Adhesion strength of ceramic top coat in thermal barrier coatings subjected to thermal cycles: Effects of thermal cycle testing method and environment
Source abstract
Abstract
This paper deals with the adhesion strength of ceramic top coat in thermal barrier coatings (TBCs) subjected to thermal cycles under several different test conditions. Here the TBC specimens consisting of 8% yttria stabilized zirconia, CoNiCrAlY alloy bond coat and Ni-base superalloy were prepared by plasma spraying. The isothermal exposure and the thermal cycles were applied to the TBC specimens by several conditions at high temperatures. A series of the test results clearly demonstrated that the adhesion strength of the top coat was significantly changed by the application of thermal cycles and by the isothermal exposure. It was also found that the thermal fatigue damage might be evolved depending on of the testing method by which the thermal cycles are applied. Some background of these findings were discussed, based on the measurements of elastic modulus, tensile strength, and thermal conductivity of the ceramic top coat, as well as both the thermally grown oxide at the top coat/bond coat interface and the residual stress in the TBC specimens.
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Research context
OpenAlex topics: High-Temperature Coating Behaviors · Nuclear Materials and Properties · Advanced materials and composites
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References (20)
Show source-provided references
1. Oxidation based model for thermal barrier coating life10.1111/j.1151-2916.1984.tb19162.x ↗
2. National Research Council, Coatings for high temperature structural materials—trends and opportunities. Washington DC: National Academy Press; 1996.
3. Seth BB. Superalloys. In: Pollock T et al. The utility gas turbine perspective, Superalloys 2000. Warrendale (PA): TMS; 2000. p. 3–12.10.7449/2000/Superalloys_2000_3_16 ↗
4. Influence of coatings and hot corrosion on the fatigue behavior of Ni-based superalloys10.1016/0040-6090(81)90006-7 ↗
5. 1990
6. The potential for the improvement of high performance thermal barrier coatings
7. ASTM standard test method for adhesion or cohesion strength of thermal spray coatings, C633; 2008.
8. Hutchinson JW. Metal–ceramic interfaces. In: Ruhle M, Evans AG, Ashby MF, Hirth JP, editors. London: Pergamon Press; 1990. p. 295–306.10.1016/B978-0-08-040505-6.50037-4 ↗
9. Failure mechanisms associated with thermally grown oxide in plasma sprayed thermal barrier coatings10.1016/S1359-6454(00)00171-3 ↗
10. Okazaki M, Take K, Kakehi K, Yamazaki Y, Sakane M, Arai M, Sakurai S, Kaneko H, Harada Y, Itoh A, Okuda T, Nonaka I, Fujiyama K, Nanba K. Collaborative research on thermo-mechanical and isothermal low-cycle fatigue strength of Ni-base superalloys and protective coatings at elevated temperatures in the society of materials science, Japan (JSMS). ASTM STP 1428; 2003. p. 180–94.10.1520/STP11434S ↗
11. Subcommittee on superalloys and coatings, Phase II Activities. Japan: The Society of Materials Science; 2005 [chapters 2–5].
12. Zhu D, Miller RA. Thermal conductivity and elastic modulus evolution of thermal barrier coatings under high heat flux conditions. NASA/TM-1999-209069; 1999.
13. Kaneko H, Torigoe T. Reliability improvement technology of thermal barrier coating for industrial gas turbines. In: Proceeding for the 31st annual conference of the GTSJ; 2003. p. 289–92.
14. Subcommittee on superalloys and coatings, Phase III Activities. Japan: The Society of Materials Science; 2008 [chapters 2–5].
15. The determination of the delamination resistance in thermal barrier coating system by four-point bending tests10.1016/j.surfcoat.2005.12.023 ↗
16. Proposal of delamination life prediction method of thermal barrier coating layer under thermal cycle condition10.2472/jsms.50.651 ↗
17. JIS H 8451. Testing methods for thermal cycle and thermal shock resistance of thermal barrier coatings; 2007.
18. Collaborative research on adhesion strength of thermal barrier coatings in JSMS10.1299/jmmp.4.252 ↗
19. Damage mechanisms and lifetime behavior of plasma sprayed thermal barrier coating systems for gas turbines—Part I: Experiments10.1016/j.surfcoat.2008.05.006 ↗
20. High temperature strength of Ni-base superalloy coatings10.1016/S1468-6996(00)00022-X ↗