The bonding strength of the thermal barrier coating including ASP and EB-PVD is studied under different high temperature experiments.The effects of different temperatures
thicknesses of coating and substrate are analyzed.Using the two-direction testing
the normal and tangent bonding strengths under high temperature oxidation are investigated.Tests show that the bonding strength of the same TBCs with different thicknesses is very close.The experiments provided many data and reference for failure modelling and aero-engine parts designing with TBC.
Study of failure mode and failure mechanisms on thermal fatigue of plasma sprayed thermal barrier coatings
Creep behavior of titanium alloy with thermal barrier coatings
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method
Aerodynamic characteristics of design Mach number of 5 two-dimensional inlet with mixed-compression under typical condition
Related Author
WEI Hong-liang
YANG Xiao-guang
QI Hong-yu
HAN Zeng-xiang
WANG Chun
BAI Yu
ZHAO Bin
ZHANG Tingting
Related Institution
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Beijing Institute of Aeronautical Materials
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
Department of Power and Propulsion, School of Engineering, Cranfield University, Bedfordshire MK4