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    • 2. 发明申请
    • Method and apparatus for actuating fuel trim valves in a gas turbine
    • 用于在燃气轮机中启动燃油调节阀的方法和装置
    • US20050097895A1
    • 2005-05-12
    • US10704302
    • 2003-11-10
    • Vasanth KothnurMohamed AliDaniel VandaleMatthew Roberts
    • Vasanth KothnurMohamed AliDaniel VandaleMatthew Roberts
    • F02C7/22F02C7/228F02C9/28F23N1/00F23N5/10F23R3/34F23R3/46F02C9/00
    • F23R3/34F02C7/222F02C7/228F02C9/28F05D2270/0831F05D2270/303F23N1/002F23N5/102F23N2035/12F23N2037/02F23R3/46
    • The gas turbines of the present invention have multiple combustion chambers, and within each chamber are multiple fuel nozzles. Each nozzle has its own fuel control valve to control the fuel flowing to the nozzles. To minimize the pressure drop through the fuel control valves, multiple manifolds are employed. Each manifold supplies at least one fuel nozzle in multiple combustion chambers with fuel. The fuel control valves are mounted on the manifolds such that the weight of the fuel control valves and nozzles are carried by the manifolds, not the multiple combustion chambers. A plurality of thermocouples for measuring exhaust gas from said multiple combustion chambers are employed to sense gas exhaust temperature. In carrying out the methods of the present invention for tuning a gas turbine, it is essential to note that the most efficient gas turbine is one which has the least nitrous oxides, the least amount of unburned hydrocarbons, and the least amount of carbon monoxide for a specified energy output. In order to tune the gas turbine to accomplish these objectives, it is desirable that each combustion chamber in the gas turbine be well balanced relative to the remaining combustion chambers. It is an aim of the present invention to tune each of the multiple combustion chambers such that no specific combustion chamber is rich or lean, and all are operating within about 1% of the remaining combustion chambers.
    • 本发明的燃气轮机具有多个燃烧室,并且在每个室内都有多个燃料喷嘴。 每个喷嘴都有自己的燃料控制阀,以控制流向喷嘴的燃料。 为了最小化通过燃料控制阀的压降,采用多个歧管。 每个歧管在具有燃料的多个燃烧室中提供至少一个燃料喷嘴。 燃料控制阀安装在歧管上,使得燃料控制阀和喷嘴的重量由歧管而不是多个燃烧室承载。 用于测量来自所述多个燃烧室的废气的多个热电偶用于感测排气温度。 在执行用于调谐燃气轮机的本发明的方法时,必须注意的是,最有效的燃气轮机是具有最少一氧化二氮,最少量的未燃碳氢化合物和最少量的一氧化碳的燃气轮机 指定能量输出。 为了调整燃气轮机以实现这些目的,期望燃气涡轮机中的每个燃烧室相对于剩余的燃烧室均衡良好。 本发明的目的是调节多个燃烧室中的每个,使得没有特定的燃烧室是富的或者是贫的,并且都在剩余的燃烧室的大约1%的范围内运行。
    • 6. 发明申请
    • METHOD AND APPARATUS FOR ACTUATING FUEL TRIM VALVES IN A GAS TURBINE
    • 用于在燃气涡轮机中执行燃料三元阀的方法和装置
    • US20070125088A1
    • 2007-06-07
    • US11670542
    • 2007-02-02
    • Vasanth KothnurMohamed AliDaniel VandaleMatthew Roberts
    • Vasanth KothnurMohamed AliDaniel VandaleMatthew Roberts
    • F02C9/26
    • F23R3/34F02C7/222F02C7/228F02C9/28F05D2270/0831F05D2270/303F23N1/002F23N5/102F23N2035/12F23N2037/02F23R3/46
    • The gas turbines of the present invention have multiple combustion chambers, and within each chamber are multiple fuel nozzles. Each nozzle has its own fuel control valve to control the fuel flowing to the nozzles. To minimize the pressure drop through the fuel control valves, multiple manifolds are employed. Each manifold supplies at least one fuel nozzle in multiple combustion chambers with fuel. The fuel control valves are mounted on the manifolds such that the weight of the fuel control valves and nozzles are carried by the manifolds, not the multiple combustion chambers. A plurality of thermocouples for measuring exhaust gas from said multiple combustion chambers are employed to sense gas exhaust temperature. In carrying out the methods of the present invention for tuning a gas turbine, it is essential to note that the most efficient gas turbine is one which has the least nitrous oxides, the least amount of unburned hydrocarbons, and the least amount of carbon monoxide for a specified energy output. In order to tune the gas turbine to accomplish these objectives, it is desirable that each combustion chamber in the gas turbine be well balanced relative to the remaining combustion chambers. It is an aim of the present invention to tune each of the multiple combustion chambers such that no specific combustion chamber is rich or lean, and all are operating within about 1% of the remaining combustion chambers.
