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13篇 您的检索式:作者名="SCITI Diletta"
    题名 作者 年代 出处 被引量
1Microstructure and mechanical properties of ZrB 2 –MoSi 2 ceramic composites produced by different sintering techniques显示文摘Diletta Sciti Frédéric Monteverde Stefano Guicciardi Giuseppe Pezzotti Alida Bellosi 2006Materials Science & Engineering A2006,,1:2
2Spark plasma sintering and mechanical behavior of ZrC-based composites 显示文摘Diletta Sciti Stefano Guicciardi Mats Nygren 2008Scripta Materialia2008,59,6:1
3Processing, sintering and oxidation behavior of SiC fibers reinforced ZrB 2 composites显示文摘Diletta Sciti Laura Silvestroni 2011Journal of the European Ceramic Society2011,,9:1
4TEM analysis, mechanical characterization and oxidation resistance of a highly refractory ZrB 2 composite显示文摘Laura Silvestroni Diletta Sciti 2014Journal of Alloys and Compounds2014,,:1
5Spark plasma sintering and mechanical behaviour of ZrC-based composites显示文摘Diletta Sciti Stefano Guicciardi Mats Nygren 2008Scripta Materialia2008,,6:1
6Microstructttre and mechanical properties of ZrB2-MoSi2 ceramic composites produced by different sintering techniques 显示文摘SCITI Diletta MONTEVERDE Frederic GUICCIARDI Stefano 2006Mater Sci Eng A2006,434,12:1
7Processing, sintefing and oxidation behavior of SiC fibers reinforced ZrB2 composites 显示文摘Diletta Sciti Laura Silvestrnni 2012Journal of the European Ceramic Society2012,32,9:1
8Influence of long term oxidation on the microstructure,mechanical and electrical properties of pressureless Sintered AlN-SiC-MoSi2 ceramic composites显示文摘Krnel Kristoffer Sciti Diletta Bellosi Alida 2003Journal of the European Ceramic Society2003,23,:1
9Surface modification and oxidation kinetics of hot-pressed AlN-SiC-MoSi2 electroconductive ceramic composite显示文摘Krnel Kristoffer Sciti Diletta Landi Elena 2003Applied Surface Science2003,210,:1
10Long-term oxidation behavior and mechanical strength degradation of a pressurelessly sintered ZrB 2 –MoSi 2 ceramic显示文摘Diletta Sciti Mylène Brach Alida Bellosi 2005Scripta Materialia2005,,11:1
11Propulsion tests on ultra-high-temperature ceramic matrix composites for reusable rocket nozzles显示文摘Ultra-high-temperature ceramic matrix composites(UHTCMCs)based on a ZrB_(2)/SiC matrix have been investigated for the fabrication of reusable nozzles for propulsion.Three 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 reusability.Sections were extracted after oxidation tests to study the microstructural changes and oxidative and thermomechanical stresses induced by the repeated tests.Compared to a reference graphite nozzle,no measurable erosion was observed for the UHTCMC-based nozzles.The 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 oxidation.Both specimens obtained by HP and SPS displayed similar performance,with very slight differences,which were attributed to small changes in porosity.These 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.Diletta Sciti Antonio Vinci Luca Zoli Pietro Galizia Simone Failla Stefano Mungiguerra Giuseppe D.Di Martino Anselmo Cecere Raffaele Savino 2023Journal of Advanced Ceramics2023,12,7:0
12ZrB_(2)-SiC ceramics toughened with oriented paper-derived graphite for a sustainable approach显示文摘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 sector.Reinforcement 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 graphite.The 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 sintering.Cellulose filter paper was selected because it undergoes thermolysis with no melting stage forming a strong carbonaceous residue that can be used as toughener.Microstructure 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 studied.Addition 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 reinforcement.The high-temperature properties,such as strength and toughness as well as oxidation resistance at 1500℃,were also examined.Luca Zoli Francesca Servadei Simone Failla Matteo Mor Antonio Vinci Pietro Galizia Diletta Sciti 2024Journal of Advanced Ceramics2024,13,2:0
13A novel approach for manufacturing of layered,ultra-refractory composites using pliable,short fibre-reinforced ceramic sheets显示文摘A new additive technique for manufacturing of short fibre-reinforced ultra-refractory ceramics is presented.This 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 possible.The amount of short carbon fibres incorporated in the sheets ranged from 20 to 50 vol%,whereas the fibre length ranged from 3 to 5 mm.The 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 observed.Four-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%).Matteo MOR Antonio VINCI Simone FAILLA Pietro GALIZIA Luca ZOLI Diletta SCITI 2023Journal of Advanced Ceramics2023,12,1:0
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