主权项 |
1. A gas turbine with at least a compressor, a combustor, a turbine, and a fuel system,
wherein fuel system comprises a gas separation system, for separating at least a first fuel fraction with high hydrocarbons, which has a higher concentration of high hydrocarbons than an incoming fuel gas, thereby providing a remaining second fuel fraction with a reduced concentration of high hydrocarbons, which has a lower concentration of high hydrocarbons than the incoming fuel gas, and a fuel gas supply line for incoming fuel and/or a fuel line for the second fuel fraction leads to the combustor of the gas turbine for feeding fuel gas into the combustor and in that a fuel line for feeding the first fuel fraction leads to the combustor to control the combustion behaviour by controlled addition of the first fuel fraction into the combustor. |