EP 2179222 B1 20141022 - BURNER FOR A COMBUSTION CHAMBER OF A TURBO GROUP
Title (en)
BURNER FOR A COMBUSTION CHAMBER OF A TURBO GROUP
Title (de)
BRENNER FÜR EINE BRENNKAMMER EINER TURBOGRUPPE
Title (fr)
BRÛLEUR POUR UNE CHAMBRE DE COMBUSTION D'UN TURBOGROUPE
Publication
Application
Priority
- EP 2008059321 W 20080716
- DE 102007037289 A 20070807
Abstract (en)
[origin: WO2009019113A2] The invention relates to a burner (1) for a combustion chamber of a turbo group, comprising a twirl generator (2), a mixer (3), and a lance (4) for introducing pilot fuel into a combustion chamber (10). In order to stabilize combustion, the lance (4) is designed and/or arranged to reach so far into an interior (5) of the burner, at least during pilot operation of the burner (1), that at least part of the flame front (16) of a combustion reaction taking place in the combustion chamber (10) extends all the way into the interior (5) of the burner.
IPC 8 full level
CPC (source: EP US)
F23R 3/286 (2013.01 - EP US); F23R 3/343 (2013.01 - EP US); F23C 2900/07002 (2013.01 - EP US); F23C 2900/07021 (2013.01 - EP US); F23D 2900/00015 (2013.01 - EP US)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2009019113 A2 20090212; WO 2009019113 A3 20090611; EP 2179222 A2 20100428; EP 2179222 B1 20141022; EP 2179222 B2 20211201; US 2010146983 A1 20100617; US 8069671 B2 20111206
DOCDB simple family (application)
EP 2008059321 W 20080716; EP 08775142 A 20080716; US 69450610 A 20100127