2022
DOI: 10.1016/j.corsci.2022.110671
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Femtosecond laser ablation behavior of SiC/SiC composites in air and water environment

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Cited by 21 publications
(3 citation statements)
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“…The microscopic morphology of 2.5-dimensional C/SiC composite grooves after laser ablation was investigated with the laser power of 80 W, scanning speed of 300 mm/s, scanning spacing of 20 μm, scanning times of 20, and scanning frequency of 50 kHz, as shown in Figure 8 . As can be seen from Figure 8 a,b, a large number of powder, loose, and porous ablative oxidation substances appeared on the bottom surface of the ablation groove, the carbon fiber and silicon carbide matrix were almost covered, with only a few fibers and matrix materials leaking out, and the trench bottom of fiber could be found on the bottom surface of grooves, and it was hypothesized that the appearance of this structure was caused by two factors: firstly, the thermal diffusion rate inside the material was not uniform, and the conduction rate along the fiber direction was faster than that in other directions [ 42 ]; secondly, when ablating, the diffuse reflection was produced on the surface of the processed material so that less carbon fiber or matrix material received more energy, and thus more material was removed [ 43 ]. The same phenomenon was found in Figure 8 c, where the bottom of the fiber trench could be observed, and the carbon fiber and silicon carbide matrix were almost covered, but some of the transverse fibers were found to be barely leaking out from the local magnified view, and the fibers and silicon carbide matrix were not uniformly removed at the same time, this was due to the different properties of carbon fiber and silicon carbide matrix materials, the sublimation temperature of SiC matrix was 2700 °C, while the sublimation temperature of carbon fiber was 3550 °C, which was higher than that of SiC, therefore, the carbon fiber was in an incomplete sublimation state and the ablation rate of SiC matrix was faster than that of C fiber [ 44 ].…”
Section: Resultsmentioning
confidence: 99%
“…The microscopic morphology of 2.5-dimensional C/SiC composite grooves after laser ablation was investigated with the laser power of 80 W, scanning speed of 300 mm/s, scanning spacing of 20 μm, scanning times of 20, and scanning frequency of 50 kHz, as shown in Figure 8 . As can be seen from Figure 8 a,b, a large number of powder, loose, and porous ablative oxidation substances appeared on the bottom surface of the ablation groove, the carbon fiber and silicon carbide matrix were almost covered, with only a few fibers and matrix materials leaking out, and the trench bottom of fiber could be found on the bottom surface of grooves, and it was hypothesized that the appearance of this structure was caused by two factors: firstly, the thermal diffusion rate inside the material was not uniform, and the conduction rate along the fiber direction was faster than that in other directions [ 42 ]; secondly, when ablating, the diffuse reflection was produced on the surface of the processed material so that less carbon fiber or matrix material received more energy, and thus more material was removed [ 43 ]. The same phenomenon was found in Figure 8 c, where the bottom of the fiber trench could be observed, and the carbon fiber and silicon carbide matrix were almost covered, but some of the transverse fibers were found to be barely leaking out from the local magnified view, and the fibers and silicon carbide matrix were not uniformly removed at the same time, this was due to the different properties of carbon fiber and silicon carbide matrix materials, the sublimation temperature of SiC matrix was 2700 °C, while the sublimation temperature of carbon fiber was 3550 °C, which was higher than that of SiC, therefore, the carbon fiber was in an incomplete sublimation state and the ablation rate of SiC matrix was faster than that of C fiber [ 44 ].…”
Section: Resultsmentioning
confidence: 99%
“…The equipment diagram for underwater processing is shown in Figure 10. In the water environment, the inhibition of oxidation reaction occurred via a water film during the decomposition process of SiC [104]. The temperature and oxygen content in the ablation area are the main reasons for corrosion mechanisms in both air and water.…”
Section: Underwater Laser Composite Processing Technologymentioning
confidence: 99%
“…A rule of practical significance in high-energy beam heat treatment is revealed, which is also applicable to SiC p /Mg composites etched by a pulsed laser. The energy beam power density q 0 of high-energy beam heat treatment is inversely proportional to the square root of its action time t, which indicates that the larger the power density of high-energy beam action, the shallower the hardening depth [ 28 , 29 , 30 , 31 , 32 , 33 ].…”
Section: Theorymentioning
confidence: 99%