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Effects of air plasma flame on the ZrB_(2)-based UHTC coatings:Microstructure,phase evolution and ablation resistance 被引量:3
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作者 Dou Hu Qiangang Fu +2 位作者 Lei Zhou Xiaoxuan Li Bing Liu 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2023年第27期194-206,共13页
As for the air plasma sprayed ZrB_(2)-based coatings,B content change caused by inevitable oxidation is predictable but commonly ignored.Affected by air plasma flame,the B element loss and residual B_(2) O_(3) in the ... As for the air plasma sprayed ZrB_(2)-based coatings,B content change caused by inevitable oxidation is predictable but commonly ignored.Affected by air plasma flame,the B element loss and residual B_(2) O_(3) in the sprayed ZrB_(2) coating were observed.Moreover,how the B content change affects the microstructure,phase evolution,and ablation resistance(2.4 MW/m^(2),60 s)of ZrB_(2)-based coatings with different sec-ondary phases(SiC,MoSi_(2),and TaC)was investigated.The B element loss contributed to the increase in surface temperature and the decline in the sintering degree of the ZrO_(2) layer.The evaporation of residual B_(2)O_(3) caused damage to the coating structure in the form of pores,whose negative effect was enhanced and reduced by MoSi_(2) and TaC secondary phases,respectively.This work will provide some insight into thermally sprayed non-oxide ceramic coatings in the atmosphere. 展开更多
关键词 Plasma spraying uhtcs Ablation behavior MICROSTRUCTURE ZrB_(2)
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Grain boundary segregation induced strong UHTCs at elevated temperatures:A universal mechanism from conventional UHTCs to high entropy UHTCs 被引量:2
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作者 Fu-Zhi Dai Bo Wen +3 位作者 Yinjie Sun Yixiao Ren Huimin Xiang Yanchun Zhou 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2022年第28期26-33,共8页
Ultra-high temperature ceramics(UHTCs)exhibit a unique combination of excellent properties,including ultra-high melting point,excellent chemical stability,and good oxidation resistance,which make them promising candid... Ultra-high temperature ceramics(UHTCs)exhibit a unique combination of excellent properties,including ultra-high melting point,excellent chemical stability,and good oxidation resistance,which make them promising candidates for aerospace and nuclear applications.However,the degradation of hightemperature strength is one of the main limitations for their ultra-high temperature applications.Thus,searching for mechanisms that can help to develop high-performance UHTCs with good high-temperature mechanical properties is urgently needed.To achieve this goal,grain boundary segregation of a series of carbides,including conventional,medium entropy,and high entropy transition metal carbides,i.e.,Zr_(0.95)W_(0.05)C,TiZrHfC_(3),ZrHfNbTaC_(4),TiZrHfNbTaC_(5),were studied by atomistic simulations with a fitted Deep Potential(DP),and the effects of segregation on grain boundary strength were emphasized.For all the studied carbides,grain boundary segregations are realized,which are dominated by the atomic size effect.In addition,tensile simulations indicate that grain boundaries(GBs)will usually be strengthened due to segregation.Our simulation results reveal that grain boundary segregation may be a universal mechanism in enhancing the high-temperature strength of both conventional UHTCs and medium/high entropy UHTCs,since GBs play a key role in controlling the fracture of UHTCs at elevated temperatures. 展开更多
