EP 2780636 A1 20140924 - TURBOMACHINE COMBUSTOR ASSEMBLY AND METHOD OF OPERATING A TURBOMACHINE
Title (en)
TURBOMACHINE COMBUSTOR ASSEMBLY AND METHOD OF OPERATING A TURBOMACHINE
Title (de)
BRENNKAMMER EINER TURBOMASCHINE SOWIE VERFAHREN ZUM BETRIEB EINER TURBOMASCHINE
Title (fr)
ENSEMBLE FOYER DE TURBOMACHINE ET MÉTHODE D'UTILISATION D'UNE TURBOMACHINE
Publication
Application
Priority
RU 2011000908 W 20111117
Abstract (en)
[origin: WO2013073984A1] A turbomachine combustor assembly includes a combustor body having a combustor outlet, and a combustion liner arranged within the combustor body. The combustion liner defines a combustion chamber. An injection nozzle is arranged within the combustor body upstream from the combustion chamber. The injection nozzle is configured and disposed to deliver a first fluid toward the combustion chamber. A fluid module is mounted to the combustor body downstream from the combustion chamber. The fluid module includes a fluid module body that defines a fluid zone, a first injector member mounted to the fluid module body and configured to deliver a second fluid into the fluid zone at a first orientation, and a second injector member mounted to the fluid module body and configured to deliver a third fluid into the fluid zone at a second orientation that is distinct from the first orientation.
IPC 8 full level
F23R 3/34 (2006.01)
CPC (source: EP US)
F23R 3/002 (2013.01 - US); F23R 3/346 (2013.01 - EP US)
Citation (search report)
See references of WO 2013073984A1
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
WO 2013073984 A1 20130523; CN 103917826 A 20140709; CN 103917826 B 20160824; EP 2780636 A1 20140924; US 2014238034 A1 20140828
DOCDB simple family (application)
RU 2011000908 W 20111117; CN 201180074781 A 20111117; EP 11855268 A 20111117; US 201113983878 A 20111117