燃焼器の制御方法及び制御装置

申请公布号：

JP5635948(B2)

申请号：

JP20110143161

申请日期：

2011.06.28

申请公布日期：

2014.12.03

分类号：

F02C9/54;F02C9/00

主分类号：

F02C9/54

摘要：

<p>Provided are a combustor control method and a combustor controller capable of calculating the combustion air flow and the fuel flow in multi-shafts gas turbine with high precision and without the need of performing complicated calculations and thereby calculating a fuel-air ratio necessary for stable combustion control. The multi-shaft gas turbine is made up of a gas generator turbine 110 and a power turbine 120. A combustor 114 includes a diffusive combustion unit F1 and a plurality of premixed combustion units F21 - F24. An ignition/extinction control unit 220 of the combustor control device calculates the combustion air flow supplied to the combustor 114 based on the open position of compressor inlet guide vanes 112A attached to the gas generator turbine 110, revolution speed of the gas generator turbine 110 and compressor inlet temperature, calculates the flow of fuel supplied to the combustor 114 based on revolution speed of the power turbine 120, and calculates the fuel-air ratio in real time as flame reference based on the calculated combustion air flow and fuel flow.</p>