料的系统和方法。 可以接收燃料，并且可以确定与所接收的燃料相关联的一个或多个参数。 至少部分地基于所确定的一个或多个参数，可以计算利用分离器从燃料中除去一种或多种液体的期望压力。 然后可以控制压力改变装置的操作以实现所需的压力。 在某些实施例中，该方法的操作可以由包括一个或多个计算机的控制器执行。
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公开(公告)号：US20110023491A1
公开(公告)日：2011-02-03
申请号：US12512527
申请日：2009-07-30
CPC分类号： F02C7/224 , F02C3/22 , Y10T137/2605
摘要： A system for supplying fuel to a gas turbine includes piping containing fuel at a pressure greater than approximately 500 psi. A pressure reducing valve connected downstream of the piping reduces the pressure of the fuel to less than approximately 200 psi. A heat exchanger connected downstream of the pressure reducing valve heats the wet saturated fuel or dry saturated fuel to produce a superheated fuel. A control valve connected downstream of the heat exchanger reduces the pressure of the superheated fuel to less than approximately 50 psi. A method for supplying superheated fuel to a gas turbine includes receiving fuel having a pressure greater than approximately 500 psi and reducing the pressure to less than approximately 200 psi. The method further includes separating gaseous fuel from liquid fuel, reducing the pressure of the gaseous fuel to less than approximately 50 psi, and flowing the superheated fuel to the gas turbine.
摘要翻译： 用于向燃气轮机供应燃料的系统包括在大于约500psi的压力下含有燃料的管道。 连接在管道下游的减压阀将燃料的压力降低到小于约200psi。 连接在减压阀下游的热交换器加热湿饱和燃料或干饱和燃料以产生过热燃料。 连接在热交换器下游的控制阀将过热燃料的压力降低到小于约50psi。 向燃气轮机供应过热燃料的方法包括接收压力大于约500psi并将压力降低到小于约200psi的燃料。 该方法还包括从气体燃料中分离出气体燃料，将气态燃料的压力降低到小于约50psi，并将过热燃料流入燃气轮机。
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公开(公告)号：US20090071118A1
公开(公告)日：2009-03-19
申请号：US11857746
申请日：2007-09-19
申请人： Jun F. Ma , Colin Wilkes
发明人： Jun F. Ma , Colin Wilkes
IPC分类号： F02C9/40
CPC分类号： F02C9/40 , F23L7/005 , F23N2021/10 , Y02E20/16
摘要： A method and system for modulating the Modified Wobbe Index (MWI) of a fuel is provided. A variety of industrial components, which may require a gas fuel, such as but not limiting of, a heavy-duty gas turbine; an aero-derivative gas turbine; or a boiler may utilize the method and system. The method and system may provide an industrial component comprising at least one steam injection system, wherein the at least one steam injection system injects steam into at least one fuel supply line upstream of a combustion system to modulate the MWI of at least one fuel. The method and system may also determine whether the MWI of the at least one fuel is outside of a predetermined range; and utilize the at least one steam injection system to automatically inject the steam at a flowrate for adjusting the MWI of the at least one fuel.
摘要翻译： 提供了用于调节燃料的改性沃泊指数（MWI）的方法和系统。 可能需要气体燃料的各种工业部件，例如但不限于重型燃气轮机; 航空导向燃气轮机; 或者锅炉可以利用该方法和系统。 该方法和系统可以提供包括至少一个蒸汽喷射系统的工业部件，其中至少一个蒸汽喷射系统将蒸汽喷射到燃烧系统上游的至少一个燃料供应管线中，以调节至少一种燃料的MWI。 所述方法和系统还可以确定所述至少一种燃料的MWI是否在预定范围之外; 并且利用所述至少一个蒸汽喷射系统以用于调节所述至少一种燃料的MWI的流量自动喷射蒸汽。
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4.发明授权Systems and methods for gas fuel delivery with hydrocarbon removal utilizing active pressure control and dew point analysis 有权采用主动压力控制和露点分析方法，采用碳氢化合物排放进行气体燃料输送的系统和方法公开(公告)号：US08850818B2
公开(公告)日：2014-10-07
申请号：US12906558
申请日：2010-10-18
CPC分类号： F02C7/22 , F02C3/22 , F02C9/40 , F05D2270/301 , F05D2270/303 , F23K5/00 , F23K2401/201 , F23N1/002 , F23N2021/10
摘要： Systems and methods for supplying fuel to a gas turbine are described. A fuel may be received, and one or more parameters associated with the received fuel may be determined. Based at least in part upon the determined one or more parameters, a desired pressure for removing one or more liquids from the fuel utilizing a separator may be calculated. The operation of a pressure changing device may then be controlled in order to achieve the desired pressure. In certain embodiments, the operations of the method may be performed by a controller that includes one or more computers.
