Gas turbine designers are increasingly using electron-beam physical vapor d
eposited (EB-PVD) thermal barrier coatings (TBC) to meet the challenge of h
igher efficiency gas turbine engine requirements. A key feature for expandi
ng the use of TBCs is increased spallation life and reduced spallation life
variability. Such a coating system comprises a substrate (Ni-based single
crystal alloy), a bond coat (diffusion aluminide or MCrAlY), a ceramic (7 w
t.% yttria stabilized zirconia), and a thin thermally grown oxide (TGO) bet
ween the bond coat and the ceramic. The TGO is intended to be alpha -alumin
a. but evidence reported by other researchers suggests that in some cases t
he alpha -deposited TGO may not be entirely ot-alumina. The thin nature of
the TGO in as-deposited TBCs (< 0.5 mum) makes analysis of the phases prese
nt and morphology difficult. Advancements in transmission electron microsco
py (TEM) sample preparation and photo-stimulated luminescence spectroscopy
(PSLS) have allowed higher quality and easier characterization of the TGO.
In this study, EB-PVD TBCs were applied to platinum-aluminide bond coats on
a Ni-based superalloy. Three types of coatings were produced by changing o
ne PVD process variable. The as-processed TGO layer was characterized utili
zing scanning transmission electron microscopy (STEM) and PSLS for each of
the three coating process variables used. Results of this work found that t
he TGO comprised two sublayers; (1) a continuous layer of gamma -Al2O3 betw
een the mixed oxide zone and the bond coat; and (2) a mixed oxide zone betw
een the continuous gamma -Al2O3 and the TBC layer. An explanation for the c
reation of the mixed oxide zone found in these TGO morphologies is presente
d. (C) 2001 Elsevier Science B.V. All rights reserved.