An experimental set-up utilizing indirect induction heating suitable for th
ermal-mechanical fatigue (TMF) tests of high-temperature materials with the
rmal barrier coatings (TBC) is described. This set-up employed for TMF test
ing of the Co-based superalloy MAR-M 509 with a NiCoCrAlY bond coat and a Z
rO2 topcoat was able to generate temperature gradients across the TBC simil
ar to the in-service conditions inside a gas turbine. The tests show the de
velopment of an extensive inelastic strain during the high temperature comp
ressive part of each cycle usually counterbalanced during the tensile part,
a fast saturation of the stress response within the first loading cycles,
and an exponential decrease in lifetime with increasing applied mechanical
strain range. Micro structural analysis demonstrates that life of the sampl
es was not limited by TBC-related processes but by cracks initiated on oxid
ized carbides on the uncoated surface of the samples. (C) 2001 Elsevier Sci
ence B.V. All rights reserved.