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Preparation and Arc Erosion Resistance of C_f/Cu Composite by Vacuum Melting Infiltration 被引量:4
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作者 张华煜 LIU Yiwen +1 位作者 ZHAO Xianling luan xingang 《Journal of Wuhan University of Technology(Materials Science)》 SCIE EI CAS 2014年第5期1039-1043,共5页
Cf/Cu composite was prepared by vacuum melting infiltration. Ti and Cr were doped to the Cu alloy to improve the wettability between Cu and carbon. The microstrueture was investigated by XRD, SEM and EDS. The arc eros... Cf/Cu composite was prepared by vacuum melting infiltration. Ti and Cr were doped to the Cu alloy to improve the wettability between Cu and carbon. The microstrueture was investigated by XRD, SEM and EDS. The arc erosion rate of Cf/Cu composite was investigated in vacuum. The results showed that the Ti and Cr could improve the wettability between Cu and C/C preform and the infiltration ability of Cu into C/ C preform greatly. A TiC interface formed between the fibers and matrix. The good bonding between the fiber and matrix guaranteed that part of the Cu matrix can still be bonded on the fibers even when the material was exposed to the plasma. Consequently, the carbon fibers were protected from the erosion. In comparison, Cu was completely consumed by the arc erosion. Hence, the graphite was eroded and presented a cauliflower-like morphology. Therefore, the prepared C/Cu bad better ability to resist the arc erosion, compared with common Cu-C material. 展开更多
关键词 Cf/Cu composite vacuum melting infiltration arc erosion
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强噪声激励下C/SiC复合材料壁板动态响应与失效分析 被引量:4
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作者 吴振强 刘宝瑞 +3 位作者 贾洲侠 王英诚 栾新刚 陈博 《复合材料学报》 EI CAS CSCD 北大核心 2019年第5期1254-1262,共9页
高超声速飞行器热防护系统和热结构包含多种形式的复合材料薄壁结构,对巡航或再入飞行中的强噪声环境十分敏感和易发生失效破坏,严重威胁着飞行器结构的完整性和可靠性。为考核复合材料薄壁结构的耐噪声性能,基于高声强行波管噪声试验系... 高超声速飞行器热防护系统和热结构包含多种形式的复合材料薄壁结构,对巡航或再入飞行中的强噪声环境十分敏感和易发生失效破坏,严重威胁着飞行器结构的完整性和可靠性。为考核复合材料薄壁结构的耐噪声性能,基于高声强行波管噪声试验系统,选取厚度为1~3mm的C/SiC复合材料平板作为试验件,试验件四周采用螺栓进行固定安装。通过开展156~165dB噪声激励动态响应试验,获得了不同量级噪声作用下的动态响应变化规律。针对厚度为1mm的试验件开展了失效试验,在168dB噪声作用下,试验件发生了迅速破坏,采用红外无损检测设备对失效后的C/SiC复合材料平板进行检测,采用SEM对断面形貌进行观察,揭示出强噪声激励下的失效模式,可为高温复合材料结构优化设计和耐噪声失效性能评估提供技术支撑。 展开更多
关键词 高超声速飞行器 C/SIC复合材料 平板 噪声载荷 加速度 动态应变 失效模式
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Laser ablation behaviors of C/SiC composites in air 被引量:1
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作者 SU Meng CHENG Laifei +1 位作者 luan xingang ZHANG Litong 《复合材料学报》 EI CAS CSCD 北大核心 2013年第6期37-47,共11页
Ablation behaviors of silicon carbide(SiC)coated 2Dcarbon fiber reinforced silicon carbide matrix(designated as 2DC/SiC)composites prepared by chemical vapor infiltration(CVI)were investigated by a continuous wave CO2... Ablation behaviors of silicon carbide(SiC)coated 2Dcarbon fiber reinforced silicon carbide matrix(designated as 2DC/SiC)composites prepared by chemical vapor infiltration(CVI)were investigated by a continuous wave CO2 laser.The 2DC/SiC specimens were exposed under laser for 0.5sin ambient air,and the laser powers varied from 500Wto 1500W.A 3Dfinite element model was established to calculate the temperature distribution in the laser ablation process.The ablation depth,width and profile were measured by Laser Confocal Microscope(LCM).The results indicate that the increase of ablation depth follows a linear relation with the increase of laser power,and the increase of ablation width follows a similar trend with the increase of the isotherm diameter of 1712℃.The ablated surface can be distinguished into three different regions by scanning electron microscope(SEM)observation,including ablation center,transition zone and ablation fringe.The ablation behaviors of carbon fibers and SiC matrices in different regions were presented and discussed in the study. 展开更多
关键词 《复合材料学报》 期刊 编辑部 编辑工作 读者
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