发明名称 Method and apparatus for gas turbine dry low NOx combustor corrected parameter control
摘要 A method for controlling a combustor of an engine, the combustor having a fuel to oxidant ratio, the fuel to oxidant ratio being defined as a ratio of an amount of fuel supplied to the combustor divided by an amount of oxygen in an oxidant stream supplied to the combustor includes controlling the fuel to oxidant ratio of the combustor as a function of the amount of oxygen in the oxidant stream.
申请公布号 US7269952(B2) 申请公布日期 2007.09.18
申请号 US20050906689 申请日期 2005.03.02
申请人 GENERAL ELECTRIC COMPANY 发明人 ARAR MALATH IBRAHIM;PRIESTLEY ROBERT RUSSELL
分类号 F02C9/28 主分类号 F02C9/28
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