Global Patent Index - EP 2540973 A1

EP 2540973 A1 20130102 - Seal system for a gas turbine

Title (en)

Seal system for a gas turbine

Title (de)

Dichtungssystem für eine Gasturbine

Title (fr)

Système d'étanchéité pour turbine à gaz

Publication

EP 2540973 A1 20130102 (EN)

Application

EP 11172105 A 20110630

Priority

EP 11172105 A 20110630

Abstract (en)

An abradable seal system for a gas turbine comprises a rotor blade tip (7) with an abrasive coating system (9, 11) and a stationary heat shield ring (1) facing opposite to the blade tip (7) and coated with an abradable coating. The abrasive coating system comprises an oxidation resistant and/or corrosion resistant bond coat (9) and a thermal barrier coating (11) atop of the bond coat (9). The thermal barrier coating (11) is a ZrO 2 coating that is partially stabilized by Y 2 O 3 and free of vertical macrocracks.

IPC 8 full level

C23C 28/00 (2006.01); F01D 5/20 (2006.01); F01D 5/28 (2006.01); F01D 11/12 (2006.01)

CPC (source: EP)

C23C 4/02 (2013.01); C23C 28/30 (2013.01); C23C 28/321 (2013.01); C23C 28/3215 (2013.01); C23C 28/345 (2013.01); C23C 28/3455 (2013.01); F01D 5/20 (2013.01); F01D 5/288 (2013.01); F01D 11/122 (2013.01); F05D 2230/90 (2013.01); F05D 2260/95 (2013.01); F05D 2300/2118 (2013.01); F05D 2300/611 (2013.01)

Citation (applicant)

EP 0707091 A1 19960417 - PRAXAIR TECHNOLOGY INC [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 2540973 A1 20130102; WO 2013001091 A1 20130103

DOCDB simple family (application)

EP 11172105 A 20110630; EP 2012062818 W 20120702