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    • 6. 发明授权
    • Systems relating to turbine engine control and operation
    • 与涡轮发动机控制和运行相关的系统
    • US08572975B2
    • 2013-11-05
    • US12480239
    • 2009-06-08
    • Timothy R. BiltonDean M. EricksonBrian M. GallagherKorey F. RendoJohn V. Hains
    • Timothy R. BiltonDean M. EricksonBrian M. GallagherKorey F. RendoJohn V. Hains
    • F02C7/08F02C7/22F02C7/224
    • F02C7/224
    • A combustion turbine engine that includes: a compressor; a combustor that receives fuel from a fuel line; a turbine; a heat exchange portion comprising a portion of the fuel line in heat transfer relationship with a heat source for heating the fuel; a rapid heating value meter disposed to test the heating value of the fuel that is configured to provide heating value test results within approximately 1 minute; a cold leg bypass comprising a fuel line that bypasses the heat exchange portion, the cold leg bypass being connected to the fuel line at an upstream fork and at a fuel mixing junction; and valves for controlling the fuel being directed through the heat exchange portion and the fuel being direct through the cold leg bypass; wherein the length of fuel line between the fuel mixing junction and the combustor is less than 20 meters.
    • 一种燃气轮机,包括:压缩机; 从燃料管线接收燃料的燃烧器; 涡轮机 热交换部分,其包括与用于加热燃料的热源的传热关系的燃料管线的一部分; 设置用于测试在大约1分钟内配置为提供热值测试结果的燃料的热值的快速发热值计; 冷腿旁路,其包括旁路热交换部的燃料管路,冷腿旁路在上游叉和燃料混合连接处连接到燃料管路; 以及用于控制燃料的阀通过热交换部分引导并且燃料直接通过冷腿旁路; 其中燃料混合连接点和燃烧器之间的燃料管线的长度小于20米。