在燃气涡轮机的燃烧器，空气分配室（19）和燃烧室（7）在空间上彼此燃烧器壳体（1）内分离。 分配室和燃烧室的多个管形元件（2）被布置，其中，预混合和Vorverdampfen通预混合喷嘴（15“）供给的燃料的油和/或通过预混合供给的预混合之间（15“）的燃料气体发生与压缩机空气。每个管状 元件（2）被提供到所述燃烧室（7）通过火焰稳定器（3）。在火焰保持器是在所述燃烧室（7）定向扩散喷嘴（8）布置成用于燃料。在负载操作中，每个元件的一小部分是唯一的（ 烧2）通过扩散喷嘴（8），通过预混合喷嘴（15“RESP。15“）的大部分另一方面的供给的燃料。

In the combustor of a gas turbine, a air distribution chamber (19) and a combustion chamber (7) are spatially separated from each other within the combustion chamber casing (1). Between distribution chamber and the combustion chamber a plurality of tubular elements (2) are arranged, in which a pre-mixing and Vorverdampfen the through premixing nozzles (15 ') supplied to the fuel oil and / or a premixing of the through premixing nozzles (15 _") supplied fuel gas takes place with the compressor air. Each tubular element (2) is provided to the combustion chamber (7) through a flame holder (3). Within the flame holder one in the combustion chamber (7) is directed diffusion nozzle (8) arranged for fuel. in the load operation a small portion of each element is only ( 2) the fuel supplied through the diffusion nozzle (8) burnt, the majority of the other hand via the premixing nozzles (15 'resp. 15 ").