Abstract
AbstractThermal barrier coatings are essential materials systems for insulating and protecting substrates exposed to high temperatures. In such systems, the heat transfer has three possible paths: conduction, convection and irradiation. The higher the operating temperature, the more important it is to control or protect against the radiative component, since the radiative heat flux becomes non-negligible. The radiation can be controlled by the use of ceramic-based photonic nanostructures, namely photonic crystals and photonic glasses, creating so-called reflective thermal barrier coatings. In this work, mullite inverse photonic glasses (PhG) have been produced by thermally induced reaction on sol–gel-based silica structures coated with nanometric films of Al2O3 by atomic layer deposition. The conversion to mullite was carried out following a two-stage heat-treatment. The pre-annealing associated with the further mullite formation results in an excellent structural stability of these PhGs up to 1500 °C, being able to retain their high reflectivity in the near infrared range. Therefore, this structure can be considered for next-generation reflective thermal barrier coatings.
Graphical abstract
Funder
Deutsche Forschungsgemeinschaft
Technische Universität Hamburg
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Reference51 articles.
1. Vassen R, Stuke A, Stoever D (2009) Recent developments in the field of thermal barrier coatings. J Therm Spray Technol 18:181–186. https://doi.org/10.1007/s11666-009-9312-7
2. Soechting FO (1999) A design perspective on thermal barrier coatings. J Therm Spray Technol 8:505–511. https://doi.org/10.1361/105996399770350179
3. Cao XQ, Vassen R, Stoever D (2004) Ceramic materials for thermal barrier coatings. J Eur Ceram Soc 24:1–10. https://doi.org/10.1016/S0955-2219(03)00129-8
4. Patnaik P, Huang X, Singh J (2006) State of the art and future trends in the development of thermal barrier coating systems. The NATO Research & Technology Organisation RTO-MP-AVT-135. vol 38, p 1–20
5. Kelly MJ, Wolfe DE, Singh J, Eldridge J, Zhu DM, Miller R (2006) Thermal barrier coatings design with increased reflectivity and lower thermal conductivity for high-temperature turbine applications. Int J Appl Ceram Technol 3:81–93. https://doi.org/10.1111/j.1744-7402.2006.02073.x
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献