发明名称 METHOD FOR OPERATING A GAS TURBINE BELOW THE NOMINAL POWER THEREOF
摘要 A method for operating a gas turbine below the nominal power includes: determining a lower power threshold value of the gas turbine which causes the gas turbine to leave a CO-emission-compliant partial load range of the gas turbine; providing a specified threshold value for output gas turbine power, wherein the specified threshold value is less than the nominal power of the gas turbine; and operating the gas turbine at an output gas turbine power above the specified threshold value at a constant exhaust gas temperature, wherein the inlet guide blades of a compressor of the gas turbine are closed further in order to reduce the output gas turbine power. A sufficiently large valve is selected for the specified threshold value so that increases of the primary zone temperature, combustion temperature, and exhaust temperature extend over a CO-emission-compliant partial load range of the gas turbine that is as large as possible.
申请公布号 US2015369137(A1) 申请公布日期 2015.12.24
申请号 US201414768095 申请日期 2014.02.12
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 Engler Thorsten;Gorynski Markus;Gutermuth Manuel;Kreutzer Philipp;Link Marco;Savilius Nicolas;Suselbeck Kai;Tertilt Marc
分类号 F02C9/20;F02C3/04 主分类号 F02C9/20
代理机构 代理人
主权项 1. A method for operating a gas turbine below its rated power, comprising: determining a lower power limit value (p1) for the gas turbine as that power limit value beyond which further lowering of the output gas turbine power leads to departure from a partial load range of the gas turbine in accordance with CO emissions limits, preparing a predefined limit value (p2) for an output gas turbine power, wherein the predefined limit value (p2) is smaller than the rated power of the gas turbine, operating the gas turbine with an output gas turbine power above the predefined limit value (p2) with a constant averaged exhaust gas temperature, or a control variable calculated therefrom, lowering the output gas turbine power, wherein in order to lower the output gas turbine power the inlet guide vanes of a compressor of the gas turbine are closed further, andwherein, if the output gas turbine power drops below the predefined limit value (p2), the exhaust gas temperature of the gas turbine continues to be raised, as the gas turbine power continues to be lowered, up to a maximum exhaust gas temperature, and wherein the predefined limit value (p2) is chosen such that the temperature rises extend over as large as possible a partial load range of the gas turbine in accordance with CO emissions limits.
地址 München DE