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Kevlar fabric reinforced polybenzoxazine composites filled with silane treated microcrystalline cellulose in the interlayers:The next generation of multi-layered armor panels
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作者 Wissam Bessa Djalal Trache +1 位作者 Mehdi Derradji Ahmed Fouzi Tarchoun 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2022年第11期2000-2007,共8页
The design of astonishing combinations of benzoxazine resins with various fillers is nowadays of great interest for high quality products,especially in ballistic armors.The objective of this study is to investigate a ... The design of astonishing combinations of benzoxazine resins with various fillers is nowadays of great interest for high quality products,especially in ballistic armors.The objective of this study is to investigate a new hybrid material prepared as multi-layered composite plate by hand lay-up technique.Different composites were manufactured from Kevlar fabrics reinforced polybenzoxazine,which was filled with silane treated microcrystalline cellulose(MCC Si)at various amounts in the interlayers.The developed materials were tested for their flexural,dynamic mechanical and ballistic performance.The aim was to highlight the effect of adding different amounts of MCC Si on the behavior of the different plates.Compared to the baseline,the dynamic mechanical and bending tests revealed an obvious decrease of the glass transition of 21℃and a notable increase in storage modulus and flexural strength of about 180%and17%,respectively,upon adding 1%MMC Si as filler.Similarly,the ballistic test exhibited an enhancement in kinetic energy absorption for which the composite supplemented with 1%MCC Si had the maximal energy absorption of 166.60 J.These results indicated that the developed panels,with interesting mechanical and ballistic features,are suitable to be employed as raw materials to produce body armor. 展开更多
关键词 POLYBENZOXAZINE Microcrystalline cellulose kevlar fabric Mechanical properties Ballistic energy absorption
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Influence of Weave Structures on the Tribological Properties of Hybrid Kevlar/PTFE Fabric Composites 被引量:14
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作者 GU Dapeng YANG Yulin +2 位作者 QI Xiaowen DENG Wei SHI Lei 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2012年第5期1044-1051,共8页
