Development of Al2o3 - Sm2sral2o7 Ceramic Composite Thermal Barrier Coatings for High Temperature Applications
Date
2023
Authors
J, Fredy James
Journal Title
Journal ISSN
Volume Title
Publisher
National Institute Of Technology Karnataka Surathkal
Abstract
Composite thermal barrier coatings with top coat composition 70 wt. % Al2O3 -
30 wt. % Sm2SrAl2O7 was prepared through atmospheric plasma spraying. The rare
earth material Sm2SrAl2O7 was synthesized in the laboratory through molten salt
technique at 1100 °C. Commercially available NiCrAlY powder was used as bond coat.
The as-coated sample is characterized by XRD, SEM, EBSD and Raman spectroscopy.
The top coat exhibited three phases Sm2SrAl2O7, ϒ-Al2O3, and α-Al2O3. The high
temperature oxidation, hot corrosion and erosion tests were performed to examine the
integrity of the coatings in critical conditions. Further, the surface of the coatings were
modified with a laser beam to reduce the roughness and to seal the open porosities.
The isothermal oxidation tests at 1100 °C for 150 h showed a parabolic weight
gain and a nearly uniform Al2O3 layer formation at interface. The laser-treated samples
showed a comparatively lower parabolic rate constant (kp = 2.2 mg2cm-4s-1) than the as-
coated samples (kp = 2.5 mg2cm-4s-1). Dissociation of top coat was observed from the
XRD analysis of oxidized surface. The electrochemical impedance spectroscopy of the
laser-treated samples revealed a higher impedance than the as-coated samples due to
eliminated porosity. The hot corrosion resistance of the samples at 700 °C and 900 °C
were analyzed in aviation and marine conditions employing the salt combinations 50
%wt. Na2SO4 + 50 %wt. V2O5 and 90 %wt. Na2SO4 + 5 %wt. V2O5 + 5 %wt. NaCl,
respectively. The samples manifested a lower resistance in marine conditions than
aviation conditions, while the laser-treated samples showed a better hot corrosion
resistance than the as-coated samples. The solid particle erosion tests using alumina
erodent was carried out on the composite coatings at 200 °C and 800 °C. A mixed mode
of failure with brittle and ductile material removal mechanisms was observed in the
eroded areas. The weight monitoring calculated a higher average erosion value for the
as-coated samples exposed to 800 °C at a 90° impact angle. Overall, the laser-treated
samples showed a better performance at high temperatures due to the better mechanical
properties and sealing of the porosities generated due to the coating process.
Description
Keywords
Thermal barrier coatings, surface modifications, isothermal oxidation, hot corrosion