| 摘要 |
<p>A fuel supply system for a gas turbine having at least one combustor (10), comprising at least one first heat exchanger (200A), receiving a fuel from a fuel source at a first temperature through a first fuel line (4) and provide the fuel to the combustor at a second temperature, at least one shut-off valve (28), selectively stoping the fuel-flow through the first fuel line to the combustor and at least one first control valve (27A), regulating the flow-rate of the fuel through the first heat exchanger to the combustor. The shut-off valve and the first control valve are coupled to the first fuel line upstream of and in fluid communication to the first heat exchanger, wherein the shut-off valve is arranged upstream of and in fluid communication to the first control valve.</p> |
