Global Patent Index - EP 3957827 A1

EP 3957827 A1 20220223 - A COATING SYSTEM FOR A COMPONENT OF A GAS TURBINE ENGINE

Title (en)

A COATING SYSTEM FOR A COMPONENT OF A GAS TURBINE ENGINE

Title (de)

BESCHICHTUNGSSYSTEM FÜR EINE KOMPONENTE EINES GASTURBINENTRIEBWERKS

Title (fr)

SYSTÈME DE REVÊTEMENT D'UN COMPOSANT D'UN MOTEUR À TURBINE À GAZ

Publication

EP 3957827 A1 20220223 (EN)

Application

EP 20425031 A 20200818

Priority

EP 20425031 A 20200818

Abstract (en)

The coating system for a component of a gas turbine engine comprises a bond coat BC layer (2) and a thermal barrier coating TBC layer (3) above the BC layer (2) . The BC layer (2) has a thickness in the range 180-300 micrometers and a roughness Ra of its surface facing the TBC layer (3) in a range 12.8-19.0 micrometers. The TBC layer (3) has a thickness in the range 200-700 micrometers and a porosity in the range 15.0-23.0 vol %. The ends of ranges are included in the ranges.

IPC 8 full level

F01D 5/28 (2006.01); C23C 4/073 (2016.01); C23C 4/11 (2016.01); C23C 4/134 (2016.01); C23C 28/00 (2006.01); C23C 28/02 (2006.01)

CPC (source: CN EP)

C23C 4/02 (2013.01 - EP); C23C 4/073 (2016.01 - CN EP); C23C 4/10 (2013.01 - CN); C23C 4/11 (2016.01 - CN EP); C23C 4/134 (2016.01 - CN EP); C23C 4/18 (2013.01 - EP); C23C 28/3215 (2013.01 - EP); C23C 28/3455 (2013.01 - EP); F01D 5/288 (2013.01 - EP); F05B 2270/1091 (2013.01 - EP); F05D 2240/15 (2013.01 - EP); F05D 2240/35 (2013.01 - EP); F05D 2250/63 (2013.01 - EP); F05D 2300/175 (2013.01 - EP); F05D 2300/2118 (2013.01 - EP); F05D 2300/514 (2013.01 - EP); F05D 2300/516 (2013.01 - EP)

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 3957827 A1 20220223; EP 3957827 B1 20241002; CN 114075644 A 20220222

DOCDB simple family (application)

EP 20425031 A 20200818; CN 202110948384 A 20210818