Global Patent Index - EP 2604810 A2

EP 2604810 A2 20130619 - Integrated Actuator Module for Gas Turbine Engine

Title (en)

Integrated Actuator Module for Gas Turbine Engine

Title (de)

Integriertes Aktuatormodul für einen Gasturbinenmotor

Title (fr)

Module d'actionneur intégré pour moteur de turbine à gaz

Publication

EP 2604810 A2 20130619 (EN)

Application

EP 12196780 A 20121212

Priority

US 201113327722 A 20111215

Abstract (en)

An actuator module (98) for a gas turbine engine includes a multiple of actuators (102,104,106) mounted within a common actuator housing (100). The actuators may drive low pressure compressor variable vane sets (92A;92B;92C), high pressure compressor variable vane sets (96A;96B;96C) and a bleed valve (94).

IPC 8 full level

F01D 17/16 (2006.01); F04D 29/56 (2006.01)

CPC (source: EP)

F01D 17/16 (2013.01); F01D 17/162 (2013.01); F04D 27/0215 (2013.01); F04D 29/563 (2013.01)

Citation (examination)

EP 2098704 A2 20090909 - UNITED TECHNOLOGIES CORP [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)

EP 2604810 A2 20130619; EP 2604810 A3 20130918

DOCDB simple family (application)

EP 12196780 A 20121212