The existing research of the woven fabric self-lubricating liner mainly focus on the tribological performance improvements and the service life raised by changing different fiber type combinations, adding additive mod... The existing research of the woven fabric self-lubricating liner mainly focus on the tribological performance improvements and the service life raised by changing different fiber type combinations, adding additive modification, and performing fiber surface modification. As fabric composites, the weave structures play an important role in the mechanical and tribological performances of the liners. However, hardly any literature is available on the friction and wear behavior of such composites with different weave structures. In this paper, three weave structures (plain, twill 1/3 and satin 8/5) of hybrid Kevlar/PTFE fabric composites are selected and pin-on-flat linear reciprocating wear studies are done on a CETR tester under different pressures and different frequencies. The relationship between the tensile strength and the wear performance are studied. The morphologies of the worn surfaces under the typical test conditions are analyzed by means of scanning electron microscopy (SEM). The analysis results show that at 10 MPa, satin 8/5 performs the best in friction-reduction and antiwear performance, and plain is the worst. At 30 MPa, however, the antiwear performance is reversed and satin 8/5 does not even complete the 2 h wear test at 16 Hz. There is no clear evidence proving that the tensile strength has an influence on the wear performance. So the different tribological performance of the three weave structures of fabric composites may be attributed to the different PTFE proportions in the fabric surface and the different wear mechanisms. The fabric composites are divided into three regions: the lubrication region, the reinforced region and the bonding region. The major mechanisms are fatigue wear and the shear effects of the friction force in the lubrication region. In the reinforced region fiber-matrix de-bonding and fiber breakage are involved. The proposed research proposes a regional wear model and further indicates the wear process and the wear mechanism of fabric composites. 展开更多
关键词 hybrid kevlar/PTFE fabric composite FRICTION WEAR weave structure scanning electron microscopy
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Containment of soft wall casing wrapped with Kevlar fabric 被引量:6
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作者 Zekan HE Haijun XUAN +2 位作者 Conger BAI Manli SONG Zhuoshen ZHU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第4期954-966,共13页
Aramid fabrics have been commonly used in the civil turbofan engine fan blade containment system for its excellent performance. To investigate the behavior and capability of soft wall containment casing, a series of f... Aramid fabrics have been commonly used in the civil turbofan engine fan blade containment system for its excellent performance. To investigate the behavior and capability of soft wall containment casing, a series of fan blade released tests were conducted on the high-speed spin tester.The soft wall casing was fabricated by wrapping multiple layers of Kevlar49 plain woven fabric