EP 0982544 B1 20030618 - Burner arrangement for a gas turbine
Title (en)
Burner arrangement for a gas turbine
Title (de)
Brenneranordnung für eine Gasturbine
Title (fr)
Brûleur pour une turbine à gaz
Publication
Application
Priority
EP 98810851 A 19980827
Abstract (en)
[origin: US6209327B1] A burner arrangement (20) for a gas turbine comprises an interior space (22) enclosed by a casing (23), in which interior space (22) at least one burner (21) is arranged, and into which interior space (22) in each case a jet (26, 27) of a gaseous medium, in particular air, is sprayed through at least two nozzle openings (24, 25) against the direction of flow of the burner (21) and along the inner wall (23a) of the casing (23) which jets (26, 27), guided by the inner wall (23a), meet one another from opposite directions and combine to form a secondary flow (28) flowing off perpendicularly from the inner wall (23a). 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 (26, 27), a dividing plate (29) arranged in the flow path of the jets (26, 27) and disposed essentially perpendicularly to the inner wall (23a) is provided.
IPC 1-7
IPC 8 full level
CPC (source: EP US)
Designated contracting state (EPC)
DE GB
DOCDB simple family (publication)
EP 0982544 A1 20000301; EP 0982544 B1 20030618; DE 59808762 D1 20030724; US 6209327 B1 20010403
DOCDB simple family (application)
EP 98810851 A 19980827; DE 59808762 T 19980827; US 36983699 A 19990809