关键词 uhtcs High entropy ceramics Grain boundary segregation High-temperature strength Machine learning potential
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Using PyC modified 3D carbon fiber to reinforce UHTC under low temperature sintering without pressure 被引量:7
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作者 Baihe DU Yuan CHENG +6 位作者 Liancai XUN Shuchang ZHANG Jing TONG Qingrong LV Shanbao ZHOU Ping HU Xinghong ZHANG 《Journal of Advanced Ceramics》 SCIE CAS CSCD 2021年第4期871-884,共14页
Finding the optimum balance between strength and toughness,as well as acquiring reliable thermal shock resistance and oxidation resistance,has always been the most concerned topic in the discussion of ultra-high tempe... Finding the optimum balance between strength and toughness,as well as acquiring reliable thermal shock resistance and oxidation resistance,has always been the most concerned topic in the discussion of ultra-high temperature ceramic composites.Herein,PyC modified 3D carbon fiber is used to reinforce ultra-high temperature ceramic(UHTC).The macroscopic block composite with large size is successfully fabricated through low temperature sintering at 1300℃without pressure.The prepared PyC modified 3D C_(f)/ZrC-SiC composites simultaneously possess excellent physical and chemical stability under the synergistic effect of PyC interface layer and low temperature 1/2 sintering without pressure.The fracture toughness is increased in magnitude to 13.05±1.72 MPa·m^(1/2)accompanied by reliable flexural strength of 251±27 MPa.After rapid thermal shock spanning from room temperature(RT)to 1200℃,there are no visible surface penetrating cracks,spalling,or structural fragmentation.The maximum critical temperature difference reaches 875℃,which is nearly three times higher than that of traditional monolithic ceramics.The haunting puzzle of intrinsic brittleness and low damage tolerance are resolved fundamentally.Under the protection of PyC interface layer,the carbon fibers around oxide layer and matrix remain structure intact after static oxidation at 1500℃for 30 min.The oxide layer has reliable physical and chemical stability and resists the erosion from fierce oxidizing atmosphere,ensuring the excellent oxidation resistance of the composites.In a sense,the present work provides promising universality in designability and achievement of 3D carbon fiber reinforced ceramic composites. 展开更多
关键词 ultra-high temperature ceramic(uhtc) pyrolytic carbon interface layer carbon fiber
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Accelerated discovery of near-zero ablation ultra-high temperature ceramics via GAN-enhanced directionally constrained active learning
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作者 Wenjian Guo Fayuan Li +6 位作者 Lingyu Wang Li'an Zhu Yicong Ye Zhen Wang Bin Yang Shifeng Zhang Shuxin Bai 《Advanced Powder Materials》 2025年第3期55-66,共12页
