EP 3008388 A2 20160420 - GAS TURBINE ENGINE COMBUSTOR LINER PANEL
Title (en)
GAS TURBINE ENGINE COMBUSTOR LINER PANEL
Title (de)
INNENVERKLEIDUNGSTAFEL FÜR EINEN GASTURBINENMOTOR
Title (fr)
PANNEAU DE REVÊTEMENT POUR CHAMBRE DE COMBUSTION DE TURBINE À GAZ
Publication
Application
Priority
- US 201361835153 P 20130614
- US 201361865912 P 20130814
- US 2014042130 W 20140612
Abstract (en)
[origin: WO2015050592A2] A liner panel is provided for a combustor of a gas turbine engine. The liner panel includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a depression, where the depression includes an entrance to at least one passage through the liner panel.
IPC 8 full level
F02C 7/12 (2006.01); F23M 5/00 (2006.01); F23M 5/04 (2006.01); F23R 3/42 (2006.01)
CPC (source: EP US)
F23R 3/002 (2013.01 - US); F23R 3/005 (2013.01 - EP US); F23R 3/007 (2013.01 - EP US); F23R 3/06 (2013.01 - EP US); F23R 2900/03041 (2013.01 - EP US); F23R 2900/03044 (2013.01 - EP US); F23R 2900/03045 (2013.01 - EP US); Y02T 50/60 (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
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
WO 2015050592 A2 20150409; WO 2015050592 A3 20150611; EP 3008388 A2 20160420; EP 3008388 A4 20160720; US 2016123592 A1 20160505
DOCDB simple family (application)
US 2014042130 W 20140612; EP 14850876 A 20140612; US 201414897725 A 20140612