around a thin steel ring. Casings with different inner metal ring and outer fabric layers number were compared. The method of using the explicit dynamic software LS-DYNA to establish the finite element analysis model for the quantitative analysis of the containment process was developed and conducted. The simulation results are in good agreement with the test results. It is shown that the containment process of the soft wall casing can be divided into three impact stages. The casing with low-stiffness inner metal ring will get severe overall deformation and lose the structural integrity when it suffers the blade impact. Kevlar fabric layers will appear large bulge on outside surface and absorb the most impact dynamic energy of the high speed released fan blade. By summing up the results of the test and simulation, an empirical critical equation was derived to describe the relationship between the released blade dynamic energy and the Kevlar fabric thickness. 展开更多
关键词 CONTAINMENT equation Fan blade Inner metal ring kevlar fabric SOFT WALL CASING
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Sliding Wear of the Hybrid Kevlar/PTFE Fabric Reinforced Phenolic Composite Filled with Nano-titania 被引量:4
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作者 YANG Yulin HUANG Shijun +2 位作者 ZU Dalei ZHANG Ruijun QI Xiaowen 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2011年第1期154-159,共6页
The Kevlar/polytetrafluroethylene(Kevlar/PTFE) fabric composite can be used as a self-lubricating liner of the self-lubricating bearing.Many types of nano-particles can improve the tribological performance of the po... The Kevlar/polytetrafluroethylene(Kevlar/PTFE) fabric composite can be used as a self-lubricating liner of the self-lubricating bearing.Many types of nano-particles can improve the tribological performance of the polymer-based composite.Unfortunately,up to now,published work on the effect of nano-particles on the tribological performance of the fabric composite which can be used as a self-lubricating liner is quite scarce.Therefore,for the purpose of exploring a way to significantly improve the tribological performance of the fabric composite,the tribological performance of the Kevlar/PTFE fabric composite filled with nano-titania is evaluated by using the block-on-ring wear tester.The scanning electron microscopy is utilized to observe the morphologies of worn surfaces of the fabric composites and the counterparts.The tensile properties of the composites are evaluated on the universal material testing machine.The test results show that the addition of nano-titania at a proper mass fraction of the matrix resin improves the wear resistance and the tensile strength,decreases the friction coefficient,and makes the wear volume of the composite reach a relative steady state more quickly;plastic