In materials science,a significant correlation often exists between material input parameters and their corresponding performance attributes.Nevertheless,the inherent challenges associated with small data obscure thes... In materials science,a significant correlation often exists between material input parameters and their corresponding performance attributes.Nevertheless,the inherent challenges associated with small data obscure these statistical correlations,impeding machine learning models from effectively capturing the underlying patterns,thereby hampering efficient optimization of material properties.This work presents a novel active learning framework that integrates generative adversarial networks(GAN)with a directionally constrained expected absolute improvement(EAI)acquisition function to accelerate the discovery of ultra-high temperature ceramics(UHTCs)using small data.The framework employs GAN for data augmentation,symbolic regression for feature weight derivation,and a self-developed EAI function that incorporates input feature importance weighting to quantify bidirectional deviations from zero ablation rate.Through only two iterations,this framework successfully identified the optimal composition of HfB_(2)-3.52SiC-5.23TaSi_(2),which exhibits robust near-zero ablation rates under plasma ablation at 2500℃ for 200 s,demonstrating superior sampling efficiency compared to conventional active learning approaches.Microstructural analysis reveals that the exceptional performance stems from the formation of a highly viscous HfO_(2)-SiO_(2)-Ta_(2)O_(5)-HfSiO_(4)-Hf_(3)(BO_(3))_(4) oxide layer,which provides effective oxygen barrier protection.This work demonstrates an efficient and universal approach for rapid materials discovery using small data. 展开更多
关键词 uhtcs Ablation resistant GAN Active learning Microstructure
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Multifunctional and anisotropic Cf/ZrB2 based composites prepared via a combined injection and vacuum impregnation approach
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作者 Jun Liu Ji Zou +3 位作者 Shuaihang Qiu Jingjing Liu Weimin Wang Zhengyi Fu 《Journal of Materials Science & Technology》 2025年第33期176-184,共9页
Multifunctional carbon fibers(C_(f))/ZrB_(2) based composites were synthesized through a series of processes termed as IVI including sequential slurry injection,vacuum impregnation,pyrolysis and reimpregnation cycles,... Multifunctional carbon fibers(C_(f))/ZrB_(2) based composites were synthesized through a series of processes termed as IVI including sequential slurry injection,vacuum impregnation,pyrolysis and reimpregnation cycles,which facilitated the effective incorporation of ZrB_(2) powder into the carbon fiber preform.A single IVI cycle reduced the porosity of the preform from∼77%to∼40%.Microstructural analysis revealed a preferential distribution of ZrB2 powders within random layers and pyrolytic carbon effectively bridging the ceramic particles and fibers.Due to the hierarchical 0°/90°carbon fiber architecture,as fabricated Cf/ZrB_(2) composites exhibited anisotropy in mechanical and physical properties.Vertically oriented com-posites demonstrated higher compressive strain and low thermal conductivity(1.00-2.59 W m^(−1) K^(−1) from 298 to 1173 K).In contrast,horizontally oriented specimens exhibited higher compressive strength(60.77±20.30 MPa)and thermal conductivity(1.6-4.5 W m^(−1) K^(−1) from 298 to 1173 K).Furthermore,the continuous Cf endowed the composites with a positive temperature-dependent electrical conductiv-ity characteristic,not only contributed to their higher electrical conductivity values,but also was helpful for maintaining the excellent EMI shielding effectiveness(19.80-22.51 dB)of Cf/ZrB_(2) up to 800℃without obvious degradation.Considering the low-density characteristics of as-prepared composites,their specific performance metrics demonstrate good competitiveness compared to those fabricated via alternative processes. 展开更多
