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The influence of ablation products on the ablation resistance of C/C-SiC composites and the growth mechanism of SiO_2 nanowires
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作者 李县辉 燕青芝 +3 位作者 米应映 韩永军 温馨 葛昌纯 《Chinese Physics B》 SCIE EI CAS CSCD 2015年第2期7-11,共5页
Ablation under oxyacetylene torch with heat flux of 4186.8(10%kW/m2 for 20 s was performed to evaluate the ablation resistance of C/C-SiC composites fabricated by chemical vapor infiltration(CVI) combined with liqu... Ablation under oxyacetylene torch with heat flux of 4186.8(10%kW/m2 for 20 s was performed to evaluate the ablation resistance of C/C-SiC composites fabricated by chemical vapor infiltration(CVI) combined with liquid silicon infiltration(LSI) process.The results indicated that C/C-SiC composites present a better ablation resistance than C/C composites without doped SiC.The doped SiC and the ablation products SiO2 derived from it play key roles in ablation process.Bulk quantities of SiO2 nanowires with diameter of 80 nm-150 nm and length of tens microns were observed on the surface of specimens after ablation.The growth mechanism of the SiO_2 nanowires was interpreted with a developed vapor-liquid-solid(VLS) driven by the temperature gradient. 展开更多
关键词 c/c-sic composites ablation products SiO2 nanowires growth mechanism
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碳组分对轨道交通C/C-SiC制动盘摩擦性能的影响
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作者 吴小军 张栖岩 +3 位作者 史耀君 杨云鹏 庞菲 胡一杰 《轨道交通材料》 2025年第1期10-15,共6页
采用2.5D无纬布/网胎叠层针刺预制体,通过化学气相渗透、树脂浸渍碳化制备了密度1.40~1.45 g/cm^(3)的热解碳、热解碳-树脂碳组分C/C坯体,再经高温热处理、净尺寸加工及反应熔渗硅获得两种C/C-SiC制动盘,分析了碳组分对C/C-SiC材料物相... 采用2.5D无纬布/网胎叠层针刺预制体,通过化学气相渗透、树脂浸渍碳化制备了密度1.40~1.45 g/cm^(3)的热解碳、热解碳-树脂碳组分C/C坯体,再经高温热处理、净尺寸加工及反应熔渗硅获得两种C/C-SiC制动盘,分析了碳组分对C/C-SiC材料物相含量、微观结构的影响;通过1∶4高速列车台架试验,对比研究了两种C/C-SiC制动盘匹配粉末冶金闸片,在不同制动压力、制动速度下的摩擦性能。结果表明,不同碳组分材料的陶瓷化性能有一定差异,树脂碳的引入改善了孔隙结构,产生均匀的陶瓷相,残留Si少,制备的C/C-SiC更致密。在50~300 km/h制动速度下,摩擦因数变化呈先快速上升后缓慢下降再逐渐平稳的趋势,150 km/h制动速度下两种制动盘摩擦因数均接近峰值;随着制动压力增加,热解碳组分C/C-SiC盘的摩擦因数呈下降趋势,热解碳+树脂碳双组分C/C-SiC盘的摩擦因数稳定在0.60~0.72。 展开更多
关键词 碳组分 摩擦性能 c/c-sic制动盘 反应熔渗 微结构
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Ablation Processes for HfC-Coated 2.5D Needle-Punched Composites Used for Aerospace Engines Under Hypersonic Flight Conditions
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作者 ZHANG Ziyi SHI Zhenyu +2 位作者 NI Jing WANG Jilai ZHANG Chengpeng 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2024年第5期645-655,共11页
The working environment of aerospace engines is extremely harsh with temperature exceeding 1700℃and accompanied by thermal coupling effects.In this condition,the materials employed in hypersonic aircraft undergo abla... The working environment of aerospace engines is extremely harsh with temperature exceeding 1700℃and accompanied by thermal coupling effects.In this condition,the materials employed in hypersonic aircraft undergo ablation issues,which can cause catastrophic