Development of Al2o3 - Sm2sral2o7 Ceramic Composite Thermal Barrier Coatings for High Temperature Applications

Thumbnail Image

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

Citation

Collections

Endorsement

Review

Supplemented By

Referenced By