Thermal Cycling Behavior of Air Plasma-Sprayed and Low-Pressure Plasma-Sprayed Environmental Barrier Coatings
Source abstract
Abstract
Yb2Si2O7/Si environmental barrier coatings (EBCs) were produced by air plasma spray (APS) and low-pressure plasma spray (LPPS) processes. The phase composition, microstructure, and bonding strength of APS and LPPS EBCs were investigated. Thermal cycling tests were performed in air and in steam atmosphere respectively at 1316 °C for both APS and LPPS EBCs. There is no coating failure in air atmosphere for both APS and LPPS EBCs after 900 cycles. In contrast, APS EBCs have an average life of 576 cycles in a steam cycling test in 90% H2O + 10% air at 1316 °C while LPPS EBCs survived 1000 cycles without failure. The superior durability of the LPPS EBCs compared to APS EBCs in the same steam cycling environment is attributed to the significantly reduced thermally grown oxide (TGO) growth rate because of the denser and crack-free microstructure, higher bonding strength, and reduced coefficient of thermal expansion (CTE) mismatch (less Yb2SiO5 phase) in the LPPS Yb2Si2O7/Si EBCs.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Advanced ceramic materials synthesis · High-Temperature Coating Behaviors · Metal and Thin Film Mechanics
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Oerlikon Metco (US), 1101 Prospect Ave, Westbury, New York, NY 11590, USA
Oerlikon Metco AG, Rigackerstr. 16, CH-5610 Wohlen, Switzerland
References (16)
Show source-provided references
1. Advanced structural ceramics in aerospace propulsion10.1038/nmat4687 ↗
2. Thermal and environmental barrier coatings for SiC/SiC CMCs in aircraft engine applications10.1111/j.1744-7402.2004.tb00181.x ↗
3. Ceramic matrix composites taking flight at GE aviation
4. Mechanisms of ytterbium monosilicate/mullite/silicon coating failure during thermal cycling in water vapor10.1111/jace.13792 ↗
5. Rare earth silicate environmental barrier coatings for SiC/SiC composites and Si3N4 ceramics10.1016/j.jeurceramsoc.2004.12.013 ↗
6. Yb2Si2O7 Environmental barrier coatings with reduced bond coat oxidation rates via chemical modifications for long life10.1111/jace.15978 ↗
7. Response of ytterbium disilicate-silicon environmental barrier coatings to thermal cycling in water vapor10.1016/j.actamat.2015.12.053 ↗
8. Yb2Si2O7 environmental barrier coatings deposited by various thermal spray techniques: A preliminary comparative study10.1007/s11666-017-0574-1 ↗
9. Structure, composition, and defect control during plasma spray deposition of ytterbium silicate coatings10.1007/s10853-015-9358-5 ↗
10. Evaluation of CFCC liners with EBC after field testing in a gas turbine10.1016/S0955-2219(02)00142-5 ↗
11. Environmental barrier coatings using low pressure plasma spray process10.1111/jace.17199 ↗
12. Recession behavior of Yb2Si2O7 phase under high speed steam jet at high temperatures10.1016/j.corsci.2007.06.014 ↗
13. Refke, A., Barbezat, G., Dorier, J.L., Gindrat, M., and Hollenstein, C. (2003, January 5–8). Characterization of LPPS processes under various spray conditions for potential applications. Proceedings of the International Thermal Spray Conference, Orlando, FL, USA.10.31399/asm.cp.itsc2003p0581 ↗
14. Substrate temperature effects on splat formation, microstructure development and properties of plasma sprayed coatings Part I: Case study for partially stabilized zirconia10.1016/S0921-5093(99)00459-1 ↗
15. General relationship for the thermal oxidation of silicon10.1063/1.1713945 ↗
16. Hysteresis upon repeated cycling through the beta-alpha cristobalite transformation