TY - JOUR
T1 - Failure modes and 3D stress analysis method of thermal barrier coatings on turbine blades
T2 - Coupling creep and oxidation effects
AU - Zhang, Tong
AU - Wang, Yanrong
AU - Tao, Qiannan
N1 - Publisher Copyright:
© 2026 Elsevier Ltd.
PY - 2026/8/10
Y1 - 2026/8/10
N2 - Thermal barrier coatings (TBCs), serving as critical thermal protection systems for engine turbine blades, significantly enhance the high-temperature load-bearing capacity of hot-section components when combined with integrated cooling designs. However, these coatings remain highly susceptible to failure under harsh operating conditions. These failures are fundamentally driven by the complex evolution of internal mechanical and thermal responses over time. Consequently, a detailed understanding of coating failure modes and the quantitative characterization of their stress–strain states remain critical challenges in the life assessment of hot-section components. To address this, this paper proposes a three-dimensional stress evaluation method for coated turbine blades that accounts for creep deformation and oxidation. By combining analytical modeling with the finite element method (FEM), this approach overcomes the cross-scale computational challenges inherent to coated blades and correlates complex stress states with specific failure modes. First, the coated turbine blade is simplified into a multi-layered cylindrical tube model. Analytical stress formulations for each structural layer under creep and oxidation conditions are derived and subsequently validated against FEM results. Second, creep and tensile tests are conducted on coated specimens to systematically investigate the relationship between various stress states and failure mechanisms. Furthermore, by integrating the analytical models with FEM, a computational framework is established to bridge the macroscopic stress distribution of the entire blade with the localized stresses within the coating, thereby quantifying the influence of key parameters on coating stress. Ultimately, this study successfully correlates stress states with failure modes in coated blades subjected to thermo-mechanical loading. The proposed methodology provides a robust framework for evaluating coating stresses in complex engineering components, while the parametric sensitivity analyses offer theoretical guidance for the structural design of coatings.
AB - Thermal barrier coatings (TBCs), serving as critical thermal protection systems for engine turbine blades, significantly enhance the high-temperature load-bearing capacity of hot-section components when combined with integrated cooling designs. However, these coatings remain highly susceptible to failure under harsh operating conditions. These failures are fundamentally driven by the complex evolution of internal mechanical and thermal responses over time. Consequently, a detailed understanding of coating failure modes and the quantitative characterization of their stress–strain states remain critical challenges in the life assessment of hot-section components. To address this, this paper proposes a three-dimensional stress evaluation method for coated turbine blades that accounts for creep deformation and oxidation. By combining analytical modeling with the finite element method (FEM), this approach overcomes the cross-scale computational challenges inherent to coated blades and correlates complex stress states with specific failure modes. First, the coated turbine blade is simplified into a multi-layered cylindrical tube model. Analytical stress formulations for each structural layer under creep and oxidation conditions are derived and subsequently validated against FEM results. Second, creep and tensile tests are conducted on coated specimens to systematically investigate the relationship between various stress states and failure mechanisms. Furthermore, by integrating the analytical models with FEM, a computational framework is established to bridge the macroscopic stress distribution of the entire blade with the localized stresses within the coating, thereby quantifying the influence of key parameters on coating stress. Ultimately, this study successfully correlates stress states with failure modes in coated blades subjected to thermo-mechanical loading. The proposed methodology provides a robust framework for evaluating coating stresses in complex engineering components, while the parametric sensitivity analyses offer theoretical guidance for the structural design of coatings.
KW - Creep
KW - Failure modes
KW - Oxidation
KW - Stress analysis
KW - Thermal barrier coatings
KW - Turbines
UR - https://www.scopus.com/pages/publications/105040776002
U2 - 10.1016/j.engfracmech.2026.112327
DO - 10.1016/j.engfracmech.2026.112327
M3 - 文章
AN - SCOPUS:105040776002
SN - 0013-7944
VL - 343
JO - Engineering Fracture Mechanics
JF - Engineering Fracture Mechanics
M1 - 112327
ER -