Thermal cycle behaviour of plasma sprayed thermal barrier coatings on cast iron substrate for the application of liner of internal combustion engine

In the present scenario, research on Thermal Barrier Coatings (TBCs) is attracting significant attention in high-temperature applications due to the rising demand in industrial applications, such as gas turbine blades and internal combustion engine components. To meet these demands, it is essential to enhance the mechanical and oxidation properties of thermal barrier coatings. The atmospheric plasma spray methodology for producing these coatings has become a central focus in recent times. In this work, TBCs were prepared by blending pure alumina and Yttria-Stabilized Zirconia (YSZ) in equal proportions. Extensive study of TBCs carried out under high-temperature conditions through thermal cycle tests at elevated temperatures, around 850 °C. A total of 350 thermal cycles were conducted, and microstructures of the coating surface were examined at 150, 250, and 350 cycles. High-temperature stress, generated due to the sintering of the coating, also influences the life of the coatings. Specimen with a topcoat thickness of 300 μm, exhibited good thermal shock resistance compared to the specimens with topcoats of thickness of 100 μm and 200 μm. The effects of process parameters, porosity, and thermal shock resistance are presented in detail. The topcoat with a thickness of 300 μm demonstrated excellent thermal shock resistance and reduced formation of thermally grown oxide (TGO). The porosity of the coating, found to be between 2% and 3%, contributed to its dense nature, effectively reducing oxidation rates and enhancing the coating's lifespan under cyclic high-temperature conditions. • The 300 μm-thick (C3) topcoat exhibits a decrease in thermally generated oxide and strong resilience to thermal shock. • The amount of oxygen trapped in the bottom surface of the topcoat and bond coat decreases with increasing coating thickness. • A denser coating that prolongs the TBC's life by resisting oxidation is composed of equal parts YSZ and pure alumina.

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Publication Details

Journal
Results in Surfaces and Interfaces
Published
2024-09-08
DOI
https://doi.org/10.1016/j.rsurfi.2024.100297
Citations
7
Primary Topic
High-Temperature Coating Behaviors
Type
article
Field-Weighted Citation Impact
9.09
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article

Thermal cycle behaviour of plasma sprayed thermal barrier coatings on cast iron substrate for the application of liner of internal combustion engine

K. R. Varun, Haridasa Nayak, Sonal Shamkuwar, M. Vijay et al.
7 citations
Results in Surfaces and Interfaces
High-Temperature Coating Behaviors
9.09
article

Thermal cycle behaviour of plasma sprayed thermal barrier coatings on cast iron substrate for the application of liner of internal combustion engine

K. R. Varun, Haridasa Nayak, Sonal Shamkuwar, M. Vijay, C. Durga Prasad, Abhijeet Malge, R. Suresh Kumar, T. A. Sudarshan, Venkatesh M. K
article en
7 citations

Abstract

In the present scenario, research on Thermal Barrier Coatings (TBCs) is attracting significant attention in high-temperature applications due to the rising demand in industrial applications, such as gas turbine blades and internal combustion engine components. To meet these demands, it is essential to enhance the mechanical and oxidation properties of thermal barrier coatings. The atmospheric plasma spray methodology for producing these coatings has become a central focus in recent times. In this work, TBCs were prepared by blending pure alumina and Yttria-Stabilized Zirconia (YSZ) in equal proportions. Extensive study of TBCs carried out under high-temperature conditions through thermal cycle tests at elevated temperatures, around 850 °C. A total of 350 thermal cycles were conducted, and microstructures of the coating surface were examined at 150, 250, and 350 cycles. High-temperature stress, generated due to the sintering of the coating, also influences the life of the coatings. Specimen with a topcoat thickness of 300 μm, exhibited good thermal shock resistance compared to the specimens with topcoats of thickness of 100 μm and 200 μm. The effects of process parameters, porosity, and thermal shock resistance are presented in detail. The topcoat with a thickness of 300 μm demonstrated excellent thermal shock resistance and reduced formation of thermally grown oxide (TGO). The porosity of the coating, found to be between 2% and 3%, contributed to its dense nature, effectively reducing oxidation rates and enhancing the coating's lifespan under cyclic high-temperature conditions. • The 300 μm-thick (C3) topcoat exhibits a decrease in thermally generated oxide and strong resilience to thermal shock. • The amount of oxygen trapped in the bottom surface of the topcoat and bond coat decreases with increasing coating thickness. • A denser coating that prolongs the TBC's life by resisting oxidation is composed of equal parts YSZ and pure alumina.

Results in Surfaces and InterfacesVol. 17
International Institute of Information Technology (IN), PES University (IN), Oxford Dental College and Hospital (IN), MIT Art, Design and Technology University (IN), Centurion University of Technology and Management (IN), Dr. Hari Singh Gour University (IN)
Affordable and clean energy
Openalex Percentile: Top 3%
High-Temperature Coating Behaviors
9.09
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