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公开(公告)号：US20100307158A1
公开(公告)日：2010-12-09
申请号：US12480239
申请日：2009-06-08
CPC分类号： F02C7/224
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US20100307157A1
公开(公告)日：2010-12-09
申请号：US12480187
申请日：2009-06-08
申请人： Timothy R. Bilton , Dean M. Erickson , DurgaPrasad R. Nallamotu , Edward L. McGrath , Tailai Hu
发明人： Timothy R. Bilton , Dean M. Erickson , DurgaPrasad R. Nallamotu , Edward L. McGrath , Tailai Hu
CPC分类号： F02C7/224 , F02C6/18 , F05D2220/75 , Y02E50/11 , Y02T50/678
摘要： A method of controlling a combustion turbine engine, wherein the engine includes: a fuel line including a heat exchange portion; a heating value meter; a cold leg bypass comprising an alternate 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, the fuel mixing junction being positioned such that a length of fuel line between it and the inlet to the combustor is short; and valves for controlling the amount of fuel being directed through the heat exchange portion; the method comprising: measuring the heating value of the fuel; determining a target fuel temperature range based on the heating value and a target Modified Wobbe Index range; and controlling the fuel that bypasses the heat exchange portion such that the temperature of the fuel is within the target temperature range.
摘要翻译： 一种控制燃气涡轮发动机的方法，其中，所述发动机包括：燃料管线，包括热交换部分; 一个发热量表; 冷腿旁路，其包括绕过热交换部分的替代燃料管路，冷腿旁路在上游叉和燃料混合连接处连接到燃料管路，燃料混合连接点被定位成使得燃料管线的长度 它与燃烧器入口之间的距离很短; 以及阀，用于控制通过所述热交换部分引导的燃料量; 该方法包括：测量燃料的热值; 基于所述加热值和目标修正沃泊指数范围确定目标燃料温度范围; 以及控制绕过所述热交换部分的燃料，使得所述燃料的温度在目标温度范围内。
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公开(公告)号：US08572975B2
公开(公告)日：2013-11-05
申请号：US12480239
申请日：2009-06-08
CPC分类号： F02C7/224
摘要： 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.
摘要翻译： 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。
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