Global Patent Index - EP 3106613 A1

EP 3106613 A1 20161221 - COOLING SYSTEM FOR GAS TURBINE ENGINES

Title (en)

COOLING SYSTEM FOR GAS TURBINE ENGINES

Title (de)

KÜHLSYSTEM FÜR GASTURBINENTRIEBWERKEN

Title (fr)

SYSTÈME DE REFROIDISSEMENT POUR MOTEUR À TURBINE À GAZ

Publication

EP 3106613 A1 20161221 (EN)

Application

EP 15001689 A 20150608

Priority

US 201562008619 P 20150606

Abstract (en)

A cooling system for gas turbine engines (100) includes a turbine rotor compartment (106) defining a cooling air plenum (120). A plurality of turbine discs (130,132) are rotatably housed within the rotor compartment (106). A cooling air inlet (122) is in fluid communication with the plenum (120). Each turbine disc includes a cooling outlet (138) in fluid communication with the plenum for cooling the rotor compartment.

IPC 8 full level

F01D 5/08 (2006.01); F01D 9/06 (2006.01)

CPC (source: EP)

F01D 5/084 (2013.01); F01D 9/065 (2013.01); F05D 2260/205 (2013.01)

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 3106613 A1 20161221

DOCDB simple family (application)

EP 15001689 A 20150608