Global Patent Index - EP 3367001 A1

EP 3367001 A1 20180829 - SECOND-STAGE COMBUSTOR FOR A SEQUENTIAL COMBUSTOR OF A GAS TURBINE

Title (en)

SECOND-STAGE COMBUSTOR FOR A SEQUENTIAL COMBUSTOR OF A GAS TURBINE

Title (de)

ZWEITE- STUFE- KOMBINATIONSKAMMER FÜR EINE SEQUENTIELLE VERBRENNUNGSKAMMER EINER GASTURBINE

Title (fr)

CHAMBRE DE COMBUSTION DE DEUXIÈME ÉTAPE POUR UNE CHAMBRE DE COMBUSTION SÉQUENTIELLE D'UN TURBINE À GAZ

Publication

EP 3367001 A1 20180829 (EN)

Application

EP 17158577 A 20170228

Priority

EP 17158577 A 20170228

Abstract (en)

A second-stage combustor for a sequential combustor of a gas turbine, includes: a burner (20); a combustion chamber (21) extending along a flow direction downstream of the burner (20), wherein the burner (20) and the combustion chamber (21) form a flow channel (15) and a downstream flame location (33) and an upstream flame location (34) are defined within the combustion chamber (21); and a downstream flame stabilizer (35) at the downstream flame location (33).

IPC 8 full level

F23R 3/34 (2006.01); F23C 6/00 (2006.01); F23C 6/04 (2006.01)

CPC (source: CN EP)

F23C 6/00 (2013.01 - EP); F23C 6/042 (2013.01 - EP); F23R 3/20 (2013.01 - EP); F23R 3/346 (2013.01 - EP); F23R 3/42 (2013.01 - CN); F23D 2207/00 (2013.01 - EP); F23R 2900/00002 (2013.01 - EP); F23R 2900/03341 (2013.01 - EP)

Citation (search report)

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 3367001 A1 20180829; EP 3367001 B1 20201223; CN 108506962 A 20180907; CN 108506962 B 20210924

DOCDB simple family (application)

EP 17158577 A 20170228; CN 201810168642 A 20180228