关键词 uhtcs Boride Anisotropic thermal conductivity Electromagnetic shielding efficiency Extreme-environment materials
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碳表面激光熔覆制备HfB_(2)-TaB_(2)-ZrB_(2)-SiC-MoSi_(2)复合涂层及其高温抗氧化性能研究 被引量:1
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作者 吴震 陈维鑫 +4 位作者 陶雪钰 郑明 范贺良 刘章生 郭立童 《陶瓷学报》 北大核心 2025年第2期308-318,共11页
碳材料虽然具有熔点高、密度低、热膨胀系数低等高温结构材料的优良特性,但高温易氧化问题限制了其应用。通过激光熔覆法在碳材料表面制备HfB_(2)-TaB_(2)-ZrB_(2)-SiC-MoSi_(2)复合涂层,对碳材料基体进行宽温域防护。利用XRD、SEM及能... 碳材料虽然具有熔点高、密度低、热膨胀系数低等高温结构材料的优良特性,但高温易氧化问题限制了其应用。通过激光熔覆法在碳材料表面制备HfB_(2)-TaB_(2)-ZrB_(2)-SiC-MoSi_(2)复合涂层,对碳材料基体进行宽温域防护。利用XRD、SEM及能谱等对涂层的显微结构进行表征,利用划痕附着力测试仪、空气炉等温氧化测试对涂层与基体的结合强度及高温抗氧化性能进行表征。所制备的涂层与碳基体间结合良好,划痕附着力达到16.8 N,对应的划痕强度为134.06 MPa;涂层截面无明显的贯穿性裂纹和孔洞等缺陷。对涂层进行多次激光线烧蚀,激光线烧蚀后涂层表面无破坏性缺陷,涂层表面更加平整;五次激光线烧蚀后涂层划痕附着力仍保持14.2 N,对应的划痕强度为113.1 MPa。涂层试样在1500℃等温氧化中表面形成致密Hf-Zr-Ta-Si-O复合氧化物层,增强涂层高温稳定性,涂层表面氧化层致密、完整、无明显缺陷,整体表现出较好的抗氧化性能和抗激光烧蚀性能。使用MoSi_(2)取代部分Si,有助于进一步提升涂层的高温抗氧化性能和抗激光烧蚀性能。 展开更多
关键词 激光熔覆 超高温陶瓷 抗氧化涂层 激光烧蚀 碳材料
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碳纤维增强超高温陶瓷基复合材料研究进展 被引量:13
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作者 陈小武 董绍明 +5 位作者 倪德伟 阚艳梅 周海军 王震 张翔宇 丁玉生 《中国材料进展》 CAS CSCD 北大核心 2019年第9期843-854,共12页
超高温陶瓷(UHTCs)因在高超声速飞行器热防护领域的巨大应用前景而备受关注,而脆性大、烧结成型困难是制约UHTCs广泛应用的实质问题。将碳纤维与UHTCs复合获得碳纤维增强超高温陶瓷基复合材料(Cf/UHTCs)是克服这一问题的可靠方案。近10... 超高温陶瓷(UHTCs)因在高超声速飞行器热防护领域的巨大应用前景而备受关注,而脆性大、烧结成型困难是制约UHTCs广泛应用的实质问题。将碳纤维与UHTCs复合获得碳纤维增强超高温陶瓷基复合材料(Cf/UHTCs)是克服这一问题的可靠方案。近10年来,我国在Cf/UHTCs工程应用方面获得了重大突破,取得了一系列具有世界先进水平的应用成果。然而,由于Cf/UHTCs制备过程复杂,服役环境苛刻(> 2000℃,> 5 Ma气流冲刷),在结构演化、性能机理等方面仍存在一些关键科学问题亟需明确。综述了Cf/UHTCs在基体改性、氧化烧蚀机理、高温力学行为等方面的研究进展,并结合本团队的研究工作对Cf/UHTCs的研究趋势进行了总结和展望,旨在为进一步推动Cf/UHTCs的研究和发展提供参考。 展开更多
关键词 Cf/uhtcs复合材料 基体改性 氧化烧蚀 高温力学性能 结构调控
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高超声速飞行器热防护用超高温复合材料的研究进展 被引量:18
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作者 刘永胜 曹立阳 +3 位作者 张运海 曹晔洁 王晶 董宁 《复合材料科学与工程》 CAS 北大核心 2022年第10期107-118,共12页
热防护系统是高超声速飞行器的关键技术之一,决定了飞行器研制的成败,而高温热防护材料则直接决定了热防护系统的性能。本文综述了以C/C复合材料、C/SiC复合材料、C/UHTC复合材料等为代表的热防护用超高温复合材料的研究进展,并重点分... 热防护系统是高超声速飞行器的关键技术之一,决定了飞行器研制的成败,而高温热防护材料则直接决定了热防护系统的性能。本文综述了以C/C复合材料、C/SiC复合材料、C/UHTC复合材料等为代表的热防护用超高温复合材料的研究进展,并重点分析了近年来超高温复合材料导热和烧蚀性能相关的研究进展,进而提出了未来发展方向,为热防护用超高温复合材料的发展提供参考。 展开更多
关键词 高超声速飞行器 热防护材料 C/C C/SIC C/uhtc 超高温复合材料
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欧洲高速飞行轻质先进材料的气动与热载荷相互作用计划(ATLLAS)研究进展 被引量:3
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作者 郭朝邦 李文杰 +1 位作者 文苏丽 张冬青 《飞航导弹》 北大核心 2011年第1期18-22,35,共6页
简述了高速飞行轻质先进材料的气动与热载荷相互作用计划(ATLLAS)的概况和研究情况,详细介绍了ATLLAS分别在飞行器机身结构材料和发动机燃烧室冷却方案的研究进展,机身结构材料包括金属中空球状芯(HSP)夹层结构、超高温陶瓷(UHTC)材料... 简述了高速飞行轻质先进材料的气动与热载荷相互作用计划(ATLLAS)的概况和研究情况,详细介绍了ATLLAS分别在飞行器机身结构材料和发动机燃烧室冷却方案的研究进展,机身结构材料包括金属中空球状芯(HSP)夹层结构、超高温陶瓷(UHTC)材料和陶瓷基复合材料(CMC),燃烧室冷却方案包括薄膜、渗透、蒸发、再生冷却技术,最后对ATLLAS的研究成果进行了总结。 展开更多
关键词 飞行器 高超声速 燃烧室 机身结构 uhtc CMC HSP
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HfB_2材料研究进展 被引量:6
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作者 郭朝邦 《战术导弹技术》 2010年第4期32-35,47,共5页
说明了HfB2具有高熔点、高硬度和优秀的热导率(相对于其它陶瓷)等特性,是一种理想的高超声速飞行器热防护系统用材料.介绍了HfB2的基本性质,从HfB2的抗氧化性、烧结助剂、烧结工艺等三方面综述了HfB2的研究进展.
