发明名称 System for controlling a combustion process for a gas turbine
摘要 A system for controlling NOx emissions and combustion pulsation levels of a gas turbine having a gas turbine combustion system, having a single combustion chamber and multiple burners, includes a cascade structure having a first and second control level (1, 2), the first level (1) having a device to control NOx emissions and generate combustion pulsation target levels based on the difference between measured and target NOx emission levels, and the second level (2) having a device to control pulsation levels and generate a ratio (gamma) of fuel flow to different types of burners or to different stages of each burner. The fuel flow ratio (gamma) is based on the difference between the measured and generated target pulsation levels. The control system enables the operation of a gas turbine to meet NOx emission requirements, while maintaining combustion pulsation levels within limits that ensure improved lifetime of the combustion system.
申请公布号 US8434311(B2) 申请公布日期 2013.05.07
申请号 US20090430314 申请日期 2009.04.27
申请人 ZHANG XIAO-YI;SPITZMUELLER TOBIAS;BERNERO STEFANO;ALSTOM TECHNOLOGY LTD. 发明人 ZHANG XIAO-YI;SPITZMUELLER TOBIAS;BERNERO STEFANO
分类号 F02C9/28;F02C9/00;F02C9/26 主分类号 F02C9/28
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