Hostname: page-component-848d4c4894-pftt2 Total loading time: 0 Render date: 2024-06-03T06:50:54.906Z Has data issue: false hasContentIssue false
  • English
  • Français

Analysis of Residual Stress and Damage Durability with Thermal Fatigue Behavior in Thermal Barrier Coatings

Published online by Cambridge University Press:  15 March 2011

Dong-Ho Park ,
Hyung-Jun Jang ,
Yeon-Gil Jung ,
Jung-Chel Chang  and
Ungyu Paik
Dong-Ho Park
Affiliation:
Dept. of Ceramic Science and Engineering, Changwon National University 9 Sarim-dong, Changwon, Kyungnam 641-773, Korea
Hyung-Jun Jang
Affiliation:
Dept. of Ceramic Science and Engineering, Changwon National University 9 Sarim-dong, Changwon, Kyungnam 641-773, Korea
Yeon-Gil Jung
Affiliation:
Dept. of Ceramic Science and Engineering, Changwon National University 9 Sarim-dong, Changwon, Kyungnam 641-773, Korea
Jung-Chel Chang
Affiliation:
Power Generation Lab, Korea Electric Power Research Institute 103-16 Munji-dong, Yusung-ku, Daejon 305-380, Korea
Ungyu Paik
Affiliation:
Dept. of Ceramic Engineering, Hanyang University 17 Haengdang-dong, Seongdong-gu, Seoul 133-791, Korea
Get access

Abstract

Static thermal fatigue tests for thermal barrier coatings (TBCs) were conducted to observe effects of temperature and holding time on its mechanical properties, hardness and modulus, and damage durability. For which three TBCs samples with different thickness in bonding layer (0.08, 0.14, and 0.28 mm) were prepared using an air plasma spraying (APS) method. Temperature of 950 and 1100°C and holding time of 10 and 100 hr were selected for the thermal fatigue tests. The TBCs with thin bonding layer (0.08 mm) maintain sound condition for all the thermal fatigue tests, even showing an evidence of cracking at the interface between coating and bonding layers. However, the TBCs with intermediate (0.14 mm) and thick (0.28 mm) bonding layers show delamination at interface and fracture of coating layer after the thermal fatigue tests at 1100°C for 100 hr. Thermal growth oxide (TGO) layer is created at the interface between coating and bonding layers in all the TBCs after the thermal fatigue tests, and the TGO layer thickness is mainly affected by temperature. Modulus and hardness of coating layer are increased with an increase of temperature in the thermal fatigue tests, due to the re-sintering of coating layer during the thermal fatigue tests. Effects of bonding layer thickness and thermal fatigue condition on mechanical properties, residual stresses, damage durability of the TBCs are discussed extensively.

Type
Research Article
Information
MRS Online Proceedings Library (OPL) , Volume 821: Symposium P – Nanoscale Materials & Modeling-Relations Among Processing, Microstructure and Mechanical Properties , 2004 , P8.18
Copyright
Copyright © Materials Research Society 2004

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Bose, S., and , DeMasi-Marcin, J. Therm. Spray. Technol. 6, 99(1997).Google Scholar
2. Bennett, A., Mater. Sci. Technol. 30, 1(1987).Google Scholar
3. Brandon, J.R., and Taylor, R., Surf. Coat. Technol. 39, 143(1989)Google Scholar
4. Haynes, J.A., Ferber, M.K., and Porter, W.D., J. Therm. Spray. Technol. 9, 38(1997).Google Scholar
5. Teixeira, V., Andritschky, M., Fischer, W., Buchkremer, H.P., and Stover, D., J. Mater. Proce. Technol. 92–93, 209(1999).Google Scholar
6. Oliver, W.C., Pharr, G.M., J. Mater. Res. 7, 1564(1992).Google Scholar
7. Guiberteau, F., Padture, N.P., Cai, H. and Lawn, B.R., Philos. Mag. A68, 1003(1993).Google Scholar
8. Swain, M.V. and Lawn, B.R., Phys. Stat. Solid. 35, 909(1969).Google Scholar