EP 3318803 B1 20210505 - STUD ARRANGEMENT FOR GAS TURBINE ENGINE COMBUSTOR
Title (en)
STUD ARRANGEMENT FOR GAS TURBINE ENGINE COMBUSTOR
Title (de)
BOLZENANORDNUNG FÜR GASTURBINENBRENNKAMMER
Title (fr)
ARRANGEMENT DE BARRES DE RENFORCEMENT POUR CHAMBRE DE COMBUSTION DE MOTEUR DE TURBINE À GAZ
Publication
Application
Priority
US 201615343988 A 20161104
Abstract (en)
[origin: EP3318803A1] A liner panel (72A,B, 74A,B) for use in a combustor of a gas turbine engine, the liner panel (72A,B, 74A,B) includes a stud free zone (200) downstream of a combustor swirler (90). A combustor for a gas turbine engine, the combustor including a liner panel (72A,B, 74A,B) mounted to the support shell via a multiple of studs (100), the liner panel (72A,B, 74A,B) including a stud free zone (200) downstream of each respective combustor swirler (90), the stud free zone (200) including a multiple of film cooling holes.
IPC 8 full level
F23R 3/00 (2006.01)
CPC (source: EP US)
F23R 3/002 (2013.01 - EP US); F23R 2900/00017 (2013.01 - US); F23R 2900/03042 (2013.01 - 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)
EP 3318803 A1 20180509; EP 3318803 B1 20210505; US 2018128485 A1 20180510
DOCDB simple family (application)
EP 17200015 A 20171103; US 201615343988 A 20161104