journal article·2020-10-04Open access

High-Porosity Thermal Barrier Coatings from High-Power Plasma Spray Equipment—Processing, Performance and Economics

Nicholas Curry, Matthias Leitner, Karl Körner

Coatings· Volume 10· Issue 10

Abstract

High-porosity thermal barrier coatings are utilized on gas turbine components where maximizing the coating thermal insulation capability is the primary design criteria. Though such coatings have been in industrial use for some time, manufacturing high-porosity coatings quickly and efficiently has proven challenging. With the industry demand to increase productivity and reduce waste generation, there is a drive to look at improved coating manufacturing methods. This article looks at high-porosity coatings manufactured using a high-power plasma system in comparison with a current industrial coating. A commercial spray powder is compared with an experimental Low-Density powder developed to maximize coating porosity without sacrificing coating deposition efficiency. The resultant coatings have been assessed for their microstructure, adhesion strength, furnace cyclic lifetime, thermal conductivity and sintering behavior. Finally, the impact of spray processing on coating economics is discussed. The use of a Low-Density powder with a high-power plasma system allows a high-porosity coating to be manufactured more efficiently and more cost effectively than with conventional powder feedstock. The improvement in thermal properties for the experimental coating demonstrates there is scope to improve industrial coatings by designing with specific thermal resistance rather than thickness and porosity as coating requirements.
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Research context

OpenAlex topics: High-Temperature Coating Behaviors · Catalytic Processes in Materials Science · Particle Dynamics in Fluid Flows

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

Affiliations

Treibacher Industrie AG, 9330 Althofen, Austria

References (54)

