Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the underlying metal substrate from deterioration during high temperature exposure. Unfortunately, the coatings fail prematurely, preventing the design engineers to fully utilize their implementation. Due to the complexity of the coatings, there are many challenges involved with developing failure hypotheses for the failures. This paper reviews some aspects of the current stateof- the-art on modeling failures of thermal barrier coatings, focusing on mechanics based models (such as finite element simulations) where the material physics is incorporated (such as oxidation and diffusion)
Advances in gas turbine technology place an increasing demand on thermal protection systems of nicke...
Thermal barrier coatings provide a means of thermal insulation of gas turbine components exposed to ...
Air plasma sprayed thermal barrier coating (APS TBC) systems are usually applied to engine component...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal barrier coatings (TBCs) are usually applied on high temperature gas turbine components. They...
The present investigation deals with a plasma-sprayed thermal barrier coating (TBC) intended for hig...
Thermal Barrier Coatings (TBC) are used to shield hot sections of gas turbine engines, helping to pr...
Thermal barrier systems are susceptible to instability of the thermally grown oxide (TGO) at the int...
Thermal barrier coatings (TBCs) are applied in gas turbines to enhance their thermal efficiency by i...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2013.Catalo...
Thermal Barrier Coating (TBC) systems are protective layers applied to critical structural component...
Advances in new materials for current power generation devices, such as gas turbines, have led to mo...
The development of modern gas turbine (GT) engines has been the result of continual improvements in...
Thermal barrier coatings (TBC) for advanced gas turbine blades have been under intensive development...
Thermal barrier coating life models developed under the NASA Lewis Research Center's Hot Section Tec...
Advances in gas turbine technology place an increasing demand on thermal protection systems of nicke...
Thermal barrier coatings provide a means of thermal insulation of gas turbine components exposed to ...
Air plasma sprayed thermal barrier coating (APS TBC) systems are usually applied to engine component...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal barrier coatings (TBCs) are usually applied on high temperature gas turbine components. They...
The present investigation deals with a plasma-sprayed thermal barrier coating (TBC) intended for hig...
Thermal Barrier Coatings (TBC) are used to shield hot sections of gas turbine engines, helping to pr...
Thermal barrier systems are susceptible to instability of the thermally grown oxide (TGO) at the int...
Thermal barrier coatings (TBCs) are applied in gas turbines to enhance their thermal efficiency by i...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2013.Catalo...
Thermal Barrier Coating (TBC) systems are protective layers applied to critical structural component...
Advances in new materials for current power generation devices, such as gas turbines, have led to mo...
The development of modern gas turbine (GT) engines has been the result of continual improvements in...
Thermal barrier coatings (TBC) for advanced gas turbine blades have been under intensive development...
Thermal barrier coating life models developed under the NASA Lewis Research Center's Hot Section Tec...
Advances in gas turbine technology place an increasing demand on thermal protection systems of nicke...
Thermal barrier coatings provide a means of thermal insulation of gas turbine components exposed to ...
Air plasma sprayed thermal barrier coating (APS TBC) systems are usually applied to engine component...