accidents.Due to the excellent high-temperature stability and ablation resistance,HfC exhibits outstanding thermal expansion coefficient matching that of C/SiC composites.2.5D needle-punched C/SiC composites coated with HfC are prepared using a plasma spraying process,and a high-enthalpy arc-heated wind tunnel is employed to simulate the re-entry environment of aircraft at 8 Mach and an altitude of 32 km.The plasma-sprayed HfC-coated 2.5D needle-punched C/SiC composites are subjected to long-term dynamic testing,and their properties are investigated.Specifically,after the thermal assessment ablation experiment,the composite retains its overall structure and profile;the total mass ablation rate is 0.07445 g/s,the average linear ablation rate in the thickness direction is-0.0675μm/s,and the average linear ablation rate in the length direction is 13.907μm/s.Results verify that plasma-sprayed HfC coating exhibits excellent anti-oxidation and ablation resistance properties.Besides,the microstructure and ablation mechanism of the C/SiC composites are studied.It is believed that this work will offer guideline for the development of thermal protection materials and the assessment of structural thermal performance. 展开更多
关键词 2.5D needle-punched c/Sic composites ablation mechanism arc-heated wind tunnel experiment high enthalpy flow
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液体冲压发动机燃烧室C/C-SiC复合材料的烧蚀行为及力学性能
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作者 王玲玲 姜韬 +2 位作者 高勇 闫联生 郭春园 《材料工程》 EI CAS CSCD 北大核心 2024年第11期118-124,共7页
采用固体粒子和不含固体粒子在不同含氧量下的液体冲压发动机对C/C-SiC复合材料燃烧室内层进行测试,研究两种实验条件下烧蚀严重区域和一般区域的烧蚀量、烧蚀行为及材料烧蚀后的力学性能。结果表明:在含固体粒子条件下,烧蚀严重区域烧... 采用固体粒子和不含固体粒子在不同含氧量下的液体冲压发动机对C/C-SiC复合材料燃烧室内层进行测试,研究两种实验条件下烧蚀严重区域和一般区域的烧蚀量、烧蚀行为及材料烧蚀后的力学性能。结果表明:在含固体粒子条件下,烧蚀严重区域烧蚀量较大,而一般区域也有一定的烧蚀量,均比不含固体粒子条件下相应区域烧蚀量大;C/C-SiC复合材料表面涂层先发生氧化反应,生成的SiO_(2)玻璃态膜覆盖在涂层表面,阻挡了氧气的进入,有效地保护了基体材料。随着温度不断上升,材料发生主动氧化,气流的剥蚀和冲刷会加速该过程,使得SiO_(2)难以附着在产品内表面上,SiC基体和碳纤维失去保护而被损耗。纤维变细,强度逐渐降低,纤维的增韧效果大幅减小,两种实验条件下C/C-SiC复合材料的弯曲强度和剪切强度均发生了下降,在颗粒冲刷下,材料的力学性能损失更加严重。 展开更多
关键词 c/c-sic燃烧室 液体冲压 固体粒子 烧蚀行为 力学性能
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不同预制体结构制备C/C-SiC复合材料的微观结构演变及力学性能
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作者 魏琰斌 王雅雷 +2 位作者 熊翔 叶志勇 刘在栋 《材料工程》 EI CAS CSCD 北大核心 2024年第10期127-138,共12页
采用缝合结构与针刺结构碳纤维预制体,经化学气相渗透法(CVI)和反应熔渗法(RMI)制备出C/C-SiC复合材料,系统研究了两种结构预制体制得的C/C多孔体微观结构、孔隙特征及C/C-SiC复合材料微观结构和弯曲性能。结果表明:缝合结构C/C多孔体... 采用缝合结构与针刺结构碳纤维预制体,经化学气相渗透法(CVI)和反应熔渗法(RMI)制备出C/C-SiC复合材料,系统研究了两种结构预制体制得的C/C多孔体微观结构、孔隙特征及C/C-SiC复合材料微观结构和弯曲性能。结果表明:缝合结构C/C多孔体孔径呈双峰分布,孔隙多为纤维束间孔,针刺结构C/C多孔体孔径呈单峰分布,由于网胎的加入使得部分纤维束间孔转变为连通的小孔隙网络,经过模拟后者Z向绝对渗透率略大于前者,有利于后者后续RMI致密化过程(高密度,低开孔率,低残余金属);缝合结构C/C-SiC复合材料平均弯曲强度高于针刺结构C/C-SiC复合材料,二者都呈现“假塑性”断裂方式;针刺结构C/C-SiC复合材料密度更高,残余Si含量更低,但其纤维体积含量较低,长直纤维的完整性较差,使得复合材料承载性能较低。 展开更多
关键词 c/c-sic复合材料 孔隙结构 微观结构 弯曲性能
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Compositional and Hollow Engineering of Silicon Carbide/Carbon Microspheres as High-Performance Microwave Absorbing Materials with Good Environmental Tolerance 被引量:5
