A Case Study on Various Set of Processes used for Formation of Deposition Barrier Substrate Thermal Coating

Abstract

Thermal barrier coatings, or TBCs for short, are superior ceramic coatings that are applied directly to the metallic surfaces of gas turbine blades and other engine types, including diesel and aerospace engines. This kind of thermal barrier system is meant to insulate the different parts from the heat of the gases that pass through them. Turbine efficiency and performance will rise automatically if thermal conductivity is reduced and insulation is used to achieve the maximum thermal gradient. TBCs are two-layer coatings made up of an insulating ceramic layer that is commonly referred to as an insulating layer and an oxidation and corrosion resistant layer known as a bond coat.

Cite as:

Walsh Christian. (2024). A Case Study on Various Set of Processes used for Formation of Deposition Barrier Substrate Thermal Coating. Advancement in Mechanical Engineering and Technology, 5(2),14-22. 

https://doi.org/10.5281/zenodo.11385388