<p>A turbine inlet temperature operating section (15) determines the turbine inlet temperature T4 based on the flow rate Gf and temperature Tf of fuel being supplied to a combustor (3) and the flow rate G3 and temperature T3 of air. Based on the turbine inlet temperature T4, a pilot ratio operating section (16) sets a pilot ratio, and a bypass valve operating section (17) and an IGV opening operating section (18) generate a bypass valve control signal and an IGV control signal, respectively.</p>
申请公布号
WO2004033874(A1)
申请公布日期
2004.04.22
申请号
WO2003JP13013
申请日期
2003.10.09
申请人
MITSUBISHI HEAVY INDUSTRIES, LTD.;TANAKA, SATOSHI;NAKAMURA, SHINSUKE;FUJII, FUMINORI;UJIIE, NAOKI;TOYAMA, KOZO