发明名称 GAS TURBINE COMBUSTOR DIAGNOSTIC SYSTEM AND METHOD
摘要 In an embodiment, a method includes performing a turbine combustor diagnostic routine including operating a first turbine combustor of a plurality of turbine combustors at a substantially steady state of combustion; adjusting an operational parameter of the first turbine combustor to cause a change in combustion products produced by the first turbine combustor; identifying a first sensor response of a first subset of a plurality of sensors disposed within or downstream from a turbine fluidly coupled to the turbine combustor, the first sensor response being indicative of the change in the combustion products, and wherein the first subset comprises one or more first sensors; correlating the first subset of sensors with the first turbine combustor; and diagnosing a condition of the first subset of the plurality of sensors, the first turbine combustor, or a combination thereof, based on the first sensor response.
申请公布号 WO2015130363(A3) 申请公布日期 2015.11.12
申请号 WO2014US68453 申请日期 2014.12.03
申请人 GENERAL ELECTRIC COMPANY;EXXONMOBIL UPSTREAM RESEARCH COMPANY 发明人 WHITE, EUGENE DELANO
分类号 F02C7/228;F01D17/08;F02C3/34;F02C9/28;F23N5/24;G01M15/10;G01M15/14 主分类号 F02C7/228
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