Publicado

2020-11-05

Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration

Determinación de esfuerzos residuales en un recubrimiento de barrera térmica debido a la cantidad infiltrada de CMAS

DOI:

https://doi.org/10.15446/dyna.v87n215.86941

Palabras clave:

Thermal barrier coating (TBC), residual stress, thermal spraying, Calcium–Magnesium–Alumino Silicates (CMAS). (en)
Recubrimiento de barrera térmica (TBC), esfuerzos residuales, rociado térmico, óxidos fundidos de calcio, magnesio, aluminio y silicio (CMAS). (es)

Autores/as

In this work, we present the effect of the amount of CMAS infiltration into YSZ of Thermal barrier coatings (TBC) on the magnitude of residual stresses. The (TBC) were deposited by thermal spraying of CoNiCrAlY (Bond Coat-BC) and YSZ (Top Coat-TC) powders. The deposition of the BC was through the high velocity oxygen fuel (HVOF) system. The TC was deposited via an atmospheric plasma-spraying gun (APS). The TBCs were heat treated at 1250 °C, with a CMAS attack at a concentration of 10 mg/cm².The attack exposure was for 2 and 4 hours respectively. In this evaluation, the measured parameter was the magnitude of the residual stress state in Yttria Stabilized Zirconia (YSZ). The residual stress profiles were obtained using the Modified Layer Removal Method for Duplex Coatings (MRCMRB) and the Noda equations. An increase of 26.446 MPa was determined for 2 hours of thermal treatment and 30.743 MPa for 4 hours.

Este trabajo muestra el efecto de la cantidad infiltrada de CMAS en el YSZ del TBC sobre la magnitud de los residuales. El recubrimiento de barrera térmica (TBC) fue fabricado mediante rociado térmico de dos capas, CoNiCrAlY y zirconia estabilizada con itria (YSZ). La capa metálica de enlace (BC) fue depositada mediante una pistola de rociado a alta velocidad por combustión de oxigeno (HVOF), mientras que la cerámica (TC) mediante rociado por plasma atmosférico (APS). Los TBC’s fueron tratados térmicamente con una temperatura de 1250 °C, con un ataque de CMAS con concentración de 10 mg/cm², durante 2 y 4 horas, respectivamente, con el fin de evaluar el efecto de la cantidad infiltrada de CMAS sobre la magnitud del estado de esfuerzos residuales del TC (YSZ). El estado de esfuerzos del recubrimiento fue determinado mediante el método de remoción de capa modificada para recubrimiento bicapa (MRCMRB) y las ecuaciones de Noda. Se determinó un incremento de 26,446 MPa durante 2 horas de tratamiento térmico y 30,743 MPa durante 4 horas.

Referencias

Habibi, M.H., Wang, L. and Guo, S.M., Evolution of hot corrosion resistance of YSZ, Gd2Zr2O7, and Gd2Zr2O7 + YSZ composite thermal barrier coatings in Na2SO4 + V2O5 at 1050 °C. Journal of the European Ceramic Society, 32, pp. 1635-1642, 2012. DOI: 10.1016/j.jeurceramsoc.2012.01.006

Rajendran, R., Gas turbine coatings - An overview, Engineering Failure Analysis, 26, pp. 355-369, 2012. DOI: 10.1016/J.ENGFAILANAL.2012.07.007

Weyant, C.M., Almer, J. and Faber, K.T., Through-thickness determination of phase composition and residual stresses in thermal barrier coatings using high-energy X-rays. Acta Materialia, 58, pp. 943-951, 2010. DOI: 10.1016/j.actamat.2009.10.01

Jang, H.J., Park, D.H., Jung, Y.G., Jang, J.C. et al., Mechanical characterization and thermal behavior of HVOF-sprayed bond coat in thermal barrier coatings (TBCs). Surface & Coatings Technology, 200, pp. 4355-4436, 2006. DOI: 10.1016/j.surfcoat.2005.02.170

Zhao, L. and Lugscheider, E., High velocity oxy-fuel spraying of a NiCoCrAlY and an intermetallic NiAl-TaCr alloy. Surface and Coatings Technology, 149, pp. 231-235, 2002. DOI: 10.1016/S0257-8972(01)01444-X

Gómez-García, J., Poza, P. y Utrilla, V., Crecimiento y caracterización de recubrimientos cerámicos con aplicaciones como barreras térmicas. Boletín de la Sociedad Española de Cerámica y Vidrio, 45(2), pp. 70-74, 2006. DOI: 10.3989/cyv.2006.v45.i2.315.

