This article was automatically translated from the original Turkish version.
Thermal barrier coatings are multilayer ceramic-based systems used in engineering components operating at high temperatures to protect the underlying structural material from thermal effects. Developed for parts exposed to high temperatures—primarily jet engines, gas turbines, automotive turbo systems, and energy generation equipment—these coatings aim to prevent performance loss, delay oxidation and corrosion, and extend component life. Thanks to these coatings, systems can operate at higher temperatures while the underlying substrate remains at lower temperatures, thereby preserving its mechanical strength. Thermal barrier coatings also have the potential to reduce maintenance costs by delaying material fatigue.
These coatings feature a layered structure composed of four fundamental components. The bottom layer is a metallic substrate that provides structural support. Above it lies a bond coat designed to enhance oxidation resistance and promote adhesion of the ceramic layer. Over time, this bond coat oxidizes to form a thermally grown oxide (TGO), which plays a critical role in the system’s oxidative behavior and internal stress accumulation. The topmost layer, which provides the primary thermal insulation, is the ceramic coating. This layer minimizes heat transfer to the underlying layers due to its low thermal conductivity.
The bond coat is typically made of nickel- or cobalt-based alloys such as NiCrAlY or CoNiCrAlY. These alloys are preferred for their resistance to high-temperature oxidation and their ability to form a controlled TGO. The ceramic top layer is predominantly based on yttria-stabilized zirconia (YSZ). This material has become the standard in TBC systems due to its high-temperature stability, low thermal conductivity, and high coefficient of thermal expansion.
The primary material for the ceramic top coat is usually zirconia stabilized with 8 mol% Y₂O₃ (YSZ). This cubic-phase structure provides thermal resistance while also offering microstructural flexibility. Its porous nature contributes to low thermal conductivity. However, it is known that YSZ can undergo phase transformations above 1200 °C, leading to performance degradation. Consequently, research continues into alternative ceramic systems.
Among alternatives to YSZ are gadolinium zirconate (Gd₂Zr₂O₇), lanthanum zirconate (La₂Zr₂O₇), and yttrium tantalate (YTaO₄). These materials offer advantages in terms of high-temperature stability and chemical resistance. However, many suffer from mechanical disadvantages such as low fracture toughness. Additionally, rare-earth silicates are used in conjunction with silicon-based substrates as environmental barrier coatings (EBCs) to enhance resistance to environmental conditions.
Bond coats are generally composed of MCrAlY alloys, where “M” represents nickel, cobalt, or a mixture of both, while “Cr” and “Al” enhance oxidation resistance. The alumina (Al₂O₃) layer formed by aluminum oxidation serves as the TGO and is critical to the system’s chemical stability.
Thermal barrier coatings can be produced using various thermal spray techniques. The most common method, Air Plasma Spray (APS), involves melting ceramic powders in a high-temperature plasma and spraying them at high velocity onto the substrate. Coatings produced by this method are typically porous, a structure that contributes to low thermal conductivity. However, APS coatings may exhibit limited thermal cycle durability and are difficult to control microstructurally.
The Electron Beam Physical Vapor Deposition (EB-PVD) method, though more expensive and complex, offers superior properties. In this process, the coating material is vaporized by an electron beam and deposited on the surface to form columnar microstructures. These columnar structures provide high resistance to thermal shock.
One of the newer methods, Cold Gas Dynamic Spray (CGDS), enables application of bond coats at low temperatures. This technique minimizes heat-induced oxidation and phase transformations. It is particularly preferred for metallic layers.
The most fundamental performance requirement for a TBC system is low thermal conductivity and high thermal stability. The thermal conductivity of the ceramic top coat should ideally be below 1 W/m·K, which is directly related to porosity level and material composition. Additionally, the coefficient of thermal expansion must be close to that of the metallic substrate to prevent cracking and stress buildup during thermal cycling.
The resistance of coatings to cyclic thermal loads is also evaluated. In thermal cycle tests, coatings are expected to show no signs of mechanical damage such as cracking, spalling, or delamination. The weakest region is typically the interface between the TGO and the ceramic coating. As the TGO thickens, internal stresses accumulate, increasing the risk of delamination over time.
The most common types of damage in thermal barrier coatings are delamination due to TGO growth, sintering at high temperatures, microcracking from thermal shock, and chemical corrosion. Each of these damage mechanisms arises from distinct processes:
Thermal barrier coatings can be applied to any system operating at high temperatures. Key application areas include aviation and aerospace engines, gas turbines, automotive turbocharger systems, nuclear reactor components, and heat exchangers. These coatings enable higher service temperatures for components, improve efficiency, and reduce fuel consumption.
Moreover, TBC systems are increasingly preferred to preserve the performance of next-generation alloys used in modern hypersonic vehicles, spacecraft, and advanced engineering systems. These critical systems are indispensable in environments where maintenance intervals are long and repair opportunities are limited, due to their essential durability requirements.
A major trend in the development of TBC systems is the concept of functionally graded materials (FGMs). These structures enable a gradual transition between ceramic and metallic layers, reducing stress accumulation. Additionally, intensive research is being conducted on multilayer systems, environmental barrier coatings (EBCs), and high-entropy alloy-based bond coats.
In the future, TBC systems are expected to expand beyond thermal insulation to include smart sensor coatings, self-healing structures, and multifunctional coatings.
Thermal barrier coatings are advanced material systems developed to manage the challenges of high temperature, chemical attack, and mechanical stress in modern engineering. This complex structure, requiring individual design of each layer, is the result of a multidisciplinary engineering field integrating metallurgy, ceramic engineering, thermodynamics, mechanics, and surface technology. A successful TBC application demands not only high-quality coating but also a holistic engineering approach that considers the substrate material, manufacturing method, service conditions, and maintenance strategies. Therefore, thermal barrier coatings are not merely technical solutions—they are fundamental pillars of system reliability and sustainability.
No Discussion Added Yet
Start discussion for "Thermal Barrier Coatings" article
Layered Structure of Thermal Barrier Coating Systems
Material Systems Used
Manufacturing Methods and Application Technologies
Thermal and Mechanical Performance Criteria
Damage Mechanisms and Degradation Processes
Applications and Industrial Significance
Evolving Technologies and Future Perspectives