PSI - Issue 23

Ladislav Čelko et al. / Procedia Structural Integrity 23 (2019) 360 – 365 Author name / Structural Integrity Procedia 00 (2019) 000 – 000

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decreased after glassification (in comparison to the initial as-sprayed state), the weight loses being 0.38 g and 0.12 g, respectively. Second significant drop in weight occurred continuously via spallation during five cycles at the burner rig test, the weight loses being 0.27 g for the multilayer TBC and 0.14 g for the functional graded TBC. Nevertheless, considering the appearance of the top coat surface, as shown in Fig. 2, and the total weight loss (0.65 g and 0.26 g for multilayer and functional graded systems, respectively) of samples after the CMAS attack, both systems are better than the conventional YSZ TBC tested at the same conditions, which was significantly damaged down to the bond coat.

Fig. 2. Macrographs of CMAS environmental attack interaction with (a) multilayer NiCrAlY – YSZ – GZ; and (b) functional graded NiCrAlY – YSZ – YSZ+GZ – GZ thermal barrier coating systems after burner-rig test.

Both as-sprayed TBCs top coats consisted of a single Gd 2 Zr 2 O 7 pyrochlore phase, as shown in Fig. 3, without any other secondary phases that are often formed during plasma spraying due to interactions with surrounding atmosphere.

Fig. 3. XRD patterns of as-sprayed and CMAS attacked (a) multilayer NiCrAlY – YSZ – GZ; and (b) functional graded NiCrAlY – YSZ – YSZ+GZ – GZ thermal barrier coating systems.