Global Patent Index - EP 2414641 B1

EP 2414641 B1 20130703 - AXIAL TURBO ENGINE ROTOR WITH SEALING DISC

Title (en)

AXIAL TURBO ENGINE ROTOR WITH SEALING DISC

Title (de)

AXIALTURBOMASCHINENROTOR MIT DICHTSCHEIBE

Title (fr)

ROTOR DE TURBOMACHINE AXIALE DOTÉ D'UN DISQUE D'ÉTANCHÉITÉ

Publication

EP 2414641 B1 20130703 (DE)

Application

EP 10715749 A 20100326

Priority

  • EP 2010054001 W 20100326
  • EP 09004781 A 20090331
  • EP 10715749 A 20100326

Abstract (en)

[origin: EP2239419A1] The axial turbo machine rotor, particularly gas turbine, has a rotor body formed in a rotation symmetrical manner around the rotor axis, a rotor blade ring having a multiple rotor blades fixed to the rotor body by a blade foot. A sealing disk (7) is formed in a rotation symmetrical manner around the rotor axis that is arranged to the outer edge (10) adjacent to an axially extending protrusion (6) of the blade foot, so that a hollow space (9) is formed between the blade foot and the sealing disk. A sealing ring (14) is formed by multiple sealing ring segments arranged in circumferential manner.

IPC 8 full level

F01D 5/30 (2006.01); F01D 11/00 (2006.01)

CPC (source: EP US)

F01D 5/3015 (2013.01 - EP US); F01D 11/006 (2013.01 - EP US)

Designated contracting state (EPC)

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 SE SI SK SM TR

DOCDB simple family (publication)

EP 2239419 A1 20101013; CN 102378850 A 20120314; CN 102378850 B 20140716; EP 2414641 A1 20120208; EP 2414641 B1 20130703; ES 2426156 T3 20131021; JP 2012522169 A 20120920; JP 5324700 B2 20131023; PL 2414641 T3 20131231; US 2012034087 A1 20120209; US 8920121 B2 20141230; WO 2010112422 A1 20101007

DOCDB simple family (application)

EP 09004781 A 20090331; CN 201080014725 A 20100326; EP 10715749 A 20100326; EP 2010054001 W 20100326; ES 10715749 T 20100326; JP 2012502600 A 20100326; PL 10715749 T 20100326; US 201013260585 A 20100326