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EP 1662202 B1 20161116 - Burner for a gas turbine

Title (en)

Burner for a gas turbine

Title (de)

Brenner für eine Gasturbinenanlage

Title (fr)

Brûleur pour une turbine à gaz

Publication

EP 1662202 B1 20161116 (DE)

Application

EP 04028334 A 20041130

Priority

EP 04028334 A 20041130

Abstract (en)

[origin: EP1662202A1] The burner has an air input (17), a primary fuel stage (20) and a secondary fuel stage (50) for the air input. The secondary fuel stage is upstream of the primary fuel stage in the air flow direction (A) of the air input. The primary and secondary fuel stage is are arranged in the air input so that there is no flow back region between them.

IPC 8 full level

F23R 3/34 (2006.01); F23R 3/36 (2006.01)

CPC (source: EP)

F23R 3/34 (2013.01); F23R 3/36 (2013.01); F23D 2900/00008 (2013.01); F23D 2900/14004 (2013.01); F23R 2900/00014 (2013.01)

Designated contracting state (EPC)

CH DE ES GB IT LI

DOCDB simple family (publication)

EP 1662202 A1 20060531; EP 1662202 B1 20161116

DOCDB simple family (application)

EP 04028334 A 20041130