发明名称 Gas turbine control apparatus and gas turbine system using the same
摘要 In a gas turbine control apparatus, a frequency analyzing section frequency-analyzes at least one of pressure oscillation in combustors of a gas turbine and acceleration oscillation of each of the combustors and outputs a first frequency analysis result as the result of frequency analysis for a plurality of predetermined frequency bands. A control unit controls at least one of a first fuel flow rate of fuel and a first air flow rate of air based on the first frequency analysis result for the plurality of frequency bands. The fuel and the air are supplied to the gas turbine.
申请公布号 US2005262849(A1) 申请公布日期 2005.12.01
申请号 US20050191945 申请日期 2005.07.29
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 NOMURA MASUMI;TOYAMA KOZO
分类号 F01D17/16;F02C7/057;F02C7/228;F02C9/00;F02C9/18;F02C9/22;F02C9/26;F02C9/28;F02C9/50;F02C9/52;F23N5/16;F23R3/26;F23R3/34;(IPC1-7):F02C9/28 主分类号 F01D17/16
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