journal article·2023-04-30Open access

Oxidation Behaviors of the NiCrAlY Bond Coats in the Thermal Barrier Coatings under External Loads

Chunyu Cheng, Min Nie, Zhili Tang, Yadong Chai, Cong Li, Li Yang, Yichun Zhou

Coatings· Volume 13· Issue 5

Abstract

To understand the oxidation behaviors of the NiCrAlY bond coats in the thermal barrier coatings (TBCs) under external loads, uniaxial tensile and compressive experiments of the TBCs in air at 900 °C for 100 h were investigated. Then, the experimental results were explained by first-principles simulation. The results showed that the oxidation rate of the NiCrAlY bond coat was accelerated by external stresses. A 0.9 μm thickness, a thermally grown oxide (TGO) layer was found in the NiCrAlY bond coat without stress after oxidation, while a 1.2 μm thickness TGO layer was obtained in the NiCrAlY bond coat under tensile stress after oxidation. The main composition of the TGO layer was Al2O3 because Al was more easily oxidized without stress and under tensile stress. The thickest TGO layer with a thickness of 1.5 μm was formed in the NiCrAlY bond coat under compressive stress after oxidation, consisting of the oxide of Al, Ni, and Cr. The first-principles results showed that the oxidation of Ni and Cr under compressive stress was easier than that under tensile stress due to the role of the 3d orbital.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: High-Temperature Coating Behaviors · Advanced materials and composites · High Entropy Alloys Studies

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Advanced Materials and Nanotechnology, Xidian University, Xi’an 710126, China

AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China

School of Materials Science and Engineering, Xiangtan University, Xiangtan 411105, China

Funding

Fundamental Research Funds for the Central Universities of China · National Basic Research Program of China · Innovation Capability Support Program of Shaanxi

References (28)

Show source-provided references
1. Microstructure design of the laser glazed layer on thermal barrier coatings and its effect on the CMAS corrosion10.1016/j.corsci.2021.109847 ↗
2. Multidisciplinary approach for investigating the hot corrosion behavior of thermal barrier coatings10.1016/j.jeurceramsoc.2021.09.001 ↗
3. High-entropy (Y0.2Gd0.2 Dy0.2Er0.2Yb0.2)2Hf2O7 ceramic: A promising thermal barrier coating material10.1016/j.jmst.2021.05.054 ↗
4. Investigating the Interface Cracking Mechanism of CMAS-Corroded Thermal Barrier Coatings Based on the Cohesive Zone Model10.1016/j.corsci.2022.110337 ↗
5. Thermal barrier coatings for gas-turbine engine applications10.1126/science.1068609 ↗
6. Effect of pre-oxidation on the failure mechanisms of EB-PVD thermal barrier coatings with (Ni, Pt)Al bond coats10.1016/j.corsci.2021.109873 ↗
7. Calcium-magnesium-alumina-silicate (CMAS) resistant high entropy ceramic (Y0.2Gd0.2Er0.2Yb0.2Lu0.2)2Zr2O7 for thermal barrier coatings10.1016/j.jmst.2021.07.053 ↗
8. Effect of TGO thickness on the thermal barrier coatings life under thermal shock and thermal cycle loading10.1016/j.ceramint.2018.02.140 ↗
9. Effects of gradient transitional layer on thermal cycling life and failure of LaZrCeO/YSZ thermal barrier coatings10.1016/j.corsci.2019.108224 ↗
10. Influence of non-uniform feature of thermally grown oxide thickness on the local stress state and cracking behavior in TBC10.1016/j.surfcoat.2022.128607 ↗
11. Preparation of long-lifetime thermal barrier coatings and toughening mechanism by using hierarchy structured zirconia-based microspheres10.1016/j.jeurceramsoc.2021.03.003 ↗
12. Synergistic effect of Re-base diffusion barrier and Pt modification on the oxidation behaviour of NiCrAlY coatings10.1016/j.corsci.2021.109919 ↗
13. Effects of residual stress on the mechanical properties of plasma-sprayed thermal barrier coatings10.1016/j.engfracmech.2013.08.016 ↗
14. Evolution of residual stress in air plasma sprayed yttria stabilised zirconia thermal barrier coatings after isothermal treatment10.1016/j.surfcoat.2014.04.009 ↗
15. Effect of material properties on residual stress distribution in thermal barrier coatings10.1016/j.ceramint.2017.11.127 ↗
16. Comprehensive investigations on fluid flow and heat transfer characteristics of a high-speed rotating turbine disk cavity system of aero-engine10.1016/j.icheatmasstransfer.2022.106170 ↗
17. Aerothermal performances of a rotating turbine disk cavity with non-uniform wall temperature profiles in an aero-engine10.1016/j.tsep.2022.101582 ↗
18. Mechanical properties and calcium-magnesium-alumino-silicate (CMAS) corrosion behavior of a promising Hf6Ta2O17 ceramic for thermal barrier coatings10.1016/j.ceramint.2020.06.316 ↗
19. Real-time detection of CMAS corrosion failure in APS thermal barrier coatings under thermal shock10.1007/s11340-020-00603-7 ↗
20. Generalized Gradient Approximation Made Simple10.1103/PhysRevLett.77.3865 ↗
21. First principles methods using CASTEP
22. Effect of stretching on the initial oxidation of 3C-SiC nanowire by first-principle simulation10.1016/j.apsusc.2019.03.185 ↗
23. Improved tangent estimate in the nudged elastic band method for finding minimum energy paths and saddle points10.1063/1.1323224 ↗
24. A climbing image nudged elastic band method for finding saddle points and minimum energy paths10.1063/1.1329672 ↗
25. Modification of NiCoCrAlY with Pt: Part II. Application in TBC with pure metastable tetragonal(t’) phase YSZ and thermal cycling behavior10.1016/j.jmst.2018.09.040 ↗
26. Comparison of stress evolution under TGO growth simulated by two different methods in thermal barrier coatings10.1016/j.ceramint.2019.09.286 ↗
27. A parametric study of the stress state of thermal barrier coatings: Part I: Creep relaxation
28. Effects of growth stress in finite-deformation thermally grown oxide on failure mechanism of thermal barrier coatings10.1016/j.mechmat.2017.08.011 ↗