Ignition detecting system and method for gas turbine

An ignition detecting method for a gas turbine comprising a combustor for burning air and fuel, a turbine driven by combustion gases from said combustor, and an exhaust temperature sensor for detecting an exhaust temperature on the outlet side of said turbine, the method comprising the steps of:

• calculating a change amount of the exhaust temperature detected after outputting of an ignition command for said combustor on the basis of the exhaust temperature detected at a particular time before the ignition command is outputted;
• and
• determining that said combustor is ignited, when the calculated change amount exceeds a predetermined value in a predetermined period from the outputting time or the ignition command.

An ignition detecting method for a gas turbine comprising a combustor for burning air and fuel, a turbine driven by combustion gases from said combustor, and an exhaust temperature sensor for detecting an exhaust temperature on the outlet side of said turbine, the method being used to detect ignition in said combustor at both of hot startup and cold startup of said gas turbine, the method comprising the steps of:

• calculating a difference between the exhaust temperature detected at a particular time before outputting of an ignition command for said combustor and the exhaust temperature detected after the outputting of the ignition command;
• and
• determining that said combustor is ignited, when the calculated difference is not less than a predetermined value set in common with the hot startup and the cold startup of said gas turbine.

A gas turbine comprising a combustor for burning air and fuel, a turbine driven by combustion gases from said combustor, and an exhaust temperature sensor for detecting an exhaust temperature on the outlet side of said turbine,

• wherein said gas turbine includes a control unit for calculating a difference between the exhaust temperature detected at a particular time before outputting of an ignition command for said combustor and the exhaust temperature detected after the outputting of the ignition command, and determining that said combustor is ignited, when the calculated difference is not less than a predetermined value.

A gas turbine comprising a combustor for burning air and fuel, a turbine driven by combustion gases from said combustor, and an exhaust temperature sensor for detecting an exhaust temperature on the outlet side of said turbine,

• wherein said gas turbine includes a control unit for calculating a change amount of the exhaust temperature detected after outputting of an ignition command for said combustor on the basis of the exhaust temperature detected at a particular time before the ignition command is outputted, and determining that said combustor is ignited, when the calculated change amount exceeds a predetermined value in a predetermined period from the outputting time of the ignition command.

A control method for a gas turbine comprising a combustor for burning air and fuel, a turbine driven by combustion gases from said combustor, and an exhaust temperature sensor for detecting an exhaust temperature on the outlet side of said turbine, the method comprising the steps of:

• calculating a difference between the exhaust temperature detected at a particular time before outputting of an ignition command for said combustor and the exhaust temperature detected after the outputting of the ignition command;
• and
• determining that ignition in said combustor has failed, and controlling a flow rate of fuel supplied to said combustor to be zero, when the calculated difference is not more than a predetermined value.

A control method for a gas turbine comprising a combustor for burning air and fuel, a turbine driven by combustion gases from said combustor, and an exhaust temperature sensor for detecting an exhaust temperature on the outlet side of said turbine, the method comprising the steps of:

• calculating a change amount of the exhaust temperature detected after outputting of an ignition command for said combustor on the basis of the exhaust temperature detected at a particular time before the ignition command is outputted;
• and
• determining that ignition in said combustor has failed, and controlling a flow rate of fuel supplied to said combustor to be zero, when the calculated change amount does not exceed a predetermined value in a predetermined period from the outputting time of the ignition command.