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作者 Lixue Gai Yahui Wang +5 位作者 Pan Wan Shuping Yu Yongzheng Chen Xijiang Han Ping Xu Yunchen Du 《Nano-Micro Letters》 SCIE EI CAS CSCD 2024年第9期128-146,共19页
Microwave absorbing materials(MAMs)characterized by high absorption efficiency and good environmental tolerance are highly desirable in practical applications.Both silicon carbide and carbon are considered as stable M... Microwave absorbing materials(MAMs)characterized by high absorption efficiency and good environmental tolerance are highly desirable in practical applications.Both silicon carbide and carbon are considered as stable MAMs under some rigorous conditions,while their composites still fail to produce satisfactory microwave absorption performance regardless of the improvements as compared with the individuals.Herein,we have successfully implemented compositional and structural engineering to fabricate hollow Si C/C microspheres with controllable composition.The simultaneous modulation on dielectric properties and impedance matching can be easily achieved as the change in the composition of these composites.The formation of hollow structure not only favors lightweight feature,but also generates considerable contribution to microwave attenuation capacity.With the synergistic effect of composition and structure,the optimized SiC/C composite exhibits excellent performance,whose the strongest reflection loss intensity and broadest effective absorption reach-60.8 dB and 5.1 GHz,respectively,and its microwave absorption properties are actually superior to those of most SiC/C composites in previous studies.In addition,the stability tests of microwave absorption capacity after exposure to harsh conditions and Radar Cross Section simulation data demonstrate that hollow SiC/C microspheres from compositional and structural optimization have a bright prospect in practical applications. 展开更多
关键词 Sic/c composites compositional engineering Hollow engineering Microwave absorption Environmental tolerance
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2.5D C/SiC复合材料磁场/液体辅助皮秒激光制孔试验研究
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作者 刘畅 王科骄 李丞 《航空制造技术》 北大核心 2025年第1期54-63,共10页
2.5D C/SiC复合材料是航空国防领域耐高温构件用关键复合材料,其高硬度、高耐磨性使该材料的高质量微孔加工异常困难。本文提出了一种基于磁场/液体辅助(MLM)的2.5D C/SiC复合材料皮秒激光制孔工艺,通过提取微孔的出/入口直径、锥度、... 2.5D C/SiC复合材料是航空国防领域耐高温构件用关键复合材料,其高硬度、高耐磨性使该材料的高质量微孔加工异常困难。本文提出了一种基于磁场/液体辅助(MLM)的2.5D C/SiC复合材料皮秒激光制孔工艺,通过提取微孔的出/入口直径、锥度、氧化、重铸层等特征,与皮秒激光加工(PM)、磁场辅助加工(MM)、液体辅助加工(LM)3种工艺进行了对比研究。结果表明,基于MLM的皮秒激光加工能够有效降低微孔的入口直径,同时增大出口直径,在两组不同的试验参数下分别获得了锥度1.3°及1.1°的微孔,比PM工艺的锥度分别降低了18.75%和45%,比MM工艺的锥度分别降低了13.33%和31.25%,比LM工艺的锥度分别降低了91.22%和79.63%。此外,利用EDS能谱分析、拉曼光谱以及XPS技术对制备的微孔开展了微观组织分析。可以发现,MLM工艺更有效地减少了孔壁的石墨化缺陷。其中,液体辅助避免了微孔入口处的氧化,同时清晰地观察到裸露的纤维和基体,有效避免了热损伤和重铸层缺陷。在皮秒激光制孔中,MLM的主要作用机制体现在液体的冷却效应、隔绝氧气机制,以及磁场纵向拉伸等离子体,从而减弱等离子体屏蔽效应。 展开更多
关键词 皮秒激光 磁场/液体辅助加工 2.5D c/Sic复合材料 孔锥度 烧蚀机理