deformation and microcutting are important for the wear of the fabric composite;a lubricating layer is formed on the worn surface of the composite during sliding,and the lubricating layer is critical for the tribological performance of the composite;the formation and properties of the lubricating layer are influenced by the nano-titania particles.The proposed study on the effect of nano-titania on the tribological performance of the Kevlar/PTFE fabric composite,especially on the evolution of the worn surface of the composite,provides the basis for further understanding of the influence mechanism of the nano-particles on the tribological performance of the composite and explores a method of improving the tribological performance of the composite. 展开更多
关键词 hybrid kevlar/PTFE fabric composite self-lubricating liner nano-titania friction and wear lubricating layer
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无钯化学镀制备导电Ni@Kevlar®复合织物及其电磁屏蔽性能 被引量:2
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作者 李敏娜 张蕾蕾 +4 位作者 李晓琳 王莎莎 盛明杰 白瑞成 邵勤思 《重庆大学学报》 CAS CSCD 北大核心 2023年第9期78-91,共14页
采用高性能Kevlar®织物作为基体,使用无刻蚀、无钯、无锡的“溶胀-银”方法进行活化,通过化学镀工艺制备Ni@Kevlar®织物。利用扫描电子显微镜(SEM)和高分辨率透射电子显微镜(HRTEM)观察织物表面及纤维截面的微观形貌,探究不... 采用高性能Kevlar®织物作为基体,使用无刻蚀、无钯、无锡的“溶胀-银”方法进行活化,通过化学镀工艺制备Ni@Kevlar®织物。利用扫描电子显微镜(SEM)和高分辨率透射电子显微镜(HRTEM)观察织物表面及纤维截面的微观形貌,探究不同时间下样品的质量增加率、增厚及面密度,并利用X射线光电子能谱仪(XPS)和广角X射线衍射仪(WXRD)测量表面成分及晶体结构,采用四探针测试仪和综合物理性能测量系统(PPMS)测量电、磁性能。结果表明,无刻蚀、无钯、无锡的“溶胀-银”活化处理能在织物表面产生大量的银催化靶点,经化学镀后可得到具有良好导电性和铁磁性的纯镍镀层。同轴法屏蔽效能测试结果表明,Ni@Kevlar®织物在低频波段(0.1 MHz~1.5 GHz)的屏蔽值最高达70 dB,能屏蔽99.99999%的电磁波,高频波段(2~18 GHz)达到25 dB,可满足生活生产的屏蔽需求。 展开更多
关键词 kevlar®织物 无钯 “溶胀-银”活化 化学镀镍 电磁屏蔽
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紫外辐照对自润滑关节轴承衬垫磨损性能的影响
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作者 叶强 谭德强 +4 位作者 宗法涛 胡月 贺强 杨文锋 周长春 《中国表面工程》 EI CAS CSCD 北大核心 2024年第3期134-144,共11页
PTFE/Kevlar织物材料具有优异自润滑性能,在航空关键部件中广泛应用,但紫外辐照对其影响规律尚不清晰。针对航空器飞行强紫外线暴露的特点,聚焦紫外辐照对航空常用PTFE/Kevlar编织关节轴承衬垫自润滑材料摩擦学性能的影响规律研究。对... PTFE/Kevlar织物材料具有优异自润滑性能,在航空关键部件中广泛应用,但紫外辐照对其影响规律尚不清晰。针对航空器飞行强紫外线暴露的特点,聚焦紫外辐照对航空常用PTFE/Kevlar编织关节轴承衬垫自润滑材料摩擦学性能的影响规律研究。对不同紫外辐照时长的PTFE/Kevlar织物衬垫材料进行往复摩擦试验,并采用多种表征手段对其宏观、微观损伤形貌以及化学状态进行分析。结果表明:PTFE/Kevlar织物衬垫材料的磨损程度随着紫外辐照时间的增加呈现出先降低后升高的趋势,短时辐照(T=100 h和200 h)的磨损最轻微,摩擦损失体积和磨痕最大深度仅为未辐照和长时辐照(T=300 h和500h)的2/3;紫外辐照后,衬垫材料与GCr15轴承钢球之间的磨损行为变化表现为PTFE纤维塑性变形和转移膜形成能力的下降,其主要原因是PTFE纤维结晶度的降低;衬垫材料的磨损机理随辐照时间的延长由疲劳磨损和粘着磨损向磨粒磨损为主转变。研究成果可为PTFE/Kevlar织物衬垫型自润滑材料在紫外辐照后的磨损性能跟踪和研制优化提供参考。 展开更多
关键词 PTFE/kevlar织物 紫外辐照 损伤形貌 转移膜 磨损机理
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Kevlar纤维叠层织物防弹机理和性能研究 被引量:21
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作者 顾冰芳 龚烈航 徐国跃 《南京理工大学学报》 EI CAS CSCD 北大核心 2007年第5期638-642,共5页
