A 3D finite element model of thermal barrier coating (TBC) system considering the interface morphology is established by using the finite element method. By calculating the change of residual stress at the interface when cooling from high temperature to room temperature, the influence of interface geometry on the residual stress of the TBC system is studied. The results show that the thickness of the TGO layer not only affects the magnitude of the residual stress, but also affects the stress state, and the thicker the TGO layer, the higher the residual stress level in the same model. The increase of the interface amplitude will increase the residual stress at the interface of the bond layer (BC) – TGO, but its influence on the residual stress at the interface of the ceramic layer (TC) – TGO is more complicated. The effect of increasing the interface wavelength will reduce the residual stress level to some extent; The 3D hybrid roughness parameter has less effect on the residual stress. Therefore, the thickness of the oxide layer, the interface amplitude and the wavelength will greatly affect the residual stress of the TBC, which in turn affects the stability of the TBC system, and the thickness of the oxide layer has a decisive significance on the failure location of the coating.
赵茹娟,程子义,于庆民. 界面形貌对热障涂层残余应力影响的三维有限元分析[J]. 航空制造技术, 2023, 66(12): 84-93.
ZHAO Rujuan, CHENG Ziyi, YU Qingmin. Study on Effect of Interfacial Morphology on Residual Stress in Thermal Barrier Coating System by 3D Finite Element Analysis[J]. Aeronautical Manufacturing Technology, 2023, 66(12): 84-93.