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Yolk-shell Si/C composites with multiple Si nanoparticles encapsulated into double carbon shells as lithium-ion battery anodes 被引量:11
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作者 Le Hu Bin Luo +3 位作者 Chenghao Wu Pengfei Hu Lianzhou Wang Haijiao Zhang 《Journal of Energy Chemistry》 SCIE EI CAS CSCD 2019年第5期124-130,共7页
The conceptual design of yolk-shell structured Si/C composites is considered to be an effective way to improve the recyclability and conductivity of Si-based anode materials. Herein, a new type of yolk-shell structure... The conceptual design of yolk-shell structured Si/C composites is considered to be an effective way to improve the recyclability and conductivity of Si-based anode materials. Herein, a new type of yolk-shell structured Si/C composite (denoted as TSC-PDA-B) has been intelligently designed by rational engineering and precise control. In the novel structure, the multiple Si nanoparticles with small size are successfully encapsulated into the porous carbon shells with double layers benefiting from the strong etching effect of HF. The TSC-PDA-B product prepared is evaluated as anode materials for lithium-ion batteries (LIBs). The TSC-PDA-B product exhibits an excellent lithium storage performance with a high initial capacity of 2108 mAh g^-1 at a current density of 100 mA g^-1 and superior cycling performance of 1113 mAh g^-1 over 200 cycles. The enhancement of lithium storage performance may be attributed to the construction of hybrid structure including small Si nanoparticles, high surface area, and double carbon shells, which can not only increase electrical conductiv让y and intimate electrical contact with Si nanoparticles, but also provide built-in buffer voids for Si nanoparticles to expand freely without damaging the carbon layer. The present findings can provide some scientific insights into the design and the application of advanced Si-based anode materials in energy storage fields. 展开更多
关键词 Si/c composites Yolk-shell Multiple SI nanoparticles Double cARBON SHELLS Energy storage
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Three-Dimensional Reconstructed Finite Element Model for C/C Composites by Micro-CT 被引量:3
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作者 张海军 周储伟 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2015年第6期639-645,共7页
The precise microscopic feature of carbon-carbon(C/C) composites is essential {or an accurate predic tion of their mechanical behavior. After fabrication, actual microscopic feature differs from simple ideal spatial... The precise microscopic feature of carbon-carbon(C/C) composites is essential {or an accurate predic tion of their mechanical behavior. After fabrication, actual microscopic feature differs from simple ideal spatial model. Micro computed lomography(CT) scan can well describe internal microstruetures of composites. Therefore, a reconstructed model is developed based on mireo-CT, by a series of prodcedures including extrac tlng components, generating new binary images and establishing a finite element (FE) model. Compared with the model designed by reconstructed commercial software MIMICS. the presented reconstructed FE model is superior in terms of high mesh quality and eontrollable mesh cluantity. The precision of the model is verified by experiment. 展开更多
