GAS TURBINE SYSTEM AND ASSOCIATED COMBUSTION CHAMBER

摘要

The invention relates to a gas turbine system (1 ), in particular for a power plant, comprising a combustion chamber (3) and a turbine (2) which comprises at least one first row of guide blades (4) and one first row of mobile blades (5). The first row of guide blades (4) is integrated into the combustion chamber (3) in order to reduce the formation of nitrogen oxide.