Asea Brown Boveri Ag

Jochem Fischer

Jakob Keller

Frank Reiss

Pirmin Schiessel

Ulf Christian M&uuml;ller

A burner arrangement (,) for a gas turbine comprises an interior space (,) enclosed by a casing (,), in which interior space (,) at least one burner (,) is arranged, and into which interior space (,) in each case a jet (,) of a gaseous medium, in particular air, is sprayed through at least two nozzle openings (,) against the direction of flow of the burner (,) and along the inner wall (,) of the casing (,) which jets (,), guided by the inner wall (,), meet one another from opposite directions and combine to form a secondary flow (,) flowing off perpendicularly from the inner wall (,). In such a burner arrangement, the flow is stabilized and evened out by virtue of the fact that, to establish the impingement point of the jets (,), a dividing plate (,) arranged in the flow path of the jets (,) and disposed essentially perpendicularly to the inner wall (,) is provided.

Growing community of inventors

Marbach, Germany

Jochem Fischer