    • 本发明的燃气轮机具有多个燃烧室,并且在每个室内都有多个燃料喷嘴。 每个喷嘴都有自己的燃料控制阀,以控制流向喷嘴的燃料。 为了最小化通过燃料控制阀的压降,采用多个歧管。 每个歧管在具有燃料的多个燃烧室中提供至少一个燃料喷嘴。 燃料控制阀安装在歧管上,使得燃料控制阀和喷嘴的重量由歧管而不是多个燃烧室承载。 用于测量来自所述多个燃烧室的废气的多个热电偶用于感测排气温度。 在执行用于调谐燃气轮机的本发明的方法时,必须注意的是,最有效的燃气轮机是具有最少一氧化二氮,最少量的未燃碳氢化合物和最少量的一氧化碳的燃气轮机 指定能量输出。 为了调整燃气涡轮机以实现这些目的,期望燃气涡轮机中的每个燃烧室相对于剩余的燃烧室良好平衡。 本发明的目的是调节多个燃烧室中的每个,使得没有特定的燃烧室是富的或者是贫的,并且都在剩余的燃烧室的大约1%的范围内运行。
    • 8. 发明申请
    • METHOD FOR TUNING VALVES FOR PRIMARY AND SECONDARY FUEL CIRCUIT
    • 主要和次要燃油电路调节阀的方法
    • US20080000214A1
    • 2008-01-03
    • US11855638
    • 2007-09-14
    • Vasanth KothnurShivakumar Srinivasan
    • Vasanth KothnurShivakumar Srinivasan
    • F02C9/00
    • F23N5/003F02C7/222F02C7/228F02C9/266F23N2037/02F23N2041/20F23R3/28
    • A method for adjusting fuel flow to individual combustion chambers in a gas turbine having fuel nozzles for each combustion chamber, manifolds for supplying fuel to at least one fuel nozzle in each combustion chamber, wherein the manifolds have flow metering devices for the fuel nozzles and a controller for adjusting the flow metering devices, the method including: supplying fuel to the combustion chambers through at least one of the manifolds; combusting the fuel in the combustion chambers and generating exhaust gases which drive the gas turbine; determining whether one of the combustion chambers is operating relatively lean or rich by actuating a corresponding to the one of the combustion chambers to adjust fuel flowing to the one of the combustion chambers; sensing a condition of the exhaust gases at various exhaust regions in the exhaust gases and determining a change in the condition of the exhaust gas due to the actuation of the flow metering device, and correlating the change in the sensed condition of the exhaust gases to the at least one combustion chamber.
    • 一种用于调节燃气轮机中的燃料流的方法,其具有用于每个燃烧室的燃料喷嘴,用于向每个燃烧室中的至少一个燃料喷嘴供应燃料的歧管,其中所述歧管具有用于所述燃料喷嘴的流量计量装置和 控制器,用于调节流量计量装置,该方法包括:通过至少一个歧管向燃烧室供应燃料; 在燃烧室中燃烧燃料并产生驱动燃气轮机的废气; 通过致动相应于所述一个所述燃烧室中的所述燃烧室来确定所述燃烧室中的一个是否相对地运行,以调节燃料流向所述燃烧室中的一个; 感测废气中各种废气区域的废气的状态,并且确定由于流量计量装置的致动引起的废气状态的变化,并将废气的感测状况的变化与 至少一个燃烧室。