发明名称 CONTROLLING METHOD FOR GAS TURBINE MECHANISM
摘要 PROBLEM TO BE SOLVED: To remove the inertia (delay in action) in the temp. sensing operation inevitable to execute the control. SOLUTION: The fuel quantity FH required to operate a first combustor is controlled with a function of the pressure P3 at the outlet from a compressor, and the ratio of FH to P3 is updated continuously with a factor K1 representing the difference of the temp. T7 at the inlet to a first turbine from its target value T7soll , while the fuel quantity FL required to operate a second combustor is controlled with a function of the pressure P11 at the inlet to the second turbine, and the ratio of FL to the pressure P11 is updated continuously with a factor K2 representing the difference of the temp. T11 at the inlet to the second turbine from its target value T11soll .
申请公布号 JPH11236823(A) 申请公布日期 1999.08.31
申请号 JP19980348409 申请日期 1998.12.08
申请人 ASEA BROWN BOVERI AG 发明人 FRUTSCHI HANS ULRICH
分类号 F02C9/00;F02C6/00;F02C9/28;(IPC1-7):F02C9/28 主分类号 F02C9/00
代理机构 代理人
主权项
地址