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ZrB_(2)-SiC ceramics toughened with oriented paper-derived graphite for a sustainable approach

Journal of Advanced Ceramics 2024年第2期13卷 207-219页

作者： Luca Zoli Francesca Servadei Simone Failla Matteo Mor Antonio Vinci pietro galizia Diletta Sciti CNR-ISSMC Institute of ScienceTechnology and Sustainability for CeramicsFaenza I-48018Italy

Carbon fibre-reinforced ultra-high temperature ceramics(UHTCs)are considered a class of promising materials for several applications,the most appealing ones being in the aerospace *** is necessary to overcome the brittleness and low thermal shock resistance of ceramics and is often provided through the addition of carbon fibres or other carbon-based phases,such as nanotubes,graphene,and *** present work is focused on the toughening of UHTCs through incorporation of 30-50 vol% thin,ordered graphite layers from conventional filter paper followed by hot pressing *** filter paper was selected because it undergoes thermolysis with no melting stage forming a strong carbonaceous residue that can be used as *** and mechanical properties of toughened composites were compared to those of other materials reinforced with short carbon fibres and the effect of different distribution of graphite was *** of graphite allowed toughness to be increased from 3−4 MPa·m^(1/2)(for unreinforced materials)to 5.1−5.5 MPa·m^(1/2),similar to results obtained with short fibre *** high-temperature properties,such as strength and toughness as well as oxidation resistance at 1500℃,were also examined.

关键词： borides paper-derived graphite microstructure toughness sustainability

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A novel approach for manufacturing of layered,ultra-refractory composites using pliable,short fibre-reinforced ceramic sheets

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Journal of Advanced Ceramics 2023年第1期12卷 155-168页

作者： Matteo MOR Antonio VINCI Simone FAILLA pietro galizia Luca ZOLI Diletta SCITI ISSMC-CNR Institute of ScienceTechnology and Sustainability for CeramicsVia Granarolo 6448018 Faenza(RA)Italy

A new additive technique for manufacturing of short fibre-reinforced ultra-refractory ceramics is *** technique allows the fabrication of solvent-free,thin(~100µm),flexible,and easy-to-handle sheets suitable for fabricating homogeneous or layered structures.A large range of compositions,in terms of matrix and fibre volumetric contents,from 0%to 100%is *** amount of short carbon fibres incorporated in the sheets ranged from 20 to 50 vol%,whereas the fibre length ranged from 3 to 5 *** matrix composition investigated with this technique consisted of ZrB_(2)/SiC/Y_(2)O_(3).By increasing the fibre amount from 35 to 50 vol%,an improvement of mechanical properties was ***-point flexural strength(σ)ranged from 107 to 140 MPa,depending on the amount of carbon fibres(Cf).The same holds true for the work of fracture,ranging from 108 to 253 J/m^(2).Functionally graded composites were fabricated by overlapping sheets with a fibre gradient(0%-50%).

关键词： ultra-high-temperature ceramics(UHTCs) ceramic matrix composites(CMCs) short carbon fibres mechanical properties

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Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles

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Journal of Advanced Ceramics 2023年第7期12卷 1345-1360页

作者： Diletta Sciti Antonio Vinci Luca Zoli pietro galizia Simone Failla Stefano Mungiguerra Giuseppe D.Di Martino Anselmo Cecere Raffaele Savino Institute of Science Technology and Sustainability for Ceramics-National Research CouncilFaenza 48018Italy Department of Industrial Engineering University of Naples Federico IINaples 80125Italy

Ultra-high-temperature ceramic matrix composites(UHTCMCs)based on a ZrB_(2)/SiC matrix have been investigated for the fabrication of reusable nozzles for *** de Laval nozzle prototypes,obtained by sintering with either hot pressing(HP)or spark plasma sintering(SPS),were tested 2-3 times in a hybrid rocket motor for proving *** were extracted after oxidation tests to study the microstructural changes and oxidative and thermomechanical stresses induced by the repeated *** to a reference graphite nozzle,no measurable erosion was observed for the UHTCMC-based *** oxidation mechanism consisted in the formation of a ZrO_(2)intermediate layer,with a liquid silicon oxide(SiO_(2))layer on the surface that was displaced by the action of the gas flux towards the divergent part of the nozzle,protecting it from further *** specimens obtained by HP and SPS displayed similar performance,with very slight differences,which were attributed to small changes in *** tests demonstrated the capability of complex-shaped prototypes made of the developed UHTCMCs to survive repeated exposure to environments representative of a realistic space propulsion application,for overall operating time up to 30 s,without any failure nor measurable erosion,making a promising step towards the development of reusable rocket components.

关键词： ultra-high-temperature ceramics(UHTCs) ceramic matrix composites(CMCs) propulsion oxidation resistance nozzle prototypes

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