Production and characterization of Alumina-Titania-ítria ceramics composites for thermal barrier aerospace exhaust system.

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Abstract
09-101 YOGENDRA PRASAD YADAVA De Albuquerque, L.T.(UNIVERSIDADE FEDERAL DE PERNAMBUCO); GOMES, N.L.(Universidade Federal de Pernambuco); Ferreira, R.A.(Universidade Federal de Pernambuco); YADAVA, Y.P.(UNIVERSIDADE FEDERAL DE PERNAMBUCO); In aerospace industry, Gas turbines, which are responsible for aircraft propulsion, have exhaust nozzles formed by a set of nickel or cobalt-based alloys, and are among the most prematurely failed equipment due to such elevated temperatures. Therefore, turbine manufacturers are looking for an improvement in these hot section components. Ceramic composites can be a solution, since these materials have the capacity to withstand high temperatures and require less air cooling, besides the possibility of acquiring lighter parts for their equipment, aiming to optimize the performance of these systems and achieve lower fuel consumption. Previous studies have shown that alumina-based ceramics incorporated with other oxides, present higher mechanical properties than other ceramic materials, obtaining properties such as chemical stability, resistance to high temperatures and fracture toughness. In the present work, Alumina-titania ceramic composites (Al2O3-TiO2) incorporated with rare earth oxide (Y2O3), varying the content of yttrium oxide by 5%, 10% and 15% were produced for aerospacial application The composites were produced by thermo mechanical process and sintered at 1350 ° C. The structure, microstructure and mechanical properties of the composites were studied by X-ray diffraction, relative density, scanning electron microscopy and Vickers micro hardness. The results showed good homogeneity in distribution and particle size. The Vickers micro hardness test for composites of 10 and 15% of yttria obtained close results when compared to the 5% of yttria, which have higher values. The results indicate good <!--[if gte mso 9]>
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