发明名称 AUTO TESTING SYSTEM FOR A GAS TURBINE
摘要 A gas turbine system has a gas turbine engine, control unit, a data acquisition system including a thermodynamic model unit and a test sequence unit, sensor device coupled to the engine for measuring performance parameter of the engine, and comparative unit. The thermodynamic model unit generates computed performance parameter based on mechanical and thermodynamic models of the engine. The test sequence unit generates test sequence data including set point operating data and time schedule data with which a test cycle of the engine is runnable. The data acquisition system generates test control data based on the test sequence data, and is coupled to the control unit for providing test control data thereto to control the engine. The comparative unit is coupled to the data acquisition system such that the measured performance parameter measured by the sensor device is comparable with the computed performance parameter.
申请公布号 US2015362405(A1) 申请公布日期 2015.12.17
申请号 US201414763765 申请日期 2014.01.22
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 Bowler Samuel;Smith Michael;Yarwood Andrew
分类号 G01M15/14;F02C9/26;F02C3/04 主分类号 G01M15/14
代理机构 代理人
主权项 1. A gas turbine system, comprising: a gas turbine engine for generating power, a control unit for controlling the gas turbine engine, a data acquisition system comprising a thermodynamic model unit and a test sequence unit, a sensor device which is coupled to the gas turbine engine for measuring a performance parameter of the gas turbine engine, and a comparative unit, wherein the thermodynamic model unit generates computed performance parameter on the basis of a mechanical model of the gas turbine engine and on the basis of a thermodynamic model of the gas turbine engine, wherein the test sequence unit generates test sequence data comprising set point operating data and time schedule data with which a test cycle of the gas turbine engine is runnable, wherein the data acquisition system generates test control data on the basis of the test sequence data, wherein the data acquisition system is coupled to the control unit for providing the test control data to the control unit such that the gas turbine engine is controllable on the basis of the test control data), and wherein the comparative unit is coupled to the data acquisition system such that the measured performance parameter measured by the sensor device is comparable with the computed performance parameter.
地址 München DE