Low cycle fatigue performance of Ni-based superalloy coated with complex thermal barrier coating
- Institute of Physics of Materials, Academy of Sciences of the Czech Republic, Žižkova 22, 616 62 Brno (Czech Republic)
- CEITEC – Central European Institute of Technology, Brno University of Technology, Purkyňova 123, 612 00 Brno (Czech Republic)
- Institute of Plasma Physics, Academy of Sciences of the Czech Republic, Za Slovankou 3, 182 00 Praha (Czech Republic)
Highlights: • Novel thermal barrier coating (TBC) with YSZ and ZrO{sub 2} + SiO{sub 2} + Al{sub 2}O{sub 3} eutectic ceramic top coat • TBC deposited via atmospheric plasma spraying and a hybrid water stabilized plasma torch spraying • Effect of eutectic ceramic TBC on LCF behaviour at 900 °C • Damage mechanisms in cyclic loading of cast nickel-based superalloy coated with TBC • The dislocation structures of a Ni-base superalloy were observed. - Abstract: Thermal barrier coatings (TBCs) are widely applied to protect high-temperature components against high temperatures in harsh environments. Nineteen cylindrical specimens of Inconel 713LC were manufactured using the investment castings technique, and 10 specimens were subsequently coated with a novel complex thermal barrier coating (TBC) system. The TBC system comprises a metallic CoNiCrAlY bond coat (BC) and a complex ceramic top coat (TC). The TC is a mixture of a near eutectic nanocrystalline ceramic made of zirconia (ZrO{sub 2}), alumina (Al{sub 2}O{sub 3}), silica (SiO{sub 2}) and conventional yttria stabilized zirconia (YSZ) ceramic in the ratio of 50/50 in wt%. Low cycle fatigue (LCF) tests were carried out in a symmetrical push-pull cycle under strain control at 900 °C. Cyclic hardening/softening curves, cyclic stress-strain curves and fatigue life curves of the TBC-coated and uncoated material were assessed. Fatigue life curves in total strain representation showed transient behaviour. Fracture surfaces and polished sections parallel to the loading axis of the TBC-coated and uncoated specimens prior and after cyclic loading were observed by means of scanning electron microscopy (SEM) to study the degradation mechanisms during high-temperature LCF. TBC delamination was observed at the TC/BC interface, and rafting of precipitates occurred after high-temperature exposure. The microstructural investigations further the discussion of the differences in the stress-strain response and the fatigue life of the TBC-coated and uncoated superalloy.
- OSTI ID:
- 22804993
- Journal Information:
- Materials Characterization, Vol. 139; Other Information: Copyright (c) 2017 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.; Country of input: International Atomic Energy Agency (IAEA); ISSN 1044-5803
- Country of Publication:
- United States
- Language:
- English
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