Influence of Porosity on Thermal Conductivity and Sintering in Suspension Plasma Sprayed Thermal Barrier Coatings

Author(s):  
H. Kaßner ◽  
A. Stuke ◽  
M. Rödig ◽  
R. Vaßen ◽  
D. Stöver
2006 ◽  
Vol 54 (12) ◽  
pp. 3343-3349 ◽  
Author(s):  
A JADHAV ◽  
N PADTURE ◽  
E JORDAN ◽  
M GELL ◽  
P MIRANZO ◽  
...  

Author(s):  
S. T. Aruna ◽  
N. Balaji ◽  
B. Arul Paligan

Ceramic thermal barrier coatings (TBCs) have been used for decades to extend the life of combustors and high temperature turbine stationary and rotating components to increase the operating temperature and in turn the performance of gas turbines or diesel engines can be increased. At present, thermal barrier coatings (TBCs) of Y2O3 partially stabilized ZrO2 (YSZ) films are widely used. In recent years ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity are being explored to further increasing the operating temperature of gas turbines and improve the engine efficiency. In the present study, a comparison of the properties of state-of-the art 8wt% yttria stabilized zirconia (YSZ) and lanthana doped YSZ plasma sprayed coatings is presented. Plasma sprayable powders were prepared in the laboratory by a single step precipitation method and characterized. Both the powders had good flowability. These powders were plasma sprayed at identical critical plasma spray parameters. The coatings were characterized for phase, microstructure and thermal conductivity. Both the powders and coatings exhibited tetragonal form of zirconia and no traces of lanthana were observed. Both the coatings exhibited similar porosity levels. Microstructure of the coatings revealed porous coating with good adhesion of the bondcoat with the topcoat. Plasma sprayed 8wt% YSZ and lanthana doped YSZ exhibited thermal conductivity values of 0.88 and 0.67 W m−1 K−1 respectively which is lower than that reported in literature. This study shows that lanthana doping in YSZ helps in lowering the thermal conductivity and hence this coating may be a potential candidate for TBC application.


2019 ◽  
Vol 45 (3) ◽  
pp. 3199-3206 ◽  
Author(s):  
Di Jiang ◽  
Yanfei Wang ◽  
Siqing Wang ◽  
Rongjun Liu ◽  
Jing Han

Author(s):  
Ralph B. Dinwiddie ◽  
Stephen C. Beecher ◽  
Wallace D. Porter ◽  
Ben A. Nagaraj

Thermal barrier coatings (TBCs) applied to the hot gas components of turbine engines lead to enhanced fuel efficiency and component reliability. Understanding the mechanisms which control the thermal transport behavior of the TBCs is of primary importance. Electron beam-physical vapor deposition (EB-PVD) and air plasma spraying (APS) are the two most commonly used coating techniques. These techniques produce coatings with unique microstructures which control their performance and stability. The density of the APS coatings was controlled by varying the spray parameters. The low density APS yttria-partially stabilized zirconia (yttria-PSZ) coatings yielded a thermal conductivity that is lower than both the high density APS coatings and the EB-PVD coatings. The thermal aging of both fully and partially stabilized zirconia are compared. The thermal conductivity of the coatings permanently increases upon exposure to high temperatures. These increases are attributed to microstructural changes within the coatings. This increase in thermal conductivity can be modeled using a relationship which depends on both the temperature and time of exposure. Although the EB-PVD coatings are less susceptible to thermal aging effects, results suggest that they typically have a higher thermal conductivity than APS coatings before thermal aging. The increases in thermal conductivity due to thermal aging for plasma sprayed partially stabilized zirconia have been found to be less than for plasma sprayed fully stabilized zirconia coatings.


2015 ◽  
Vol 279 ◽  
pp. 44-52 ◽  
Author(s):  
Michael P. Schmitt ◽  
Amarendra K. Rai ◽  
Dongming Zhu ◽  
Mitchell R. Dorfman ◽  
Douglas E. Wolfe

Sign in / Sign up

Export Citation Format

Share Document