EP 3084308 B1 20190911 - COMBUSTION CHAMBER IN A TURBOMACHINE
Title (en)
COMBUSTION CHAMBER IN A TURBOMACHINE
Title (de)
BRENNKAMMER IN EINER TURBOMASCHINE
Title (fr)
CHAMBRE DE COMBUSTION DANS UNE TURBOMACHINE
Publication
Application
Priority
- FR 1363348 A 20131220
- FR 2014053401 W 20141217
Abstract (en)
[origin: WO2015092284A1] The invention relates to an annular combustion chamber in a turbomachine, comprising two coaxial walls of revolution, one an internal wall (12) and the other an external wall (14), between which emerge fuel injectors (19) each engaged in centring means (36) which are moveable in the radial direction in support means (38), the chamber also comprising means (50, 68) of axial retention in the upstream direction of the centring means. According to the invention, the means of axial retention in the upstream direction are fixed removably to at least one of the internal (12) or external (14) walls of revolution.
IPC 8 full level
F23R 3/28 (2006.01)
CPC (source: EP US)
F23R 3/002 (2013.01 - US); F23R 3/06 (2013.01 - US); F23R 3/283 (2013.01 - EP US); F23R 3/50 (2013.01 - US); F23R 3/60 (2013.01 - US); F05D 2260/30 (2013.01 - US); F23R 2900/00005 (2013.01 - US); F23R 2900/00012 (2013.01 - EP US)
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 2015092284 A1 20150625; EP 3084308 A1 20161026; EP 3084308 B1 20190911; FR 3015639 A1 20150626; FR 3015639 B1 20180831; US 10458654 B2 20191029; US 2018163965 A1 20180614
DOCDB simple family (application)
FR 2014053401 W 20141217; EP 14828233 A 20141217; FR 1363348 A 20131220; US 201415104835 A 20141217