Invention Grant
US08434291B2 Systems and methods for detecting a flame in a fuel nozzle of a gas turbine 有权
用于检测燃气轮机的燃料喷嘴中的火焰的系统和方法

Systems and methods for detecting a flame in a fuel nozzle of a gas turbine
Abstract:
A system may detect a flame about a fuel nozzle of a gas turbine. The gas turbine may have a compressor and a combustor. The system may include a first pressure sensor, a second pressure sensor, and a transducer. The first pressure sensor may detect a first pressure upstream of the fuel nozzle. The second pressure sensor may detect a second pressure downstream of the fuel nozzle. The transducer may be operable to detect a pressure difference between the first pressure sensor and the second pressure sensor.
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