Teixeira, V., Andritschky, M., Fischer, W., Buchkremer, H.P. and Stöver, D., Effects of deposition temperature and thermal cycling on residual stress state in zirconia-based thermal barrier coatings. Surface and Coatings Technology, 120-121, pp. 103-111, 1999. DOI: 10.1016/S0257-8972(99)00341-2.

Hashmi, M.S.J., Pappalettere, C. and Ventola, F., Residual stresses in structures coated by a high velocity oxy-fuel technique. Journal of Materials Processing Technology. 75, pp. 81-86, 1998. DOI: 10.1016/S0924-0136(97)00295-1

Widjaja, S., Limarga, A.M. and Yip, T.H. Modeling of residual stresses in a plasma-sprayed zirconia y alumina functionally graded-thermal barrier coating. Thin Solid Films, 434, pp. 216-227, 2003. DOI: 10.1016/S0040-6090(03)00427-9

Bansal, P., Shipway, P.H. and Leen, S.B., Residual stresses in high-velocity oxy-fuel thermally sprayed coatings - Modelling the effect of particle velocity and temperature during the spraying process. Acta Materialia, 55, pp. 5089-5101, 2007. DOI: 10.1016/j.actamat.2007.05.031

Lima. R.C. and Guilemany, J.M., Adhesion improvements of Thermal Barrier Coatings with HVOF thermally sprayed bond coats. Surface & Coatings Technology, 201, pp. 4694-4701, 2007. DOI: 10.1016/j.surfcoat.2006.10.005

Taymaz, I., The effect of thermal barrier coatings on diesel engine performance. Surface & Coatings Technology, 201, pp. 5249-5252, 2007. DOI: 10.1016/j.surfcoat.2006.07.123

Loganathan, A. and Gandhi, A.S., Effect of phase transformations on the fracture toughness of t´ yttria stabilized zirconia. Materials Science & Engineering: A, 556, pp. 927-935, 2012. DOI: 10.1016/j.msea.2012.07.095

Khor, K.A. and Gu, Y.W., Effects of residual stress on the performance of plasma sprayed functionally graded ZrO2:NiCoCrAlY coatings. Materials Science and Engineering, A277, pp. 64-76, 2000. DOI: 10.1016/S0921-5093(99)00565-1

Wellman, R., Whitman, G. and Nicholls, J.R., CMAS corrosion of EB PVD TBCs: identifying the minimum level to initiate damage. International Journal of Refractory Metals & Hard Materials, 28, pp. 124-132, 2010. DOI: 10.1016/j.ijrmhm.2009.07.005

Mercer, C., Faulhaber, S., Evans, A.G. and Darolia, R.A., Delamination mechanism for thermal barrier coatings subject to calcium-magnesium-alumino-silicate (CMAS) infiltration. Acta Materialia, 53, pp. 1029-1039, 2005. DOI: 10.1016/j.actamat.2004.11.028

Shan, X., Luo, L, Chen, W., Zou, Z, Guo, F., He, L., Zhang, A., Zhao, X. and Xiao, P., Pore filling behavior of YSZ under CMAS attack: implications for designing corrosion‐resistant thermal barrier coatings. Journal of the American Ceramic Society, 101, pp. 5756-5770, 2018. DOI: 10.1111/jace.15790

Naraparaju, R., Chavez, J.J.G., Schulz, U. and Ramana, C.V., Interaction and infiltration behavior of Eyjafjallajökull, Sakurajima volcanic ashes and a synthetic CMAS containing FeO with/in EB-PVD ZrO2-65 wt. % Y2O3 coating at high temperature, Acta Materialia, 136, pp. 164-180, 2017. DOI: 10.1016/j.actamat.2017.06.055