关键词 HfB2 uhtc 进展
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纳米SiC晶须和SiC颗粒混合增韧ZrB_2陶瓷性能 被引量:9
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作者 王海龙 汪长安 +3 位作者 张锐 黄勇 许红亮 卢红霞 《复合材料学报》 EI CAS CSCD 北大核心 2009年第4期95-101,共7页
分别采用纳米SiC晶须(SiCW)、SiC颗粒(SiCP)及SiCW与SiCP共同增韧ZrB2陶瓷,在1950℃、20 MPa压力、氩气气氛下热压烧结制备了致密的SiC/ZrB2陶瓷材料。研究了SiCW和SiCP的添加量对于SiC/ZrB2陶瓷材料的显微结构、力学性能的影响,并分析... 分别采用纳米SiC晶须(SiCW)、SiC颗粒(SiCP)及SiCW与SiCP共同增韧ZrB2陶瓷,在1950℃、20 MPa压力、氩气气氛下热压烧结制备了致密的SiC/ZrB2陶瓷材料。研究了SiCW和SiCP的添加量对于SiC/ZrB2陶瓷材料的显微结构、力学性能的影响,并分析了SiCW和SiCP对ZrB2陶瓷力学性能影响的协同作用和增韧机制。结果表明:含15 vol%SiCW的复合材料的韧性达到8.08 MPa.m1/2,含15 vol%SiCP的复合材料的韧性达到8.515MPa.m1/2,共同添加15 vol%SiCW和15 vol%SiCP的复合材料的韧性最高达到9.03 MPa.m1/2。SiC/ZrB2复合材料强度和韧性提高的原因在于SiCW和SiCP抑制ZrB2晶粒长大,促进ZrB2的致密化,此外,SiCW和SiCP的协同作用也有助于材料韧性的提高。 展开更多
关键词 SiC/ZrB2 超高温陶瓷 强韧化 晶须增韧
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超高温陶瓷材料抗热冲击性能及抗氧化性能研究 被引量:17
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作者 张幸红 胡平 +1 位作者 韩杰才 杜善义 《中国材料进展》 CAS CSCD 2011年第1期27-31,25,26,共7页
研究了多种强韧化方法以提高超高温陶瓷材料抗热冲击性能,包括碳化硅晶须增强增韧、石墨软相增韧和氧化锆相变增韧。同时,还研究了碳化硅含量对超高温陶瓷材料的抗氧化性能影响。研究结果表明:碳化硅晶须和氧化锆的添加显著提高了材料... 研究了多种强韧化方法以提高超高温陶瓷材料抗热冲击性能,包括碳化硅晶须增强增韧、石墨软相增韧和氧化锆相变增韧。同时,还研究了碳化硅含量对超高温陶瓷材料的抗氧化性能影响。研究结果表明:碳化硅晶须和氧化锆的添加显著提高了材料的抗热冲击临界温差,而石墨软相的引入对抗冲击临界温差的影响不大,但显著提高了裂纹扩展阻力和强度保持率。高SiC含量超高温陶瓷材料在1 800℃以下具有的优异的抗氧化性能,在更高的温度下,高与低的SiC含量对超高温陶瓷材料的抗氧化性能均不利,通过优化材料的组分以降低材料表面温度是提高超高温陶瓷材料的抗氧化性能的一个非常有效的途径。 展开更多
关键词 超高温陶瓷材料 强韧化 抗热冲击 抗氧化
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超高温陶瓷复合材料抗热冲击性能影响因素的实验研究 被引量:5
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作者 金华 孟松鹤 +2 位作者 解维华 朱燕伟 杨强 《固体火箭技术》 EI CAS CSCD 北大核心 2013年第2期255-260,共6页
为研究超高温陶瓷复合材料抗热冲击性能的影响因素,自行搭建多参数导电类热防护材料热冲击测试装置,测试导电类材料表面温度响应、升温速率、尺寸效应、压力及气体组分对其抗热冲击性能的影响。针对ZrB2-SiC-石墨(ZSG)典型超高温陶瓷复... 为研究超高温陶瓷复合材料抗热冲击性能的影响因素,自行搭建多参数导电类热防护材料热冲击测试装置,测试导电类材料表面温度响应、升温速率、尺寸效应、压力及气体组分对其抗热冲击性能的影响。针对ZrB2-SiC-石墨(ZSG)典型超高温陶瓷复合材料,通过正交实验获得不同参数下热冲击实验后材料的剩余弯曲强度,并利用极差、方差分析各参数对抗热冲击性能的影响权重及显著性,结果表明表面温度响应,升温速率和尺寸效应具有显著影响,压力和气体组分影响甚微。 展开更多
关键词 超高温陶瓷 抗热冲击 正交实验 影响因素
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Design, Preparation and Properties of Carbon Fiber Reinforced Ultra-High Temperature Ceramic Composites for Aerospace Applications: A Review 被引量:75
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作者 Sufang Tang Chenglong Hu 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2017年第2期117-130,共14页
