Study of the Evolution of the Residual Stresses in Thermal Barrier Coatings from Manufacturing to Its Operation Work
Source abstract
Abstract
Residual stresses’ magnitude generated by deposition, quenching stress, thermal stress operation temperature, and infiltration in the thermal barrier coating (TBC) of gas turbines was determined. A thermal barrier coating was manufactured by the deposition of two layers, CoNiCrAlY and yttria-stabilized zirconia (YSZ), on an AISI 304 stainless steel substrate. The CoNiCrAlY was deposited by using an HVOF gun and the YSZ by an atmospheric plasma spray (APS). The TBCs were heat-treated at 1250 °C, with a CMAS (CaO, MgO, Al2O3, and SiO2) attack with a concentration of 10 mg/cm2 for 6 h in order to evaluate the evolution of the state of residual stresses in the coating at a high temperature. Residual stresses were determined by employing the modified layer removal method for duplex coatings (MLRMDC), ANSYS Version R19.2, and the equations proposed by Noda et al. In the YSZ, the total maximum residual stresses were 139 MPa in compression, and in the CoNiCrAlY, the maximum residual stress was 214 MPa in compression. The factor that has the largest effect on the magnitude of residual stresses was the infiltration of the CMAS in the YSZ.
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Research context
OpenAlex topics: High-Temperature Coating Behaviors · Nuclear Materials and Properties · High Entropy Alloys Studies
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Departamento de Ingeniería en Tecnologías de Manufactura, Universidad Politécnica de Guanajuato, Cortazar 38496, Mexico
Departamento de Ingeniería Robótica, Universidad Politécnica de Guanajuato, Cortazar 38496, Mexico
Departamento de Ingeniería Mecánica, Tecnológico Nacional de México en Celaya, Celaya 38010, Mexico
Departamento de Ingeniería Industrial, Tecnológico Nacional de México en Celaya, Celaya 38010, Mexico
References (42)
Show source-provided references
1. Evolution of hot corrosion resistance of YSZ, Gd2Zr2O7, and Gd2Zr2O7 + YSZ composite thermal barrier coatings in Na2SO4 + V2O5 at 1050 °C10.1016/j.jeurceramsoc.2012.01.006 ↗
2. Gas turbine coatings—An overview10.1016/j.engfailanal.2012.07.007 ↗
3. Through-thickness determination of phase composition and residual stresses in thermal barrier coatings using high-energy X-rays10.1016/j.actamat.2009.10.010 ↗
4. Mechanical characterization and thermal behavior of HVOF-sprayed bond coat in thermal barrier coatings (TBCs)10.1016/j.surfcoat.2005.02.170 ↗
5. High velocity oxy-fuel spraying of a NiCoCrAlY and an intermetallic NiAl–TaCr alloy10.1016/S0257-8972(01)01444-X ↗
6. Crecimiento y caracterización de recubrimientos cerámicos con aplicaciones como barreras térmicas
7. Development of deposition beam current dependent microstructure and nanomechanical properties in ZrO2-8wt% Y2O3 thermal barrier coatings produced by electron beam-physical vapor deposition technique10.1016/j.matchemphys.2021.124998 ↗
8. Analysis of mechanical and thermal stresses due to TiN coating of Fe substrate by physical vapor deposition10.1016/j.finmec.2021.100042 ↗
9. Modeling of residual stresses in a plasma-sprayed zirconia/alumina functionally graded-thermal barrier coating10.1016/S0040-6090(03)00427-9 ↗
10. Metco, S. (2010). HVOF Solutions, Advanced Technology Solutions and Service, HVOF Solutions, Advanced Technology Solutions and Service.
11. Sulzer Metco, S. (2022, July 01). An Introduction to Thermal Spray. Available online: https://silo.tips/download/an-introduction-to-thermal-spray-sulzer-metco.
