Method for determining at least one firing temperature for controlling a gas turbine and gas turbine for performing the method
A technology of gas turbine and combustion temperature, which is applied in the direction of gas turbine device, fuel control of turbine/propulsion device, machine/engine, etc.
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[0029] The invention relates to the use of a control valve position measurement, a pressure measurement upstream and downstream of the control valve, a mass flow measurement of a cooling medium and / or a valve characteristic as input variables for determining the combustion temperature. Taking into account the advantages of the determination of the combustion temperature, as disclosed in documents EP 1 231 369 A2 and EP 1 959 115 A2 or US 2010 / 050591 A1, additional measurements are taken into account in addition to the measurement quantities applied there , in particular the position of the regulating valve (in the cooling line), the pressure ratio at the regulating valve and / or the corresponding valve characteristic.
[0030] Although the influence of the cooling air mass flow as a function of operating conditions (environment-limited and / or load-limited) has been studied in detail and is known sufficiently well for a fixed cooling air supply (see the mentioned document EP 1 23...
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