TURBINE ARRANGEMENT

摘要

The invention relates to a turbine arrangement (1; 30; 45; 47) with a compressor, at least one burner arrangement (2; 31; 48) comprising multiple burners (4) and a combustion chamber (5; 34; 51), and a turbine (49), wherein the compressor, the at least one burner arrangement (2; 31; 48) and the turbine (49) are fluidically connected to one another such that, during proper operation, air compressed by the compressor is guided through the burners (4) and is mixed with fuel, whereupon the fuel-air mixture produced is burnt in the combustion chamber (5; 34; 51) and the combustion gases are fed to the turbine (49), characterized in that there is provided a bypass device which is designed such that part of the air compressed by the compressor can be guided, as a bypass flow, past the burners (4) into the region of the outlet end of the combustion chamber (5; 34; 51).