Carbon fiber reinforced ultra-high temperature ceramic (UHTC) composites, consisting of carbon fibers embedded in a UHTC-matrix or a C-SiC-UHTC-matrix, are deemed as the most viable class of materials that can overc... Carbon fiber reinforced ultra-high temperature ceramic (UHTC) composites, consisting of carbon fibers embedded in a UHTC-matrix or a C-SiC-UHTC-matrix, are deemed as the most viable class of materials that can overcome the poor fracture toughness and thermal shock resistance of monolithic UHTC ma- terials, and also improve the oxidation resistance and ablation resistance of C/C and C/SiC composites at ultra-high temperatures. In this review, we summarize the different processing routes of the compos- ites based on the UHTC introducing methods, including chemical vapor infiltration/deposition (CVI/D), precursor infiltration and pyrolysis (PIP), reactive melt infiltration (RMI), slurry infiltration (SI). in-sito reaction, hot pressing (HP), etc; and the advantages and drawbacks of each method are briefly dis- cussed. The carbon fiber reinforced UHTC composites can be highly tailorable materials in terms of fiber. interface, and matrix. From the perspective of service environmental applications for engine propul- sions anti hypersonic vehicles, the material designs (mainly focusing on the composition, quantity, structure of matrix, as well as the architecture of carbon fibers, UHTCs and pores), their relevant processing routes and properties (emphasizing on the mechanical and ablation properties) are discussed in this paper. In addition, we propose a material architecture to realize the multi-function through changing the distri- bution of carbon fibers, UHTCs and pores, which will be an important issue for future development of carbon fiber reinforced UHTC composites. 展开更多
关键词 Carbon fiber composites Ceramic matrix composites (CMC) Ultra-high temperature ceramic uhtc Ablation
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High porosity and low thermal conductivity high entropy(Zr0.2Hf0.2Ti0.2Nb0.2Ta0.2C 被引量:29
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作者 Heng Chen Huimin Xiang +4 位作者 Fu-Zhi Dai Jiachen Liu Yiming Lei Jie Zhang Yanchun Zhou 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2019年第8期1700-1705,共6页
Porous ultra-high temperature ceramics(UHTCs)are promising for ultrahigh-temperature thermal insulation applications.However,the main limitations for their applications are the high thermal conductivity and densificat... Porous ultra-high temperature ceramics(UHTCs)are promising for ultrahigh-temperature thermal insulation applications.However,the main limitations for their applications are the high thermal conductivity and densification of porous structure at high temperatures.In order to overcome these obstacles,herein,porous high entropy(Zr(0.2)Hf(0.2)Ti(0.2)Nb(0.2)Ta(0.2))C