12. Residual stresses in high-velocity oxy-fuel thermally sprayed coatings—Modelling the effect of particle velocity and temperature during the spraying process10.1016/j.actamat.2007.05.031 ↗
13. Adhesion improvements of Thermal Barrier Coatings with HVOF thermally sprayed bond coats10.1016/j.surfcoat.2006.10.005 ↗
14. Studies on the Influence of Residual Stresses on the Fatigue Life of Rolling Bearings in Dependence on the Production Processes10.3389/fmech.2020.00056 ↗
15. The effect of thermal barrier coatings on diesel engine performance10.1016/j.surfcoat.2006.07.123 ↗
16. Effect of phase transformations on the fracture toughness of t′ yttria stabilized zirconia10.1016/j.msea.2012.07.095 ↗
17. CMAS corrosion of EB PVD TBCs: Identifying the minimum level to initiate damage10.1016/j.ijrmhm.2009.07.005 ↗
18. A delamination mechanism for thermal barrier coatings subject to calcium–magnesium–alumino-silicate (CMAS) infiltration10.1016/j.actamat.2004.11.028 ↗
19. High-temperature interaction of yttria stabilized zirconia coatings with CaO–MgO–Al2O3–SiO2 (CMAS) deposits10.1016/j.surfcoat.2009.07.034 ↗
20. Mechanisms of cracking and delamination within thick thermal barrier systems in aero-engines subject to calcium-magnesium-alumino-silicate (CMAS) penetration10.1016/j.msea.2008.01.006 ↗
21. The influence of calcium–magnesium–aluminosilicate deposits on internal stresses in Yb2Si2O7 multilayer environmental barrier coatings10.1016/j.actamat.2015.12.016 ↗
22. Effect of APS flash bond coatings and curvature on TBC performance on rod specimens10.1016/j.surfcoat.2019.124940 ↗
23. Optimum designs for multi-layered film structures based on the knowledge on residual stresses10.1016/j.apsusc.2006.12.076 ↗
24. Effect of residual stresses on air plasma sprayed thermal barrier coatings10.1016/S0257-8972(03)00207-X ↗
25. On the determination of residual stress and mechanical properties by indentation10.1016/j.msea.2005.10.034 ↗
26. Evaluation of residual stresses of thermal barrier coatings with HVOF thermally sprayed bond coats using the Modified Layer Removal Method (MLRM)10.1016/j.surfcoat.2005.09.016 ↗
27. A finite element analysis technique for predicting as-sprayed residual stresses generated by the plasma spray coating process10.1016/j.finel.2005.02.002 ↗
28. Simulation of residual stresses and their effects on thermal barrier coating systems using finite element method
29. Simulation of residual stress in thick thermal barrier coating (TTBC) during thermal shock: A response surface-finite element modeling10.1016/j.ceramint.2021.11.073 ↗
30. Effect of TGO thickness, pores, and creep on the developed residual stresses in thermal barrier coatings under cyclic loading using SEM image-based finite element model10.1016/j.ceramint.2021.03.336 ↗
31. Ahmad, B., Zhang, X., Guo, H., Fitzpatrick, M.E., Neto, L.M.S.C., and Williams, S. (2022). Influence of Deposition Strategies on Residual Stress in Wire + Arc Additive Manufactured Titanium Ti-6Al-4V. Metals, 12.10.3390/met12020253 ↗
32. Estudio de la evolución del perfil de esfuerzos residuales en recubrimientos barrera térmica depositados sobre acero inoxidable AISI 30410.15446/dyna.v83n197.51150 ↗
33. Noda, N., Hernarski, R.B., and Tanigawa, Y. (2003). Thermal Stress, Taylor and Francis. [2nd ed.].
34. Modeling of residual stresses variation with thermal cycling in thermal barrier coatings10.1016/j.mechmat.2006.01.002 ↗
35. Meza, J.M., Franco, E.E., Farias, M.C.M., Buiochi, F., Souza, R.M., and Cruz, J. (2008). Medición del Módulo de Elasticidad en Materiales de Ingeniería Utilizando la Técnica de Indentación Instrumentada y de Ultra-Sonido. Rev. Metal., 44, Available online: http://revistademetalurgia.revistas.csic.es/index.php/revistademetalurgia/article/viewFile/95/94.10.3989/revmetalm.2008.v44.i1.95 ↗
36. Mechanical and thermal properties of calcium–magnesium aluminosilicate (CMAS) glass10.1016/j.jeurceramsoc.2015.03.032 ↗
37. (2018, May 20). Available online: http://data.irestal.com/files/files/2012030204152933979.pdf.
38. Analysis of residual stresses in thermal barrier coatings10.1016/S0924-0136(99)00157-0 ↗
39. Armengol González, S. (2006). Caracterización Micro Estructural y Mecánica de Barreras Térmicas por APS y EB-PBD Degradadas por Fatiga Térmica y por Contacto. [Master’s Thesis, Departamento de Ingeniería de Materiales, Universidad Politécnica de Cataluña]. Available online: http://upcommons.upc.edu/handle/2099.1/3196.
40. Effects of TGO growth on the stress distribution and evolution of three-dimensional cylindrical thermal barrier coatings based on finite element simulations10.1016/j.ceramint.2021.11.334 ↗
41. Stress distributions in plasma-sprayed thermal barrier coatings as a function of interface roughness and oxide scale thickness10.1016/S0257-8972(02)00359-6 ↗
42. Microstructure and thermo-physical properties of yttria stabilized zirconia coatings with CMAS deposits10.1016/j.jeurceramsoc.2011.04.006 ↗