Ceramic Matrix Composites 2014
DOI: 10.1002/9781118832998.ch5
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Carbon/Carbons and their Industrial Applications

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Cited by 10 publications
(7 citation statements)
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“…From a thermal viewpoint, it appears from Fig. (11) that the evolutions of the temperatures at selected locations have been quite well reproduced, with a notable exception at the top of the preform, a region where expulsion of the liquid from the preform has been predicted but not achieved experimentally, as opposed to the rest of the preform. From the time evolutions of the temperature and porosity fields reported in Figure (12), it is seen that the infiltration reproduces again the "trilby hat" effect, though only with a slight depletion of the density in the middle of the preform section, accompanied by a strong decrease of the space gradient of temperature in the central region.…”
Section: 1 Direct Numerical Simulationsmentioning
confidence: 89%
See 1 more Smart Citation
“…From a thermal viewpoint, it appears from Fig. (11) that the evolutions of the temperatures at selected locations have been quite well reproduced, with a notable exception at the top of the preform, a region where expulsion of the liquid from the preform has been predicted but not achieved experimentally, as opposed to the rest of the preform. From the time evolutions of the temperature and porosity fields reported in Figure (12), it is seen that the infiltration reproduces again the "trilby hat" effect, though only with a slight depletion of the density in the middle of the preform section, accompanied by a strong decrease of the space gradient of temperature in the central region.…”
Section: 1 Direct Numerical Simulationsmentioning
confidence: 89%
“…This composite structure confers them a non-brittle behavior with progressive damage during loading, therefore countering the largest weakness of ceramics as structural materials. Successful applications of C/C composites encompass aircraft braking discs [7], solid rocket motor throttles and divergents [8], thermal protection systems for atmospheric re-entry [9], ion thruster grids [10] and other applications in industry [11,12]. C/SiC composites [13] were designed to overcome the poor oxidation resistance of C/C composites, with successful applications as automotive braking discs [14], rocket nozzles [15], thermal protection systems, parts for industrial furnace management [16] and in aeronautic propulsion [17,18].…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, in some long fibres CMCs, the matrix itself can be a particulate ceramic, as it is the case of some melt infiltrated SiC/SiC. Ghosh et al [13,14] studied the behaviour of a particulate ZrB2-SiC when performing scratch tests at different loads. Even if the main objective of the study was not to understand the material removal mechanism but to comprehend the impact resistance, similarities in the results can be obtained as very small uncut chip thickness are normally used when machining hard ceramics/CMCs.…”
Section: Figure 5 Sem Images Of a C/sic With A Scratch Angle Of (A) 90° And (B) 45°mentioning
confidence: 99%
“…The chemical vapor infiltration (CVI) process is one of the routes used for the manufacturing of ceramic-matrix composites [1,2], among which SiC-matrix composites [3,4], ultra-high temperature ceramics (UHTCs) [5], and especially carbon-fiber-reinforced carbon (C f /C) composites [6,7]. This process, a variation of chemical vapor deposition (CVD) [8], has the advantage of producing high-quality matrices without damaging to the fibers, thus allowing a nearly optimal performance of the constituents in the composite [9,10].…”
Section: Introductionmentioning
confidence: 99%