关键词 c/c composites mirco-cF binary image reconstructed procedure finite element model
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Non‑Magnetic Bimetallic MOF‑Derived Porous Carbon‑Wrapped TiO2/ ZrTiO4 Composites for Efficient Electromagnetic Wave Absorption 被引量:18
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作者 Jing Qiao Xue Zhang +7 位作者 Chang Liu Longfei Lyu Yunfei Yang Zhou Wang Lili Wu Wei Liu Fenglong Wang Jiurong Liu 《Nano-Micro Letters》 SCIE EI CAS CSCD 2021年第5期45-60,共16页
Modern communication technologies put forward higher requirements for electromagnetic wave(EMW)absorption materials.Metal-organic framework(MOF)derivatives have been widely concerned with its diverse advantages.To bre... Modern communication technologies put forward higher requirements for electromagnetic wave(EMW)absorption materials.Metal-organic framework(MOF)derivatives have been widely concerned with its diverse advantages.To break the mindset of magneticderivative design,and make up the shortage of monometallic non-magnetic derivatives,we first try non-magnetic bimetallic MOFs derivatives to achieve efficient EMW absorption.The porous carbon-wrapped TiO2/ZrTiO4 composites derived from PCN-415(TiZr-MOFs)are qualified with a minimum reflection loss of−67.8 dB(2.16 mm,13.0 GHz),and a maximum effective absorption bandwidth of 5.9 GHz(2.70 mm).Through in-depth discussions,the synergy of enhanced interfacial polarization and other attenuation mechanisms in the composites is revealed.Therefore,this work confirms the huge potentials of nonmagnetic bimetallic MOFs derivatives in EMW absorption applications. 展开更多
关键词 Bimetallic metal-organic framework PcN-415 MOF derivatives TiO2/ZrTiO4/c composites Electromagnetic wave absorption
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Experimental Investigation of the Anisotropic Thermal Conductivity of C/SiC Composite Thin Slab
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作者 毋克凡 张虎 唐桂华 《Chinese Physics Letters》 SCIE EI CAS CSCD 2024年第3期48-60,共13页
Fiber-reinforced composites possess anisotropic mechanical and heat transfer properties due to their anisotropic fibers and structure distribution.In C/Si C composites,the out-of-plane thermal conductivity has mainly ... Fiber-reinforced composites possess anisotropic mechanical and heat transfer properties due to their anisotropic fibers and structure distribution.In C/Si C composites,the out-of-plane thermal conductivity has mainly been studied,whereas the in-plane thermal conductivity has received less attention due to their limited thickness. 展开更多
关键词 composites c/Si ANISOTROPIc