was prepared by a simple method combing in-situ reaction and partial sintering.Porous high entropy(Zr(0.2)Hf(0.2)Ti(0.2)Nb(0.2)Ta(0.2))C possesses homogeneous microstructure with grain size in the range of 100–500 nm and pore size in the range of 0.2–1μm,which exhibits high porosity of 80.99%,high compressive strength of 3.45 MPa,low room temperature thermal conductivity of 0.39 W·m^-1K^-1,low thermal diffusivity of 0.74 mm^2·s^-1and good high temperature stability.The combination of these properties renders porous high entropy(Zr(0.2)Hf(0.2)Ti(0.2)Nb(0.2)Ta(0.2))Cpromising as light-weight ultrahigh temperature thermal insulation materials. 展开更多
关键词 Ultrahigh temperature CERAMICS (uhtcs) HIGH ENTROPY CERAMICS (Zr(0.2)Hf(0.2)Ti(0.2)Nb(0.2)Ta(0.2))C Thermal CONDUCTIVITY POROSITY
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混合炸药爆炸压实制备ZrB_2-SiC_w超高温陶瓷 被引量:2
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作者 李金平 孟松鹤 +2 位作者 韩杰才 张幸红 梁军 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2007年第A02期8-11,共4页
为了改善ZrB_2-SiC超高温陶瓷材料的韧性,采用黑索今与硝酸铵混合炸药爆炸压实制备了SiC晶须增韧ZrB_2基超高温陶瓷,并研究爆炸压实过程中的能量与变形,爆炸压实坯密度与显微组织。结果表明,采用爆炸压实工艺制备了相对密度约95.25%的Zr... 为了改善ZrB_2-SiC超高温陶瓷材料的韧性,采用黑索今与硝酸铵混合炸药爆炸压实制备了SiC晶须增韧ZrB_2基超高温陶瓷,并研究爆炸压实过程中的能量与变形,爆炸压实坯密度与显微组织。结果表明,采用爆炸压实工艺制备了相对密度约95.25%的ZrB2-SiC_w陶瓷复合材料。随着混合炸药中黑索今质量的增加,爆轰压力单调增加,爆炸坯密度先增加,后减小,有一个最大值;钢管的外径收缩率、等效应变与爆炸坯密度变化一致;钢管变形能几乎不变,爆炸冲击能与粉末压实能同步增加。由于爆炸冲击波的作用,SiC晶须被折断成碎片;其组织为均匀、碎小的SiC晶须镶嵌于较大的ZrB_2颗粒中。 展开更多
关键词 超高温陶瓷 ZRB2-SIC 爆炸压实 密度 组织
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MoSi_2对注凝成型HfB_2超高温陶瓷材料性能的影响 被引量:4
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作者 唐竹兴 杨晴晴 杨赞中 《硅酸盐通报》 CAS CSCD 北大核心 2009年第5期930-934,共5页
在pH为10.9,分散剂PMAA-NH4为8vol%,固体含量为40vol%的条件下采用注凝成型技术制备了HfB2-(5%~15wt%)MoSi2超高温陶瓷坯体,密度达到4.25g/cm3以上,在氩气气氛下1950℃保温30min烧成。采用X射线衍射仪、扫描电镜等分析方法研究了添加剂... 在pH为10.9,分散剂PMAA-NH4为8vol%,固体含量为40vol%的条件下采用注凝成型技术制备了HfB2-(5%~15wt%)MoSi2超高温陶瓷坯体,密度达到4.25g/cm3以上,在氩气气氛下1950℃保温30min烧成。采用X射线衍射仪、扫描电镜等分析方法研究了添加剂MoSi2对HfB2超高温陶瓷材料性能的影响、烧结体的物相组成和显微结构。结果表明:添加剂MoSi2可有效促进HfB2超高温陶瓷材料的致密化,随着MoSi2加入量的提高,HfB2超高温陶瓷材料的力学性能不断提高,当加入量为15%时,可得到显微硬度为9.8GPa,抗弯强度为389.7MPa,断裂韧性为3.7MPa.m1/2的HfB2超高温陶瓷材料。 展开更多
关键词 注凝成型 超高温陶瓷材料 显微结构 力学性能
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超高韧性水泥基材料桥面连续构造的疲劳试验 被引量:9
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作者 胡克旭 侯梦君 +1 位作者 余江滔 董思卫 《同济大学学报(自然科学版)》 EI CAS CSCD 北大核心 2018年第6期776-783,共8页
通过3个桥面连续构造节点的疲劳试验,分析不同材料(普通混凝土和超高韧性水泥基材料(UHTC))和配筋下桥面连续构造的疲劳性能.试验结果表明:在疲劳荷载作用下,UHTC材料表现出了明显的多缝开裂和延性破坏特征;在同等应力条件下,UHTC材料... 通过3个桥面连续构造节点的疲劳试验,分析不同材料(普通混凝土和超高韧性水泥基材料(UHTC))和配筋下桥面连续构造的疲劳性能.试验结果表明:在疲劳荷载作用下,UHTC材料表现出了明显的多缝开裂和延性破坏特征;在同等应力条件下,UHTC材料桥面连续构造节点的疲劳寿命是普通钢筋混凝土试件的3倍以上;相同荷载作用下,相比于普通混凝土,UHTC能有效减缓钢筋应变幅的增长,减缓桥面连续构造在疲劳荷载作用下的刚度退化,从而大大提高了桥面连续构造的疲劳寿命. 展开更多
