EP 0985745 B1 20060712 - Bond coat for a thermal barrier coating system
Title (en)
Bond coat for a thermal barrier coating system
Title (de)
Haftbeschichtung für wärmedämmendes Beschichtungssystem
Title (fr)
Couche de liaison pour système de revêtement de barrière thermique
Publication
Application
Priority
- EP 98307244 A 19980908
- JP 26927098 A 19980924
Abstract (en)
[origin: EP0985745A1] A thermal barrier coating system (20) for the surface of an article (22) designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The thermal barrier coating system (20) employs a bond coat (24) of a nickel aluminide alloy over which a thermal-insulating ceramic layer (26) is deposited. The nickel aluminide bond coat (24) contains zirconium, but is otherwise predominantly of the beta ( beta ) NiAl phase. The bond coat (24) is preferably deposited by a physical vapor deposition process (PVD), such as by magnetron sputtering, electron beam physical vapor deposition (EBPVD), jet vapor deposition (JVD) and plasma spray. The NiAl bond coat (24) with zirconium additions of between 0.05 and 0.5 atomic percent have been shown to exhibit drastically improved thermal fatigue life over prior art bond coats, with optimal results appearing to be obtained at or near 0.1 atomic percent zirconium. <IMAGE>
IPC 8 full level
B23P 9/00 (2006.01); C23C 28/00 (2006.01); C23C 4/10 (2016.01); C23C 8/20 (2006.01); C23C 14/14 (2006.01)
CPC (source: EP)
C23C 28/00 (2013.01)
Citation (examination)
- EP 0792948 A1 19970903 - SNECMA [FR], et al
- US 3450512 A 19690617 - MAXWELL DOUGLAS H
Designated contracting state (EPC)
DE FR GB IT NL
DOCDB simple family (publication)
EP 0985745 A1 20000315; EP 0985745 B1 20060712; JP 2000096259 A 20000404; JP 3579262 B2 20041020
DOCDB simple family (application)
EP 98307244 A 19980908; JP 26927098 A 19980924