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原位生长SiC晶须对C/C-SiC复合材料摩擦磨损性能影响
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作者 齐冀 《铁道机车车辆》 北大核心 2024年第2期61-66,共6页
采用聚合物浸渍热解(PIP)技术向C/C-SiC复合材料纤维束内引入了SiC晶须(SiC_(W)),然后结合化学气相渗透(CVI)和液硅渗透(LSI)法制备了C/SiCW-C-SiC复合材料,系统研究了原位生长SiCW的物相组成及典型微结构特征,在不同制动初速度下测试了... 采用聚合物浸渍热解(PIP)技术向C/C-SiC复合材料纤维束内引入了SiC晶须(SiC_(W)),然后结合化学气相渗透(CVI)和液硅渗透(LSI)法制备了C/SiCW-C-SiC复合材料,系统研究了原位生长SiCW的物相组成及典型微结构特征,在不同制动初速度下测试了C/SiC_(W)-C-SiC复合材料的摩擦磨损性能,结果表明:引入SiC_(W)后,对平均摩擦系数和瞬时摩擦系数影响较小,摩擦性能未发生明显变化,中高速制动时,C/SiC_(W)-C-SiC的磨损率相比于C/C-SiC可降低20%~60%。 展开更多
关键词 SIc晶须 c/c-sic 微结构 摩擦磨损性能
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Microwave absorption properties of Ni/C@SiC composites prepared by precursor impregnation and pyrolysis processes 被引量:1
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作者 Xinli Ye Junxiong Zhang +4 位作者 Zhaofeng Chen Junfeng Xiang Yun Jiang Faqin Xie Xiaomin Ma 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2023年第3期94-102,共9页
In the present study,the unique three-dimensional graphene coated nickel(Ni/C)foam reinforced silicon carbide(Ni/C@SiC)composites were first obtained via the precursor impregnation and pyrolysis(PIP)processes.The micr... In the present study,the unique three-dimensional graphene coated nickel(Ni/C)foam reinforced silicon carbide(Ni/C@SiC)composites were first obtained via the precursor impregnation and pyrolysis(PIP)processes.The microstructure images indicated that the SiC fillers were successfully prepared in the skeleton pores of the Ni/C foam.The influence of the PIP cycles on the microwave absorption performances was researched,and the results indicated that after the primary PIP process,Ni/C@SiC-I possessed the optimal microwave absorbing performance with a minimum reflection loss(RL)of-25.87 d B at 5.28 GHz and 5.00 mm.Besides,the RL values could be below-10.00 dB from 5.88 GHz to 7.74 GHz when the corresponding matching thickness was 3.85 mm.However,the microwave absorption properties of Ni/C@SiC-II and Ni/C@SiC-Ⅲwere tremendously degraded as the PIP times increased.At last,the electromagnetic parameter,dielectric loss,attenuation constant as well as impedance matching coefficient were further investigated to analyze the absorbing mechanism,which opened a new path for the certain scientific evaluation of the absorbing materials and had extremely important to the defence technology. 展开更多
关键词 composites Ni/c ABSORPTION
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Thermodynamic and structural properties of polystyrene/C60 composites: A molecular dynamics study
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作者 Junsheng Yang Ziliang Zhu +1 位作者 Duohui Huang Qilong Cao 《Chinese Physics B》 SCIE EI CAS CSCD 2020年第2期224-230,共7页
