EP 3078914 A1 20161012 - ANNULAR COMBUSTOR FOR A GAS TURBINE ENGINE
Title (en)
ANNULAR COMBUSTOR FOR A GAS TURBINE ENGINE
Title (de)
RINGBRENNER FÜR EINEN GASTURBINENMOTOR
Title (fr)
CHAMBRE DE COMBUSTION ANNULAIRE POUR UN MOTEUR À TURBINE À GAZ
Publication
Application
Priority
EP 15162999 A 20150409
Abstract (en)
An annular combustor (10) for a gas turbine engine (1), axially extending between a first axial burner end (11) and a second axial outlet end (12) and radially extending between an annular inner liner (15) and an annular outer liner (16), wherein the annular combustor (10) is at least an assembly of: - a first part (21) including the annular inner liner (15) and a first connection element (31) for connecting the first part (21) to the gas turbine engine (1), - a second part (22) including the annular outer liner (16) and a second connection element (32) for connecting the second part (22) to the gas turbine engine (1), - at least one of the first connection element (31) and of the second connection element (32) being adjacent to the outlet end (12) of the combustor (10).
IPC 8 full level
CPC (source: EP US)
F23R 3/005 (2013.01 - EP US); F23R 3/60 (2013.01 - EP US); F23R 2900/00012 (2013.01 - EP US)
Citation (search report)
[XA] GB 1578474 A 19801105 - GEN ELECTRIC
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)
EP 3078914 A1 20161012; EP 3256782 A1 20171220; US 2018073738 A1 20180315; WO 2016162239 A1 20161013
DOCDB simple family (application)
EP 15162999 A 20150409; EP 16713399 A 20160329; EP 2016056793 W 20160329; US 201615563687 A 20160329