Bhattacharyya, A. and Maurice, D., Residual stresses in functionally graded thermal barrier coatings. Mechanics of Materials, 129, pp. 50-56, 2018. DOI: 10.1016/j.mechmat.2018.11.002

Ng, H.W. and Gan, Z., A finite element analysis technique for predicting as-sprayed residual stresses generated by the plasma spray coating process. Finite Elements in Analysis and Design, 41, pp. 1235-1254, 2005. DOI: 10.1016/j.finel.2005.02.002

Lima, C.R.C., Nin, J. and Guilemany, J.M., Evaluation of residual stresses of thermal barrier coatings with HVOF thermally sprayed bond coats using the Modified Layer Removal Method (MLRM). Surface & Coatings Technology, 200, pp. 5963-5972, 2006. DOI: 10.1016/j.surfcoat.2005.09.016

Noda, N., Hernarski, R.B. and Tanigawa, Y., Thermal Stress, 2nd ed., Taylor and Francis, New York, USA, 2003, pp. 29-76.

Yáñez-Contreras, P., Barceinas-Sánchez, J., Poblano-Salas, C., Medina-Flores, J., Garcia-Garcia, A. and Dominguez-Lopez, I., Study of the evolution of residual stresses due to glassy deposits (CMAS) attack in thermal barrier coatings. DYNA, 91(5), pp. 554-559, 2016. DOI: 10.6036/7907

Wu, J., Guo, H., Gao, Y. and Gong, S., Microstructure and thermo-physical properties of yttria stabilized zirconia coatings with CMAS deposits. Journal of the European Ceramic Society, 31, pp. 1881-1888, 2011. DOI: 10.1016/j.jeurceramsoc.2011.04.006

Armengol-González, S., Caracterización microestructural y mecánica de barreras térmicas por APS y EB-PVD degradadas por fatiga térmica y por contacto, Tesis, Departamento de Ingeniería de Materiales, Universidad Politécnica de Cataluña, Barcelona, España, [en línea]. 2006. Disponible en: http://upcommons.upc.edu/handle/2099.1/3196

Hui, D., Guan-Jun, Y., Hong-Neng, C., Hang, D., Cheng-Xin, L. y Chang-Jiu, L., The influence of temperature gradient across YSZ on thermal cyclic lifetime of plasma-sprayed thermal barrier coatings. Ceramics International, 41 (9A), pp. 11046-11056, 2015. DOI: 10.1016/j.ceramint.2015.05.049

Busso, E.P., Lin, J., Sakurai, S. and Nakayama, M., A mechanistic study of oxidation-induced degradation in a plasma-sprayed thermal barrier coating system. Part I: model formulation. Acta Materialia, 49, pp. 1515-1528, 2001. DOI: 10.1016/S1359-6454(01)00061-1

Ahrens, M., Vassen, R. and Stöver, D., Stress distributions in plasma-sprayed thermal barrier coatings as a function of interface roughness and oxide scale thickness. Surface and Coatings Technology, 161, pp. 26-35, 2001. DOI: 10.1016/S0257-8972(02)00359-6

Cómo citar

IEEE

[1]
P. Yáñez Contreras, M. León Rodríguez, J. M. Medina Flores, J. A. Jiménez García, F. J. Santander Bastida, y J. Yáñez Rodríguez, «Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration», DYNA, vol. 87, n.º 215, pp. 76–83, nov. 2020.

ACM

[1]
Yáñez Contreras, P., León Rodríguez, M., Medina Flores, J.M., Jiménez García, J.A., Santander Bastida, F.J. y Yáñez Rodríguez, J. 2020. Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration. DYNA. 87, 215 (nov. 2020), 76–83. DOI:https://doi.org/10.15446/dyna.v87n215.86941.

ACS

(1)
Yáñez Contreras, P.; León Rodríguez, M.; Medina Flores, J. M.; Jiménez García, J. A.; Santander Bastida, F. J.; Yáñez Rodríguez, J. Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration. DYNA 2020, 87, 76-83.

