EP 1892472 B1 20101229 - Combustion system particularly for a gas turbine
Title (en)
Combustion system particularly for a gas turbine
Title (de)
Verbrennungssystem insbesondere für eine Gasturbine
Title (fr)
Système de combustion en particulier pour une turbine à gaz
Publication
Application
Priority
EP 06016932 A 20060814
Abstract (en)
[origin: EP1892472A1] The burner (1) has a nozzle pipe (7) and a fuel fluid inlet pipe (9), which are in connection with the nozzle pipe for feeding the fuel fluid into the nozzle pipe, is proposed. The nozzle pipe has a nozzle discharge opening (15) and is designed for spraying a stream of fuel fluid or a mixture of air and fuel fluid into a combustion chamber (3) and further comprises in the region of the nozzle discharge opening protruding elements (19) towards the center of the opening. The elements are formed by a nozzle tube section extending to nozzle discharge opening with inner circumferential surfaces.
IPC 8 full level
F23D 11/40 (2006.01); F23D 14/70 (2006.01); F23R 3/28 (2006.01)
CPC (source: EP)
F23C 9/006 (2013.01); F23D 11/406 (2013.01); F23D 14/70 (2013.01); F23R 3/28 (2013.01); F23C 2900/09002 (2013.01); F23D 2900/11401 (2013.01); F23R 2900/03282 (2013.01)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
EP 1892472 A1 20080227; EP 1892472 B1 20101229; AT E493615 T1 20110115; DE 502006008611 D1 20110210; EP 2052184 A1 20090429; ES 2356924 T3 20110414; WO 2008019969 A1 20080221
DOCDB simple family (application)
EP 06016932 A 20060814; AT 06016932 T 20060814; DE 502006008611 T 20060814; EP 07788256 A 20070806; EP 2007058144 W 20070806; ES 06016932 T 20060814