To tailor properties of polymer composites are very important for their applications.Very small concentrations of nanoparticles can significantly alter their physical characteristics.In this work,molecular dynamics si... To tailor properties of polymer composites are very important for their applications.Very small concentrations of nanoparticles can significantly alter their physical characteristics.In this work,molecular dynamics simulations are performed to study the thermodynamic and structural properties of polystyrene/C60(PS/C60)composites.The calculated densities,glass transition temperatures,and coefficient of thermal expansion of the bulk PS are in agreement with the experimental data available,implying that our calculations are reasonable.We find that the glass transition temperature Tg increases accordingly with an added concentration of C60 for PS/C60 composites.However,the self-diffusion coefficient D decreases with increase of addition of C60.For the volumetric coefficients of thermal expansion(CTE)of bulk PS and PS/C60 composites,it can be seen that the CTE increases with increasing content of C60 above Tg(rubbery region).However,the CTE decreases with increasing content of C60 below Tg(glassy region). 展开更多
关键词 polystyrene/c60 composites molecular dynamics glass transition DIFFUSION
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High thermal stability of diamond-cBN-B_4C-Si composites
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作者 Hong-Sheng Jia Pin-Wen Zhu +7 位作者 Hao Ye Bin Zuo Yuan-Long E Shi-Chong Xu Ji Li Hai-Bo Li Xiao-Peng Jia Hong-An Ma 《Chinese Physics B》 SCIE EI CAS CSCD 2017年第1期521-525,共5页
Improving the thermal stability of diamond and other superhard materials has great significance in various applications. Here, we report the synthesis and characterization of bulk diamond–cBN–B4C–Si composites sint... Improving the thermal stability of diamond and other superhard materials has great significance in various applications. Here, we report the synthesis and characterization of bulk diamond–cBN–B4C–Si composites sintered at high pressure and high temperature(HPHT, 5.2 GPa, 1620–1680 K for 3–5 min). The results show that the diamond, cBN, B4C,BxSiC, SiO2 and amorphous carbon or a little surplus Si are present in the sintered samples. The onset oxidation temperature of 1673 K in the as-synthesized sample is much higher than that of diamond, cBN, and B4C. The high thermal stability is ascribed to the covalent bonds of B–C, C–N, and the solid-solution of BxSiC formed during the sintering process. The results obtained in this work may be useful in preparing superhard materials with high thermal stability. 展开更多
关键词 high pressure and high temperature diamond–cBN–B4c–Si composites high thermal stability
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复合材料C型梁R角褶皱缺陷的形成机理及评价方法研究
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作者 李紫璇 孙金贵 +4 位作者 岳广全 满珈诚 申文轲 林德志 刘卫平 《航空制造技术》 北大核心 2025年第1期110-116,共7页
C型梁R角区域在热压罐成型过程中易产生褶皱缺陷,严重影响构件成型质量和使用性能。为了准确评价褶的皱缺陷程度,提供减少褶皱产生的思路,利用热压罐成型工艺开展了国内外两种不同牌号预浸料在不同铺层数下的C型梁样件制造,对成型过程中... C型梁R角区域在热压罐成型过程中易产生褶皱缺陷,严重影响构件成型质量和使用性能。为了准确评价褶的皱缺陷程度,提供减少褶皱产生的思路,利用热压罐成型工艺开展了国内外两种不同牌号预浸料在不同铺层数下的C型梁样件制造,对成型过程中R角预浸料的变形行为进行了分析,探究了褶皱缺陷形成的机理。提出了包含厚度分布、边缘滑移角和R角部分褶皱量化分析3个方面的评价方法,并利用该方法对样件进行了评价和对比。结果表明,预浸料的层间滑移行为是褶皱形成机理的关键,滑移阻力过大导致褶皱缺陷的产生;所测试的国产预浸料与国外预浸料相比,其整体黏度更大,所制造的C型梁更易产生褶皱缺陷;3个方面的评价指标具有一致性,可以从多个角度综合衡量C型梁R角的褶皱缺陷程度。 展开更多