选取多种形状的冲击体对Kevlar纤维叠层织物进行了弹道冲击实验。研究了Kevlar纤维受冲击时的表观破坏形态和微观损伤机理。结果表明:纤维的变形破坏随冲击物的形状和速度变化呈现出多形态、多阶段模式;纤维的微观变形形态为:除拉伸破坏... 选取多种形状的冲击体对Kevlar纤维叠层织物进行了弹道冲击实验。研究了Kevlar纤维受冲击时的表观破坏形态和微观损伤机理。结果表明:纤维的变形破坏随冲击物的形状和速度变化呈现出多形态、多阶段模式;纤维的微观变形形态为:除拉伸破坏外,断口处产生大量的侧向劈裂,并且呈现明显的塑性流动。同时研究了试样面密度、冲击速度等因素对材料防弹性能的影响规律。构建了材料防弹性能的一般方程。 展开更多
关键词 kevlar纤维 弹道冲击 防弹
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Kevlar织物增强复合材料层合板冲击损伤特性研究 被引量:16
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作者 黄英 刘晓辉 李郁忠 《西北工业大学学报》 EI CAS CSCD 北大核心 2002年第3期486-491,共6页
采用空气炮实验装置、渗透剂增强的 X射线照相法和高强光背射法 ,对中心受到横向冲击的 Kevlar/环氧层合板的冲击损伤情况进行了研究 ,借助于有限元程序对层合板的应力状态进行分析、计算 ,讨论了冲击速度、铺层角、弹丸质量变化时材料... 采用空气炮实验装置、渗透剂增强的 X射线照相法和高强光背射法 ,对中心受到横向冲击的 Kevlar/环氧层合板的冲击损伤情况进行了研究 ,借助于有限元程序对层合板的应力状态进行分析、计算 ,讨论了冲击速度、铺层角、弹丸质量变化时材料的破坏机理与特征 。 展开更多
关键词 kevlar织物 复合材料层合板 冲击损伤 装甲防护 抗弹复合材料 应力分析
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SiO_2纳米粒子/Kevlar织物复合材料的防刺性能研究 被引量:16
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作者 王志刚 周兰英 朱杰 《产业用纺织品》 北大核心 2008年第10期15-18,21,共5页
经过对SiO2纳米粒子与Kevlar织物以及SiO2纳米粒子与锦纶、涤纶织物的复合材料防刺性能的研究发现,相对于同样面密度的纯织物,SiO2纳米粒子与Kevlar织物复合材料的防刺性能有了极大的改进。研究结果显示这种新颖的SiO2纳米粒子与Kevlar... 经过对SiO2纳米粒子与Kevlar织物以及SiO2纳米粒子与锦纶、涤纶织物的复合材料防刺性能的研究发现,相对于同样面密度的纯织物,SiO2纳米粒子与Kevlar织物复合材料的防刺性能有了极大的改进。研究结果显示这种新颖的SiO2纳米粒子与Kevlar织物复合材料能用来制造防刺服等防刺装备,而且比纯Kevlar织物的防刺材料更有效、更轻、更柔软、更经济。 展开更多
关键词 SIO2纳米粒子 kevlar 织物 复合材料 防刺服
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Kevlar纤维织物的性能研究 被引量:6
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作者 李桂娟 李茂银 +1 位作者 李娜娜 周恩乐 《化工新型材料》 CAS CSCD 北大核心 2011年第8期51-53,118,共4页
通过电子织物强力仪、万能试验机、圆盘式平磨仪、广角X-射线衍射(WAXD)、示差扫描量热(DSC)、红外光谱(IR)、热失重分析(TG)对对位芳纶纤维(Kevlar Twaron)织物进行表征,分析了热处理前后KevLar纤维织物的取向结晶行为和热性能。结果表... 通过电子织物强力仪、万能试验机、圆盘式平磨仪、广角X-射线衍射(WAXD)、示差扫描量热(DSC)、红外光谱(IR)、热失重分析(TG)对对位芳纶纤维(Kevlar Twaron)织物进行表征,分析了热处理前后KevLar纤维织物的取向结晶行为和热性能。结果表明,KevLar单纱的断裂强力为693.82 cN/tex,伸长率为49.5%;KevLar纤维织物的拉伸强度为53.7MPa,伸长率为50.2%,拉伸模量为2445.9MPa;耐磨性为1020转/min;KevLar纤维织物的取向结晶峰随着等温条件的不同而发生一定的蓝移;热分析表明,KevLar纤维织物的玻璃化转变温度Tg为295℃,在593℃时基本分解。 展开更多
关键词 对位芳纶 纤维织物 性能
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基于单胞模型的Kevlar织物高速冲击数值仿真方法研究 被引量:2
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作者 刘璐璐 陈伟 +2 位作者 时起珍 赵振华 关玉璞 《航空科学技术》 2015年第11期119-125,共7页
针对航空发动机软壁包容机匣用的Kevlar49机织织物,基于Ivanov提出的单胞模型,采用三元件粘弹性本构模型描述纱线应变率相关的力学特性,建立了Kevlar49织物高速冲击数值仿真模型;通过对单个单元拉伸进行数值仿真获得Kevlar织物的应力应... 针对航空发动机软壁包容机匣用的Kevlar49机织织物,基于Ivanov提出的单胞模型,采用三元件粘弹性本构模型描述纱线应变率相关的力学特性,建立了Kevlar49织物高速冲击数值仿真模型;通过对单个单元拉伸进行数值仿真获得Kevlar织物的应力应变响应;对钢球撞击四边固支的单层织物开展了数值仿真计算。结果表明:所建立的基于单胞结构的数值仿真方法既能描述织物的宏观力学特性,又可反映出撞击过程中纱线的相互运动;单元拉伸仿真获得的拉伸应力应变响应与试验结果一致;Kevlar织物在钢球下的冲击响应与法向变形与纱线细观有限元模型结果一致,验证了发展的基于单胞模型的数值仿真方法的有效性。 展开更多
关键词 机匣包容 kevlar织物 单胞模型 高速冲击 数值仿真
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浸轧压力对STF-Kevlar织物高速冲击性能影响研究
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作者 刘璐璐 柳旭 +2 位作者 赵振华 罗刚 陈伟 《振动与冲击》 EI CSCD 北大核心 2021年第8期1-9,共9页
