FUEL INJECTION DEVICE FOR A GAS TURBINE

A fuel injection device for a gas turbine, including a plurality of streamlined bodies arranged in a ring adjacent to one another in a circumferential direction relative to a central axis of the fuel injection device, each streamlined body having a trailing edge and at least one streamlined body having a fuel nozzle on the trailing edge, wherein the plurality of streamlined bodies is split into at least a first group of streamlined bodies and a second group of streamlined bodies, all the streamlined bodies in the first group being the same and being different from the streamlined bodies in the second group, and all the streamlined bodies in the second group being the same. The first group of streamlined bodies includes at least two streamlined bodies adjacent to one another. Alternatively, the streamlined bodies are clustered in sets of two adjacent streamlined bodies. Alternatively, the streamlined bodies are arranged such that the fuel injection device has a maximum of four-fold rotational symmetry in the plane perpendicular to the central axis.