Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1656588 | Surface and Coatings Technology | 2015 | 5 Pages |
•The effect of substrate on TBC lifetime was studied using 1483, X4 and 247 alloys.•Substrates with HVOF NiCoCrAlYHfSi bond coatings and APS–YSZ top coatings were studied.•Photo-stimulated piezospectroscopy stress maps were collected on oxide scales on bare bond coatings and with a YSZ coating.•X-ray fluorescence was used to measure chemical changes in the bond coating.
Directionally-solidified (DS) superalloy components with advanced thermal barrier coatings (TBC) to lower the metal operating temperature have the potential to replace more expensive single crystal superalloys for large land-based turbines. In order to assess relative TBC performance, furnace cyclic testing was used with superalloys 1483, X4 and Hf-rich DS 247 substrates and high velocity oxygen fuel (HVOF)-NiCoCrAlYHfSi bond coatings at 1100 °C with 1-h cycles in air with 10% H2O. With these coating and test conditions, there was no statistically-significant effect of substrate alloy on the average lifetime of the air plasma sprayed (APS) yttria-stabilized zirconia (YSZ) top coatings on small coupons. Using photo-stimulated luminescence piezospectroscopy maps at regular cycling intervals, the residual compressive stress in the α-Al2O3 scale underneath the YSZ top coating and on a bare bond coating was similar for all three substrates and delaminations occurred at roughly the same rate and frequency. X-ray fluorescence (XRF) measurements collected from the bare bond coating surface revealed higher Ti interdiffusion occurring with the 1483 substrate, which contained the highest Ti content.