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    • 3. 发明授权
    • Pressure compensated fuel delivery system for the combustors of
turbomachinery
    • 用于涡轮机械燃烧器的压力补偿燃料输送系统
    • US6079198A
    • 2000-06-27
    • US69409
    • 1998-04-29
    • Kevin Joseph ProwseHoward Jay KaplanGeorge Raymond HubschmittThomas Edward Wickert
    • Kevin Joseph ProwseHoward Jay KaplanGeorge Raymond HubschmittThomas Edward Wickert
    • F02C7/22F02C7/228F02C9/40F02C7/26
    • F02C7/228
    • A positive displacement pump supplies a low lubricity liquid fuel through a main supply line to the combustors of a turbine. A pressure transducer and a flow meter are provided in the main fuel supply line. The fuel is supplied to a pressure compensated fuel delivery valve which divides the fuel equally among the combustors and affords pressure compensation. A controller is responsive to the pressure in the main fuel supply line to control a bypass pressure valve to supply fuel in the main supply line at a predetermined pressure. The controller also controls the total volume of fuel flow rate through the pressure compensated fuel delivery valve responsive to the flow meter. In another form, a centrifugal pump supplies fuel to the pressure compensated fuel delivery valve. A controller responsive to the flow meter in the main supply line controls the total fuel flow rate to the valve which divides the fuel equally among the combustors at equal flow rates.
    • 正排量泵通过主供应管线将低润滑性液体燃料供应到涡轮机的燃烧器。 在主燃料供应管线中设置有压力传感器和流量计。 燃料被供应到压力补偿燃料输送阀,其在燃烧器中平均分配燃料并提供压力补偿。 控制器响应于主燃料供应管线中的压力来控制旁通压力阀以在预定压力下在主供应管线中供应燃料。 控制器还根据流量计控制通过压力补偿燃料输送阀的燃料流量的总体积。 在另一种形式中,离心泵将燃料供给到压力补偿燃料输送阀。 响应于主供应管线中的流量计的控制器控制到以相等流量在燃烧器中平均分配燃料的阀的总燃料流量。
    • 5. 发明授权
    • Method and operational strategy for controlling variable stator vanes of a gas turbine power generator compressor component during under-frequency events
    • 在低频事件期间控制燃气轮机发电机压缩机部件的可变定子叶片的方法和操作策略
    • US06794766B2
    • 2004-09-21
    • US09893608
    • 2001-06-29
    • Thomas Edward WickertBryan Edward Sweet
    • Thomas Edward WickertBryan Edward Sweet
    • F01D1510
    • F04D27/0246F01D15/10F01D17/14F01D17/16F02C9/20F05D2270/061F05D2270/304
    • A method is provided for controlling variable inlet and stator vanes of a heavy-duty gas turbine electrical power generator compressor component upon occurrence of power grid under-frequency events. Variable inlet guide vanes and the front four variable stator vanes of the compressor are ganged together by means of a common actuation mechanism. Altering the angle of the ganged vanes changes the overall airflow consumption of the compressor and affects the amount of turbine output power produced. Predetermined operational schedules for varying the angular position of the stator vanes in accordance with compressor speed are defined for both nominal and under-frequency operating conditions to ensure optimum compressor efficiency without violating minimum safe compressor surge margin criteria. During a power grid under-frequency event, the variable stator vanes of the compressor are operated in a manner that provides a smooth transition from the predetermined nominal operational schedule to the predetermined under-frequency operational schedule.
    • 提供一种用于在发生电力网频率事件时控制重型燃气轮机发电机压缩机部件的可变入口和定子叶片的方法。 压缩机的可变入口引导叶片和前四个可变定子叶片通过公共致动机构联接在一起。 改变组合叶片的角度会改变压缩机的总体气流消耗并影响所产生的涡轮机输出功率。 根据压缩机转速来定义用于改变定子叶片的角位置的预定操作计划,用于额定和低频操作条件,以确保最佳压缩机效率,而不会违反最小安全压缩机喘振裕度标准。 在电网欠频事件期间,压缩机的可变定子叶片以提供从预定的标称操作时间表到预定的低频操作时间表的平滑过渡的方式操作。