APA

Yáñez Contreras, P., León Rodríguez, M., Medina Flores, J. M., Jiménez García, J. A., Santander Bastida, F. J. & Yáñez Rodríguez, J. (2020). Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration. DYNA, 87(215), 76–83. https://doi.org/10.15446/dyna.v87n215.86941

ABNT

YÁÑEZ CONTRERAS, P.; LEÓN RODRÍGUEZ, M.; MEDINA FLORES, J. M.; JIMÉNEZ GARCÍA, J. A.; SANTANDER BASTIDA, F. J.; YÁÑEZ RODRÍGUEZ, J. Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration. DYNA, [S. l.], v. 87, n. 215, p. 76–83, 2020. DOI: 10.15446/dyna.v87n215.86941. Disponível em: https://revistas.unal.edu.co/index.php/dyna/article/view/86941. Acesso em: 20 mar. 2026.

Chicago

Yáñez Contreras, Pedro, Miguel León Rodríguez, José Martín Medina Flores, José Alfredo Jiménez García, Francisco Javier Santander Bastida, y José Yáñez Rodríguez. 2020. «Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration». DYNA 87 (215):76-83. https://doi.org/10.15446/dyna.v87n215.86941.

Harvard

Yáñez Contreras, P., León Rodríguez, M., Medina Flores, J. M., Jiménez García, J. A., Santander Bastida, F. J. y Yáñez Rodríguez, J. (2020) «Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration», DYNA, 87(215), pp. 76–83. doi: 10.15446/dyna.v87n215.86941.

MLA

Yáñez Contreras, P., M. León Rodríguez, J. M. Medina Flores, J. A. Jiménez García, F. J. Santander Bastida, y J. Yáñez Rodríguez. «Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration». DYNA, vol. 87, n.º 215, noviembre de 2020, pp. 76-83, doi:10.15446/dyna.v87n215.86941.

Turabian

Yáñez Contreras, Pedro, Miguel León Rodríguez, José Martín Medina Flores, José Alfredo Jiménez García, Francisco Javier Santander Bastida, y José Yáñez Rodríguez. «Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration». DYNA 87, no. 215 (noviembre 5, 2020): 76–83. Accedido marzo 20, 2026. https://revistas.unal.edu.co/index.php/dyna/article/view/86941.

Vancouver

1.
Yáñez Contreras P, León Rodríguez M, Medina Flores JM, Jiménez García JA, Santander Bastida FJ, Yáñez Rodríguez J. Determination of residual stresses in thermal barrier coating due to the amount of CMAS infiltration. DYNA [Internet]. 5 de noviembre de 2020 [citado 20 de marzo de 2026];87(215):76-83. Disponible en: https://revistas.unal.edu.co/index.php/dyna/article/view/86941

Descargar cita

CrossRef Cited-by

CrossRef citations4

1. Zachary Stein, Ravisankar Naraparaju, Uwe Schulz, Laurene Tetard, Seetha Raghavan. (2023). Residual stress effects of CMAS infiltration in high temperature jet engine ceramic coatings captured non-destructively with confocal Raman-based 3D rendering. Journal of the European Ceramic Society, 43(4), p.1579. https://doi.org/10.1016/j.jeurceramsoc.2022.11.003.

2. Huwei Dai, Anshun Xie, Lang Gao, Junhong Zhang, Xueling Zhang, Jiewei Lin. (2024). Effect of CMAS penetration behavior on stress evolution in TBCs under three-dimensional temperature gradients. Ceramics International, 50(1), p.660. https://doi.org/10.1016/j.ceramint.2023.10.144.

3. Niranjan Patra, Prathipati Ramesh, Omar Cedillos-Barraza. (2025). Advances in Mechanical Coating. Materials Horizons: From Nature to Nanomaterials. , p.37. https://doi.org/10.1007/978-981-96-7484-8_2.

4. Hyokyeong Kim, Jongwook Kwak, Jinyong Lee, Insu Kim, Jiwoong Kim. (2025). Development of innovative MAX phase bond coats for thermal barrier coatings using multi-scale simulations. Journal of Materials Research and Technology, 36, p.5355. https://doi.org/10.1016/j.jmrt.2025.04.189.

Dimensions

PlumX

Visitas a la página del resumen del artículo

684

Descargas

Los datos de descargas todavía no están disponibles.