Global Patent Index - EP 2385219 A3

EP 2385219 A3 20130605 - Diffuser for gas turbine system between compressor exit and combustor inlet

Title (en)

Diffuser for gas turbine system between compressor exit and combustor inlet

Title (de)

Diffusor einer Gasturbine zwischen Verdichteraustritt und Brennkammereintritt

Title (fr)

Diffuseur d'une turbine à gaz entre la sortie du compresseur et l'entrée de la chambre à combustion

Publication

EP 2385219 A3 20130605 (EN)

Application

EP 11164824 A 20110504

Priority

US 77426210 A 20100505

Abstract (en)

[origin: EP2385219A2] A diffuser (20) for a gas turbine system (10) having a longitudinal axis (90) is disclosed. The diffuser (20) includes a plurality of diffuser ducts (30). Each of the plurality of diffuser ducts (30) is disposed annularly about the longitudinal axis (90) and has an inlet (32), an outlet (36), and a passage (34) extending between the inlet (32) and the outlet (36). The outlet (36) of each of the plurality of diffuser ducts (30) is tangentially offset from the inlet (32) of the respective diffuser duct (30). Each of the plurality of diffuser ducts (30) is configured to flow a gas flow (80) therethrough, reducing the gas flow (80) velocity.

IPC 8 full level

F01D 9/02 (2006.01); F04D 29/44 (2006.01)

CPC (source: EP US)

F01D 9/02 (2013.01 - EP US); F04D 29/541 (2013.01 - EP US); F04D 29/545 (2013.01 - EP US); F05D 2240/12 (2013.01 - EP US); F05D 2260/60 (2013.01 - EP US)

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 2385219 A2 20111109; EP 2385219 A3 20130605; CN 102235387 A 20111109; JP 2011236897 A 20111124; US 2011271654 A1 20111110

DOCDB simple family (application)

EP 11164824 A 20110504; CN 201110125149 A 20110505; JP 2011094586 A 20110421; US 77426210 A 20100505