EP 2812636 A2 20141217 - ANNULAR-COMBUSTION-CHAMBER BYPASS
Title (en)
ANNULAR-COMBUSTION-CHAMBER BYPASS
Title (de)
RINGBRENNKAMMER-BYPASS
Title (fr)
DÉRIVATION DE CHAMBRE DE COMBUSTION ANNULAIRE
Publication
Application
Priority
- DE 102012204162 A 20120316
- EP 2013055344 W 20130315
Abstract (en)
[origin: WO2013135859A2] The invention relates to an annular combustion chamber (1) for a gas turbine having an outer shell (12) which has at least one inlet opening (4) for a burner (3) and an outlet (7) which opens into a turbine chamber (8), wherein ducts (14) which can be closed, which are oriented substantially parallel to the symmetry axis (2) of the annular combustion chamber (1), and through which final compressor air can be guided into the annular combustion chamber (1) are provided in the outer shell (12) in the region of the outlet (7). Furthermore, the invention relates to a gas turbine.
IPC 8 full level
F23R 3/08 (2006.01); F23R 3/04 (2006.01); F23R 3/26 (2006.01)
CPC (source: EP US)
F23R 3/04 (2013.01 - EP US); F23R 3/08 (2013.01 - US); F23R 3/26 (2013.01 - EP US)
Citation (search report)
See references of WO 2013135859A2
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
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
WO 2013135859 A2 20130919; WO 2013135859 A3 20131114; CN 104169649 A 20141126; CN 104169649 B 20161109; DE 102012204162 A1 20130919; EP 2812636 A2 20141217; EP 2812636 B1 20160629; KR 20140138710 A 20141204; US 2015007573 A1 20150108
DOCDB simple family (application)
EP 2013055344 W 20130315; CN 201380013443 A 20130315; DE 102012204162 A 20120316; EP 13710388 A 20130315; KR 20147025333 A 20130315; US 201314382918 A 20130315