journal article·1999-01

Determination of creep behavior of thermal barrier coatings under laser imposed high thermal and stress gradient conditions

Dongming Zhu, Robert A. Miller

Journal of Materials Research· Volume 14· Issue 1
Publisher page

Abstract

A laser sintering/creep technique has been established to determine the creep behavior of thermal barrier coatings under steady-state high heat flux conditions. For a plasma sprayed zirconia–8 wt.% yttria coating, a significant primary creep strain and a low apparent creep activation energy were observed. Possible creep mechanisms involved include stress induced mechanical sliding and temperature and stress enhanced cation diffusion through the splat and grain boundaries. The elastic modulus evolution, stress response, and total accumulated creep strain variation across the ceramic coating are simulated using a finite difference approach. The modeled creep response is consistent with experimental observations.
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Research context

OpenAlex topics: High-Temperature Coating Behaviors · Nuclear Materials and Properties · Particle Dynamics in Fluid Flows

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

References (32)

Show source-provided references
1. 10.1115/1.280454410.1115/1.2804544 ↗
2. Goedjen · 1995 · 73
3. Kokini · 1995 · 235
4. 5. Beardsley M.B. and Larson H.J. , “Thick Thermal Barrier Coatings for Diesel Components,” DOE/NASA/0332–1, NASA CR-190759 (1992).
5. Cruse · The Gas Turbine and Aeroengine Congress and Exposition · 1988 · 88–GT–284 · 1
6. 10.1111/j.1151-2916.1990.tb07612.x10.1111/j.1151-2916.1990.tb07612.x ↗
7. Kingery · 1976
8. 20. Choi S. R. , Zhu D. , and Miller R. A. , “High Temperature Slow Crack Growth, Fracture Toughness and Room-Temperature Deformation Behavior of Plasma-Sprayed ZrO2–8 wt. %Y2O3,” in Int. Symp. on Advanced Synthesis and Processing, The 22nd Annual Conference on Composites and Advanced Ceramic Materials 1998. Also Ceram. Eng. Sci. Proc. (in press, 1998).
9. Miller · 1995 · 17
10. Novak · 1995 · 153
11. Firestone · 1982 · 758
12. Eaton · 1994 · 22 · 289
13. Okamoto · 1986 · 24B · 565
14. 10.1111/j.1460-2695.1997.tb01546.x10.1111/j.1460-2695.1997.tb01546.x ↗
15. 10.1111/j.1151-2916.1994.tb07063.x10.1111/j.1151-2916.1994.tb07063.x ↗
16. 8. Zhu D. and Miller R.A. , “Influence of High Cycle Thermal Loads on Thermal Fatigue Behavior of Thick Thermal Barrier Coatings,” NASA Technical Paper TP-3676, Army Research Laboratory Technical Report ARL-TR-1341 (May 1997).
17. 12. DeMasi J. T. , Sheffler K. D. , and Ortiz M. , “Thermal Barrier Coating Life Prediction Model Development: Phase I-Final Report,” NASA CR-182230 (December 1989).
18. 10.1016/0257-8972(95)02647-910.1016/0257-8972(95)02647-9 ↗
19. Boley · 1960
20. 4. Yonushonis T.M. , “Thick Thermal Barrier Coatings for Diesel Components,” NASA CR-187111 (1991).
21. 10.1002/978352761553710.1002/9783527615537 ↗
22. Zhu · 1997 · 139
23. Wakai · 1986 · 24B · 583
24. Zhu · 1997 · PV96–26 · 289
25. 10.1016/0257-8972(87)90003-X10.1016/0257-8972(87)90003-X ↗
26. 10.1016/S0921-5093(97)00062-210.1016/S0921-5093(97)00062-2 ↗
27. Dinwiddie · The International Gas Turbine and Aeroengine Congress and Exhibition · 1996 · 96–GT–282 · 1
28. Solmon · 1991 · 24 · 175
29. 10.1016/0956-7151(95)90144-210.1016/0956-7151(95)90144-2 ↗
30. 10.1016/S0257-8972(97)00484-210.1016/S0257-8972(97)00484-2 ↗
31. 2. Miller R.A. , “Assessment of Fundamental Materials Needs for Thick Thermal Barrier Coatings for Truck Diesel Engines,” NASA Technical Memorandum TM-103130, DOE/NASA/21794–1 (1990).10.2172/6973994 ↗
32. 13. Meier S. M. , Nissely D. M. , and Sheffler K. D. , “Thermal Barrier Coating Life Prediction Model Development: Phase II-Final Report,” NASA CR-182230 (July 1991).10.1115/91-GT-040 ↗