关键词 热固性复合材料 热压罐成型工艺 c型梁 R角区域 褶皱缺陷
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T-C复合吸附管应用于室内空气中低沸点挥发性有机物测定
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作者 梁缉攀 余塘 +1 位作者 江伟武 戴静 《分析测试学报》 北大核心 2025年第3期527-533,共7页
室内空气挥发性有机物检测中常用的Tenax TA吸附管在采集低沸点挥发性有机物时易出现样品穿透的问题,显著影响检测结果的准确性。该研究利用吸附-热解吸/气相色谱法对比分析了Tenax TA吸附管和TC复合吸附管采集常见的低沸点挥发性有机... 室内空气挥发性有机物检测中常用的Tenax TA吸附管在采集低沸点挥发性有机物时易出现样品穿透的问题,显著影响检测结果的准确性。该研究利用吸附-热解吸/气相色谱法对比分析了Tenax TA吸附管和TC复合吸附管采集常见的低沸点挥发性有机物时的穿透曲线及采样吸附率,并进一步考察了T-C复合吸附管的样品解吸率、方法准确度及精密度。结果表明,相比于Tenax TA管,T-C复合吸附管采集低沸点挥发性有机化合物时的性能更优,可有效避免样品穿透的发生,采样吸附率不小于98.4%,样品解吸率大于99.7%,目标物质量在0~2.00μg范围的标准曲线相关系数不小于0.997 4,方法回收率为95.7%~112%,相对标准偏差为1.5%~6.3%,说明T-C复合吸附管可应用于装饰装修材料及室内空气中低沸点挥发性有机物的检测。 展开更多
关键词 低沸点 挥发性有机物 穿透 T-c复合吸附管 室内空气 气相色谱
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C/C-SiC复合材料熔融渗硅制备工艺 被引量:10
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作者 王其坤 胡海峰 +3 位作者 郑文伟 马青松 简科 陈朝辉 《材料导报》 EI CAS CSCD 北大核心 2005年第7期93-96,共4页
C/C-SiC 复合材料具有许多优异的性能,如高比强度、高比模量、优良的高温性能、高热导率以及低热膨胀系数等。与其它制备工艺相比,采用熔融渗硅法制备 C/C-SiC 复合材料的工艺具有操作简单、周期短、成本低等优点。综述了目前熔融渗硅... C/C-SiC 复合材料具有许多优异的性能,如高比强度、高比模量、优良的高温性能、高热导率以及低热膨胀系数等。与其它制备工艺相比,采用熔融渗硅法制备 C/C-SiC 复合材料的工艺具有操作简单、周期短、成本低等优点。综述了目前熔融渗硅法制备 C/C-SiC 复合材料的研究状况。 展开更多
关键词 c/c-sic复合材料 熔融渗硅 制备工艺 c/c-sic复合材料 低热膨胀系数 高比强度 高温性能 高热导率 研究状况 比模量 成本低
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C/C-SiC复合材料的导热性能及其影响因素 被引量:14
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作者 李专 肖鹏 +1 位作者 熊翔 黄伯云 《中南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2013年第1期40-45,共6页
以炭纤维针刺毡为预制体,采用化学气相渗透法和熔融渗硅法相结合制得C/C-SiC复合材料;研究C/C-SiC材料在室温至1 300℃之间的导热性能以及预制体结构、基体炭结构和石墨化处理对其热扩散率的影响。研究结果表明:C/C-SiC材料的比热容随... 以炭纤维针刺毡为预制体,采用化学气相渗透法和熔融渗硅法相结合制得C/C-SiC复合材料;研究C/C-SiC材料在室温至1 300℃之间的导热性能以及预制体结构、基体炭结构和石墨化处理对其热扩散率的影响。研究结果表明:C/C-SiC材料的比热容随着温度的升高不断增大,在700℃时达到最大值2.18 J/(g·K),随后降至1 300℃时的0.57 J/(g·K),其导热系数在1 300℃时为3.95 W/(m.K);C/C-SiC材料的热扩散率在室温时为0.12 cm2/s,随着温度的升高不断降低并趋于常量,平行摩擦面方向的热扩散率明显比垂直于摩擦面方向的大;以全网胎为预制体的C/C-SiC材料其垂直和平行摩擦面的热扩散率相当,树脂炭质量分数增大及石墨化处理均可显著提高C/C-SiC材料的热扩散率。 展开更多
关键词 c c-sic复合材料 导热系数 熔融渗硅 炭纤维
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三维针刺C/C-SiC复合材料的烧蚀性能 被引量:13
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作者 王玲玲 嵇阿琳 +3 位作者 黄寒星 王航 崔红 闫联生 《固体火箭技术》 EI CAS CSCD 北大核心 2012年第4期532-535,540,共5页
采用"化学气相渗透+先驱体浸渍裂解"(CVI+PIP)混合工艺,制备了三维针刺C/C-SiC复合材料,使用氧气流量和乙炔流量之比为2∶1的氧乙炔焰,研究了复合材料的烧蚀性能,烧蚀时间长达600 s;分别用扫描电镜和表面能谱,分析了烧蚀表面... 采用"化学气相渗透+先驱体浸渍裂解"(CVI+PIP)混合工艺,制备了三维针刺C/C-SiC复合材料,使用氧气流量和乙炔流量之比为2∶1的氧乙炔焰,研究了复合材料的烧蚀性能,烧蚀时间长达600 s;分别用扫描电镜和表面能谱,分析了烧蚀表面的形貌和成分。结果表明,复合材料的线烧蚀率和质量烧蚀率的平均值分别是0.004 3 mm/s和0.001 4 g/s。烧蚀表面不同区域微观形貌和烧蚀机理不同,烧蚀中心以基体氧化流失、C纤维的氧化以及气流冲刷为主;在过渡区域,烧蚀是以SiC基体的氧化和气流冲刷为主;烧蚀边缘则以SiC基体的热氧化为主。C/C-SiC复合材料在氧-乙炔条件下的烧蚀机制是热化学烧蚀、热物理烧蚀和机械冲刷的综合作用。 展开更多
关键词 三维针刺 cVI+PIP” c/c-sic复合材料 烧蚀性能
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