Method for operating a combustion system
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[0046]The terms upstream and downstream refer to the flow direction of the airflow and / or working gas flow through the gas turbine engine 14 unless otherwise stated. If used and not otherwise specified, the terms axial, radial and circumferential are made with reference to a rotational axis 64 of the gas turbine engine 14.
[0047]FIG. 1 shows an example of a gas turbine engine unit 46 with a gas turbine engine 14 and a unit 48 for an oxygen extraction process in a sectional view. The gas turbine engine 14 comprises, in flow series of a working fluid, like air 22, 50 or a combustion gas 52, an air inlet 54 and a compressor section 56 with a compressor 58, a combustion section 12 with a combustion system 10 and a turbine section 60 with a turbine 62, which are generally arranged in flow series in the direction of a longitudinal or rotational axis 64. The gas turbine engine 14 further comprises a shaft 66 which is rotatable about the rotational axis 64 and which extends longitudinally th...
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