摘要翻译： 描述了向燃气轮机供应燃料的系统和方法。 可以接收燃料，并且可以确定与所接收的燃料相关联的一个或多个参数。 至少部分地基于所确定的一个或多个参数，可以计算利用分离器从燃料中除去一种或多种液体的期望压力。 然后可以控制压力改变装置的操作以实现所需的压力。 在某些实施例中，该方法的操作可以由包括一个或多个计算机的控制器执行。
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公开(公告)号：US07055395B2
公开(公告)日：2006-06-06
申请号：US10219331
申请日：2002-08-16
申请人： Colin Wilkes
发明人： Colin Wilkes
IPC分类号： G01F1/00
摘要： A method for detecting and controlling the elemental sulfur deposition on pressure reducing gas fuel control valves in cases where the sulfur deposition results from a temperature drop during expansion across the control valve, such as that encountered in gas turbine engines. The control method and algorithm according to the invention uses measured parameters of gas flow rate, pressure and temperature, combined with known pressure reducing valve characteristics to first determine whether sulfur deposition has occurred, and thereafter to calculate a valve position control parameter used to control the gas temperature upstream of the control valve, thereby maintaining the sulfur in a vapor phase through the pressure reducing process and preventing subsequent sulfur deposition on the valve and downstream piping.
摘要翻译： 在诸如在燃气涡轮发动机中遇到的控制阀膨胀过程中由于温度下降导致硫沉积的情况下，在减压气体燃料控制阀上检测和控制元素硫沉积的方法。 根据本发明的控制方法和算法使用气体流量，压力和温度的测量参数，结合已知的减压阀特性来首先确定是否发生硫沉积，然后计算用于控制的阀位置控制参数 控制阀上游的气体温度，从而通过减压过程将硫保持在气相中，并防止随后的硫沉积在阀和下游管道上。
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公开(公告)号：US06820427B2
公开(公告)日：2004-11-23
申请号：US10318922
申请日：2002-12-13
申请人： Colin Wilkes
发明人： Colin Wilkes
IPC分类号： F02C322
CPC分类号： F02C9/00
摘要： A method for operating a turbine is provided. The method includes supplying working fluid to a first flow path input and routing the fluid through a heating unit coupled in flow communication to the flow path between first flow path input and the turbine. The method also includes extracting a portion of the working fluid from first flow path at a point intermediate the heating unit and an inlet of the turbine. The method further includes re-circulating the extracted fluid through a second flow path such that the extracted fluid is discharged upstream from the heating unit.
摘要翻译： 提供了一种用于操作涡轮机的方法。 该方法包括将工作流体提供给第一流路输入并将流体通过流动连通的加热单元路由到第一流路输入和涡轮之间的流动路径。 该方法还包括在加热单元和涡轮机的入口之间的点处从第一流动路径提取一部分工作流体。 该方法还包括使提取的流体再循环通过第二流动路径，使得提取的流体从加热单元的上游排出。
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公开(公告)号：US4958488A
公开(公告)日：1990-09-25
申请号：US339449
申请日：1989-04-17
申请人： Colin Wilkes , Hukam C. Mongia , Peter C. Tramm
发明人： Colin Wilkes , Hukam C. Mongia , Peter C. Tramm
摘要： An external combustion system for a stationary gas turbine engine includes a rich zone combustor, a water or steam quench stage, a lean zone combustor and a dilution stage. Fuel such as natural gas or liquid hydrocarbon, which forms no ash or slag, burns in a primary air supply in the rich zone combustor at an equivalence ratio exceeding 1 which inhibits rapid formation of of oxides of nitrogen. The effluent from the rich zone combustor is a stream of combustible gas including carbon monoxide and hydrogen. The combustible gas stream is quenched in the quench stage and mixed with a secondary supply of compressed air in the lean zone combustor. The combustible gas ignites spontaneously in the lean zone combustor and burns at an equivalence ratio of less than 1 and at a temperature below the range characterized by rapid formation of oxides of nitrogen. The discharge from the lean zone combustor is a stream of hot gas motive fluid which is diluted in the dilution stage and introduced into the turbine section of the engine.
