发明名称 REAL-TIME MONITORING OF GAS TURBINE LIFE
摘要 A system, method and computer-readable medium for monitoring a life of a gas turbine component is disclosed. A numerical model of the gas turbine component is created and parameter measurements are obtained in real-time for at least a portion of the gas turbine component. The parameter measurements are fused with a subset of the numerical model corresponding to the portion of the gas turbine component to obtain a subset of a fused parameter model corresponding to the portion of the gas turbine component. The subset of the fused parameter model is expanded to obtain the fused parameter model that corresponds to at least a location outside of the portion of the gas turbine component. The life of the gas turbine component is monitored using the fused temperature model.
申请公布号 US2015322789(A1) 申请公布日期 2015.11.12
申请号 US201414270588 申请日期 2014.05.06
申请人 General Electric Company 发明人 Pandey Achalesh Kumar;Khan Khan Mohamed Khirullah Genghis;Madyastha Venkatesh Kattigari;Pai Niranjan Gokuldas;Patrick Romano;Reimann Johan Michael;Viana Felipe Antonio Chegury
分类号 F01B25/00;G01M15/14 主分类号 F01B25/00
代理机构 代理人
主权项 1. A method of monitoring a life of a gas turbine component, comprising: estimating, using a processor, a numerical model of a parameter at the gas turbine component; obtaining measurements of the parameter in real-time for a portion of the gas turbine component; fusing the parameter measurements and a subset of the numerical model corresponding to the portion of the gas turbine component to obtain a subset of a fused parameter model corresponding to the portion of the gas turbine component; expanding the subset of the fused parameter model obtain the fused parameter model that corresponds to at least a location outside of the portion of the gas turbine component; and monitoring the life of the gas turbine component using the fused parameter model.
地址 Schenectady NY US
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