Gas turbine combustion chamber.

摘要

In an annular combustion chamber (A), there is arranged on the inflow side in circumferential direction a row of pre-mix burners (B, C). The large pre-mix burners (B), which are the main burners of the annular combustion chamber (A), and the small pre-mix burners (C), which are the pilot burners of the annular combustion chamber, are positioned alternately and at a uniform distance from one another. Both the main burners (B) and the pilot burners (C) open into a single annular front wall (10).