ZrO2 coatings partially stabilized by yttria and/or alumina were prepa
red by reactive d.c. magnetron sputtering. Coatings about 6 mu m thick
were deposited on high temperature Ni-based alloy (Inconel 617) with
the aim of protecting the steel against corrosion (oxidation and sulph
uration) at 1000 degrees C. The tensile thermal coating stress during
thermal cycling was controlled by introducing an intrinsic compressive
stress of about 1.7 x 10(9) N m(-2) during the deposition procedure.
Owing to this stress control, the coatings remained undamaged (without
visible cracks and delamination) during rapid thermal cycling at heat
ing and cooling rates of about 9 K s(-1) and during prolonged exposure
to atmospheric pressure. Nevertheless, owing to the high diffusity of
oxygen in ZrO2, some oxidation of the substrate was unavoidable for t
he ZrO2-Y2O3 coatings. Substrate oxidation could be significantly dimi
nished by the use of ZrO2-4 wt.%Y2O3-15 wt.%Al2O3 coatings. The corros
ion of the protected substrates followed a parabolic law with a parabo
lic corrosion constant of about k(p)=9x10(-10)kg(2)m(-4) s(-1)(K-p=9x1
0(-12) g(2)cm(-4)s(-1)). The adherence of the as-deposited coating was
found to be a critical load of about 22 N as determined by scratch te
sting. A 1000 degrees C heat treatment at atmospheric pressure did not
alter the adherence of the ZrO2-4 wt.%Y2O3-15 wt.%Al2O3 on the growin
g Cr2O3 layer. The adherence of the growing Cr2O3 layer on the substra
te was always superior to the adherence of the physical vapour deposit
ion layer on the corrosion layer. These results and scanning electron
microscopy studies showed the capability of stabilized ZrO2 to protect
high temperature steel in gas mixtures typical for gas turbines.