Show source-provided references
1. Evolution of thermal insulation of plasma-sprayed thermal barrier coating systems with exposure to high temperature10.1016/j.jeurceramsoc.2019.01.026 ↗
2. Technical and economical aspects of current thermal barrier coating systems for gas turbine engines by thermal spray and EBPVD: A review10.1007/s11666-007-9148-y ↗
3. Lima, R.S. (2020). Perspectives on thermal gradients in porous ZrO2-7–8 wt.% Y2O3 (YSZ) thermal barrier coatings (TBCs) manufactured by air plasma spray (APS). Coatings, 10.10.3390/coatings10090812 ↗
4. The behavior of high-purity, low-density air plasma sprayed thermal barrier coatings10.1016/j.surfcoat.2009.09.065 ↗
5. Thermal shock testing of burner cans coated with a thick thermal barrier coating10.1361/105996398770350828 ↗
6. Some aspects of thick thermal barrier coating lifetime prolongation10.1361/105996399770350197 ↗
7. Taylor, T.A. (1991). Thermal Barrier Coating for Substrates and Process for Producing It. (5073433A), U.S. Patent.
8. Mechanical and thermophysical properties of thick PYSZ thermal barrier coatings: Correlation with microstructure and spraying parameters10.1016/S0257-8972(98)00628-8 ↗
9. Thermophysical properties and thermal cycling behavior of plasma sprayed thick thermal barrier coatings10.1016/j.surfcoat.2004.02.004 ↗
10. Thermal conductivity analysis and lifetime testing of suspension plasma-sprayed thermal barrier coatings10.3390/coatings4030630 ↗
11. Thermal fatigue behavior of thick and porous thermal barrier coatings systems10.1007/s11666-007-9128-2 ↗
12. Evolution of thermal conductivity of dysprosia stabilised thermal barrier coating systems during heat treatment10.1016/j.surfcoat.2012.08.018 ↗
13. Heat transfer through plasma-sprayed thermal barrier coatings in gas turbines: A review of recent work10.1007/s11666-009-9337-y ↗
14. Thermal barrier coating validation testing for industrial gas turbine combustion hardware10.1115/1.4031448 ↗
15. Scheibel, J., and Smith, J.S. (2016). Gas Turbine Low Conductivity Thermal Barrier Coating Validation and Demonstration, European Turbine Network.
16. Failure mechanism for thermal fatigue of thermal barrier coating systems10.1007/s11666-009-9307-4 ↗
17. TBC experience in land-based gas turbines10.1007/s11666-997-0009-5 ↗
18. Damage progression in thermal barrier coating systems during thermal cycling: A nano-mechanical assessment10.1016/j.matdes.2019.107615 ↗
19. Preliminary study on the TriplexPro™-200 gun for atmospheric plasma spraying of yttria-stabilized zirconia10.1016/j.surfcoat.2008.04.012 ↗
20. Process maps for plasma spraying of yttria-stabilized zirconia: An integrated approach to design, optimization and reliability10.1016/j.msea.2008.07.058 ↗
21. Characteristics of conventional and cascaded arc plasma spray-deposited ceramic under standard and high-throughput conditions10.1007/s11666-019-00841-9 ↗
22. Environmental, economical, and performance impacts of Ar-H2 and N2-H2 plasma-sprayed YSZ TBCs10.1007/s11666-019-00955-0 ↗
23. Yttria-stabilized zirconia thermal barriers sprayed using N2-H2 and Ar-H2 plasmas: Influence of processing and heat treatment on coating properties10.1007/s11666-007-9093-9 ↗
24. Advanced oxide powders processing based on cascade plasma10.1088/1742-6596/550/1/012017 ↗
25. Bobzin, K., Ernst, F.B.G., Zwick, J.B., Richardt, K.R.M., Sporer, D., and Molz, R. (2007). Triplex Pro 200: Potentials and advanced applications. Global Coating Solutions, ASM International.10.31399/asm.cp.itsc2007p0723 ↗
26. A Novel single cathode plasma column design for process stability and long component life10.1007/s11666-009-9449-4 ↗
27. Influence of hydrogen on the microstructure of plasma-sprayed yttria-stabilized zirconia coatings10.1361/10599630522422 ↗
28. Influence of plasma spray parameters on formation and morphology of ZrO2−8 wt% Y2O3 deposits10.1111/j.1151-2916.2001.tb00728.x ↗
29. (2009, March 18). ImageJ, Available online: http://imagej.nih.gov/ij/.
30. ISO Standard 18754 (2003). Fine Ceramics (Advanced Ceramics, Advanced Technical Ceramics)—Determination of Density and Apparent Porosity, International Organization for Standardization.
31. Effects of pores and interfaces on effective properties of plasma sprayed zirconia coatings10.1016/S1359-6454(03)00390-2 ↗
32. Effect of the starting microstructure on the thermal properties of as-sprayed and thermally exposed plasma-sprayed YSZ coatings10.1111/j.1551-2916.2009.02953.x ↗
33. Quantification of void network architectures of suspension plasma-sprayed (SPS) yttria-stabilized zirconia (YSZ) coatings using Ultra-small-angle X-ray scattering (USAXS)10.1016/j.msea.2010.06.082 ↗
34. The influence of heat treatments on the porosity of suspension plasma-sprayed yttria-stabilized zirconia coatings10.1007/s11666-017-0682-y ↗
35. ASTM C633 (2017). B08 committee test method for adhesion or cohesion strength of thermal spray coatings. ASTM Int.
36. Studies of the sintering kinetics of thick thermal barrier coatings by thermal diffusivity measurements10.1016/j.jeurceramsoc.2004.01.009 ↗
37. Effect of deposition rate on the stress evolution of plasma-sprayed yttria-stabilized zirconia10.1007/s11666-012-9807-5 ↗
38. EB-PVD process and thermal properties of hafnia-based thermal barrier coating10.1016/S1468-6996(03)00009-3 ↗
39. Thermal cycling behavior and interfacial stability in thick thermal barrier coatings10.1016/j.surfcoat.2010.08.062 ↗
40. Lima, R.S., Nagy, D., and Marple, B.R. (2014). Bond coat engineering influence on the evolution of the microstructure, bond strength, and failure of TBCS subjected to thermal cycling. J. Therm. Spray Technol.10.1007/s11666-014-0181-3 ↗
41. Thermal shock testing of thermal barrier coating/bondcoat systems10.1361/10599490419883 ↗
42. Evaluation of the lifetime and thermal conductivity of dysprosia-stabilized thermal barrier coating systems10.1007/s11666-013-9932-9 ↗
43. Thermal cyclic lifetime and oxidation behavior of air plasma sprayed CoNiCrAlY bond coats for thermal barrier coatings10.1016/j.surfcoat.2008.08.054 ↗
44. A sintering model for plasma-sprayed zirconia thermal barrier coatings. Part II: Coatings bonded to a rigid substrate10.1016/j.actamat.2008.10.058 ↗
45. Microstructure-thermal conductivity relationships for plasma-sprayed yttria-stabilized zirconia coatings10.1111/j.1551-2916.2008.02476.x ↗
46. Sintering studies of plasma-sprayed zirconia10.1016/0257-8972(87)90109-5 ↗
47. XPS investigation of impurity phase segregation in 25.5 wt.% CeO2−2.5 Y2O3−72 ZrO2 plasma-sprayed thermal barrier coatings10.1002/sia.740160193 ↗
48. Influence of impurity content and porosity of plasma-sprayed yttria-stabilized zirconia layers on the sintering behaviour10.1016/S0257-8972(01)01269-5 ↗
49. Effects of impurity content on the sintering characteristics of plasma-sprayed zirconia10.1007/s11666-007-9097-5 ↗
50. Properties and performance of high-purity thermal barrier coatings10.1007/s11666-007-9079-7 ↗
51. Impact of impurity content on the sintering resistance and phase stability of dysprosia- and yttria-stabilized zirconia thermal barrier coatings10.1007/s11666-013-0014-9 ↗
52. The effect of a high thermal gradient on sintering and stiffening in the top coat of a thermal barrier coating system10.1361/10599630420380 ↗
53. Thermal gradient behavior of TBCS subjected to a laser gradient test rig: Simulating an air-to-air combat flight10.1007/s11666-015-0311-6 ↗
54. Insights on the high-temperature operational limits of ZrO2-Y2O3 TBCs manufactured via air plasma spray10.1007/s11665-017-2562-5 ↗