摘要翻译： 用于固定燃气涡轮发动机的外部燃烧系统包括富燃烧室，水或蒸汽骤冷段，贫区燃烧室和稀释段。 不形成灰分或渣的天然气或液体烃等燃料在富燃烧室中的一次空气供应中以等于1的当量比燃烧，抑制氮气的快速形成。 来自富区燃烧器的流出物是包括一氧化碳和氢气的可燃气体流。 可燃气体流在淬火阶段淬火，并与贫区燃烧器中的二次压缩空气供应混合。 可燃气体在稀区燃烧器中自发点燃，并以小于1的当量比和低于以氮气氧化物形成为特征的温度的温度燃烧。 来自贫区燃烧室的排放物是在稀释级中稀释并引入发动机的涡轮部分的热气体动力流。
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公开(公告)号：US4313300A
公开(公告)日：1982-02-02
申请号：US113635
申请日：1980-01-21
申请人： Colin Wilkes , Bruce W. Gerhold
发明人： Colin Wilkes , Bruce W. Gerhold
摘要： The quantity of NOx emissions generated by a combined gas turbine-steam boiler power plant is controlled by recycling a controlled amount of the steam boiler exhaust gas to the air compressor of the gas turbine such that the recycled gases constitutes up to about 30% of the fluid flowing through the air compressor and by cooling the recycled steam boiler exhaust gases to about the desired gas turbine compressor inlet temperature prior to its introduction into the air compressor.
摘要翻译： 由燃气轮机 - 蒸汽锅炉发电厂组合产生的氮氧化物排放量是通过将受控量的蒸汽锅炉废气再循环到燃气轮机的空气压缩机来控制的，因此循环气体构成高达30％ 流经空气压缩机的流体和在再循环的蒸汽锅炉排放气体被引入空气压缩机之前将其冷却到大约所需的燃气轮机压缩机入口温度。
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公开(公告)号：US4292801A
公开(公告)日：1981-10-06
申请号：US56510
申请日：1979-07-11
申请人： Colin Wilkes , Milton B. Hilt
发明人： Colin Wilkes , Milton B. Hilt
CPC分类号： F23R3/34 , F05D2270/082 , F05D2270/31 , F23D2209/10
摘要： An improved dual stage-dual mode combustor capable of reduced emissions of nitrogen oxide from a combustion turbine is disclosed. The combustor includes two combustion chambers separated by a throat region. Fuel is initially introduced and ignited in the first chamber. Thereafter, fuel is introduced near the downstream end of the first chamber for ignition and burning in the second chamber. Burning in the first chamber is extinguished by shifting the fuel flow to burning in the second chamber and after termination of the flame in the first chamber, fuel is reintroduced into the first chamber for premixing only with burning in the second chamber. By selectively controlling the percentage of fuel introduced into the first stage, low emissions of nitrogen oxide are realized.
摘要翻译： 公开了一种能够减少来自燃气轮机的氮氧化物排放的改进的双级双模燃烧器。 燃烧器包括由喉部区域分开的两个燃烧室。 燃料最初被引入并在第一室中点燃。 此后，在第一室的下游端附近引入燃料，以在第二室中点燃和燃烧。 通过将燃料流转移到第二室中的燃烧并且在第一室中的火焰终止之后燃烧在第一室中，燃料再次被引入到第一室中，以便仅在第二室中燃烧进行预混合。 通过选择性地控制引入第一阶段的燃料的百分比，实现了氮氧化物的低排放。
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公开(公告)号：US4255927A
公开(公告)日：1981-03-17
申请号：US920191
申请日：1978-06-29
申请人： Robert H. Johnson , Colin Wilkes
发明人： Robert H. Johnson , Colin Wilkes
CPC分类号： F23R3/26 , F05B2200/15
摘要： A combustion system for gas turbines is disclosed which is capable of burning gaseous and liquid fuels. Excess air injected into the reaction zone of the combustor produces either a fuel-lean or fuel-rich mixture which lowers the temperature at which combustion occurs and thereby reduces the amount of nitrogen oxides in the turbine exhaust. Efficient combustion is maintained across a wide range of turbine loads by means of a control mechanism disposed externally of the combustor, which directs the airflow from the compressor to the reaction zone and to the downstream dilution zone respectively in a manner which permits variable, inverse proportioning of the air supplied to these zones. The variation in the pressure drop across the combustor is maintained within acceptable limits throughout the full load range.
摘要翻译： 公开了一种能够燃烧气体和液体燃料的用于燃气轮机的燃烧系统。 喷射到燃烧器的反应区域中的过量空气产生贫燃料或富含燃料的混合物，其降低燃烧发生的温度，从而减少涡轮机废气中的氮氧化物的量。 通过设置在燃烧器外部的控制机构在宽范围的涡轮机负载下保持有效的燃烧，其将气流从压缩机引导到反应区和下游稀释区，其方式允许可变的反比例 供应给这些区域的空气。 在整个负载范围内，跨燃烧器的压降的变化保持在可接受的范围内。
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