| 摘要 |
Method and arrangement for providing and controlling a gas turbine ( 1 ) at least one turbine ( 11, 20, 20 '), at least one compressor ( 2, 5 ) driven by the turbine and a combustion chamber ( 16 ) arranged between the compressor and the turbine in the airflow path. The gas turbine includes devices ( 8 ) for direct measurement of the air mass flow at a position upstream of the combustion chamber in the airflow path, with the aim of regulating the quantity of fuel that is delivered to the combustion chamber ( 16 ) on the basis of the measured air mass flow.
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