关键词 高延性纤维增强水泥基复合材料 超高韧性水泥基材料 桥面连续构造 疲劳试验 疲劳寿命
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Effect of reaction routes on the porosity and permeability of porous high entropy(Y0.2Yb0.2Sm0.2Nd0.2Eu0.2)B6 for transpiration cooling 被引量:9
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作者 Heng Chen Zifan Zhao +5 位作者 Huimin Xiang Fu-Zhi Dai Jie Zhang Shaogang Wang Jiachen Liu Yanchun Zhou 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2020年第3期80-85,共6页
Transpiration cooling technique is a reusable and high-efficiency thermal protection system(TPS),which is potential to improve the reusability and security of re-entry space vehicle.Relatively low density,high permeab... Transpiration cooling technique is a reusable and high-efficiency thermal protection system(TPS),which is potential to improve the reusability and security of re-entry space vehicle.Relatively low density,high permeability and high porosity are general requirements for porous media of transpiration cooling systems.In this work,a new porous high entropy metal hexaboride(Y0.2Yb0.2Sm0.2Nd0.2Eu0.2)B6 is designed and prepared by the in-situ reaction/partial sintering method.Two reaction routes are designed to synthesize(Y0.2Yb0.2Sm0.2Nd0.2Eu0.2)B6,including boron thermal reduction and borocarbon thermal reduction.The as-prepared porous HE(Y0.2Yb0.2Sm0.2Nd0.2Eu0.2)B6 ceramics possess homogeneous microstructure and exhibit low density,high porosity,high compressive strength and high permeability.The combination of these properties makes porous HE(Y0.2Yb0.2Sm0.2Nd0.2Eu0.2)B6 promising as a candidate porous media for various transpiration cooling applications. 展开更多
关键词 HIGH ENTROPY ceramics (Y0.2Yb0.2Sm0.2Nd0.2Eu0.2)B6 TRANSPIRATION COOLING POROUS uhtcs IN-SITU reaction synthesis
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振荡热压烧结ZrB_(2)-SiC陶瓷的力学性能
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作者 李冰 赵科 +1 位作者 刘佃光 刘金铃 《航空制造技术》 CSCD 北大核心 2024年第13期100-105,112,共7页
采用振荡热压烧结(HOP)和热压烧结(HP)工艺制备了ZrB_(2)-SiC陶瓷,研究了振荡压力对ZrB_(2)-SiC陶瓷致密化及力学性能的影响。结果表明,与采用HP工艺制备ZrB_(2)-SiC陶瓷相比,HOP工艺的致密化速率有显著提升;ZrB_(2)与SiC两相界面结合良... 采用振荡热压烧结(HOP)和热压烧结(HP)工艺制备了ZrB_(2)-SiC陶瓷,研究了振荡压力对ZrB_(2)-SiC陶瓷致密化及力学性能的影响。结果表明,与采用HP工艺制备ZrB_(2)-SiC陶瓷相比,HOP工艺的致密化速率有显著提升;ZrB_(2)与SiC两相界面结合良好;HOP工艺制备的ZS30样品的硬度和断裂韧性分别达到了21.1 GPa和7.3 MPa·m^(1/2),较采用HP工艺在相同烧结参数下制备的试样有大幅提升。HOP在制备高性能ZrB_(2)-SiC陶瓷方面展现出良好发展前景。 展开更多
关键词 超高温陶瓷(uhtcs) ZrB_(2) 烧结 致密化 力学性能
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