为研究浸轧压力对剪切增稠液体(STF)增强Kevlar织物高速冲击性能的影响,分别采用50 kPa, 100kPa, 200kPa的压力浸轧STF-Kevlar织物,并使用钛合金模拟叶片弹体开展打靶试验。研究结果表明:STF表现出明显的剪切增稠现象,增稠范围为169~1 5... 为研究浸轧压力对剪切增稠液体(STF)增强Kevlar织物高速冲击性能的影响,分别采用50 kPa, 100kPa, 200kPa的压力浸轧STF-Kevlar织物,并使用钛合金模拟叶片弹体开展打靶试验。研究结果表明:STF表现出明显的剪切增稠现象,增稠范围为169~1 500 s^(-1),增稠比为56.4;Kevlar织物浸渍STF后,二氧化硅(SiO_(2))纳米粒子均匀附着在纤维表面;浸轧压力的增加使STF-Kevlar织物的质量增加率降低;STF-Kevlar织物的能量吸收较纯Kevlar织物高29.4%,但其弹道性能指数(BPI)低于纯Kevlar;浸轧后STF-Kevlar织物的能量吸收高于纯Kevlar织物,但低于未浸轧STF-Kevlar织物;在100 kPa的浸轧压力下,STF-Kevlar织物的单位面密度吸收的能量最高;STF-Kevlar织物能量吸收的变化趋势与织物极限变形高度的变化一致。 展开更多
关键词 剪切增稠液体(STF) kevlar织物 流变性能 高速冲击 能量吸收
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Co(60)γ射线辐照对Kevlar织物性能影响研究 被引量:3
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作者 李茂银 乔迁 +2 位作者 李桂娟 吴琼 周恩乐 《化工新型材料》 CAS CSCD 北大核心 2013年第12期131-133,共3页
对Kevlar织物进行Co60γ射线辐照,通过拉伸性能和DSC,TG,XRD测试,分析了Co60γ射线辐照前后样品结构及性能的变化。研究表明:经Co(60)γ射线辐照处理后,Kevlar织物在一定的辐照剂量范围内,拉伸强度提高了44.66%,弹性模量提高了21.35%;... 对Kevlar织物进行Co60γ射线辐照,通过拉伸性能和DSC,TG,XRD测试,分析了Co60γ射线辐照前后样品结构及性能的变化。研究表明:经Co(60)γ射线辐照处理后,Kevlar织物在一定的辐照剂量范围内,拉伸强度提高了44.66%,弹性模量提高了21.35%;伸长率下降了77.06%;当辐照剂量超过一定数值后,拉伸强度下降了19.29%,弹性模量下降了16.52%;伸长率提高了39.71%;热性能测试表明,辐照剂量对芳纶纤维的热性能影响较小,在600℃都基本分解;辐照对芳纶纤维的玻璃化转变温度(Tg)没有产生影响,样品的Tg均为265℃。红外测试表明,在辐照剂量范围内,芳纶纤维结构未发生变化;X-射线表明,辐照剂量大小影响Kevlar织物的取向结晶,但不改变其晶型。 展开更多
关键词 kevlar织物 Γ射线辐照 性能
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Kevlar纤维布/剪切增稠液复合材料制备及防刺性能 被引量:5
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作者 熊芳 周大利 +4 位作者 顾建文 华坚 杨为中 张琴 林朝阳 《四川兵工学报》 CAS 2013年第4期130-133,148,共5页
采用纳米SiO2和聚乙二醇(PEG200)制备不同SiO2质量浓度的剪切增稠液体(Shear Thickening Fluid,STF),并检测其流变性能;用落锤式冲击实验装置检测纯Kevlar纤维布和经STF浸渍的STF-Kevlar复合纤维布防刺性能。研究结果表明:不同SiO2质量... 采用纳米SiO2和聚乙二醇(PEG200)制备不同SiO2质量浓度的剪切增稠液体(Shear Thickening Fluid,STF),并检测其流变性能;用落锤式冲击实验装置检测纯Kevlar纤维布和经STF浸渍的STF-Kevlar复合纤维布防刺性能。研究结果表明:不同SiO2质量浓度的STF均有剪切增稠现象,随着SiO2质量浓度升高,起始粘度增大,增稠现象越显著,而临界剪切速率基本不变;同层数的STF-Kevlar复合纤维布的防刺性能明显优于纯Kevlar纤维布,防刺性能随SiO2质量浓度的增加而提高。 展开更多
关键词 纳米SIO2 剪切增稠 kevlar纤维布 防刺性能
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黏接压力对PTFE/Kevlar双层织物摩擦磨损性能的影响 被引量:1
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作者 刘宇飞 尹忠慰 +2 位作者 蒋丹 李虎林 霍亚军 《东华大学学报(自然科学版)》 CAS CSCD 北大核心 2015年第4期433-437,共5页
通过PTFE(聚四氟乙烯)/Kevlar双层织物与GCr15钢制金属盘的黏接试验,研究黏接面经过喷砂处理后,黏接压力对PTFE/Kevlar双层织物摩擦磨损性能的影响.结果表明:黏接压力为0.30 MPa时,PTFE/Kevlar双层织物的摩擦因数和磨损率最低,润滑性能... 通过PTFE(聚四氟乙烯)/Kevlar双层织物与GCr15钢制金属盘的黏接试验,研究黏接面经过喷砂处理后,黏接压力对PTFE/Kevlar双层织物摩擦磨损性能的影响.结果表明:黏接压力为0.30 MPa时,PTFE/Kevlar双层织物的摩擦因数和磨损率最低,润滑性能和耐磨性能最好;同时,与黏接压力为0.10及0.20 MPa时相比,黏接压力为0.30及0.40 MPa时,PTFE/Kevlar双层织物的摩擦因数与磨损率的一致性较好,故适当提高黏接压力有利于提高PTFE/Kevlar双层织物摩擦磨损性能的稳定性. 展开更多
关键词 黏接压力 PTFE/kevlar双层织物 摩擦因数 磨损率
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Kevlar织物软壁包容环抗冲击数值仿真分析研究 被引量:5
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作者 冯振宇 裴惠 +2 位作者 迟琪琳 解江 牟浩蕾 《振动与冲击》 EI CSCD 北大核心 2020年第10期15-23,共9页
针对机匣包容性问题,提出Kevlar平纹织物本构模型的拟合方法,分别采用单层壳、多层壳、层合壳三种有限元建模方式对Kevlar织物软壁包容环弹道冲击过程进行模拟,发展了机匣包容性仿真分析模型。结果表明,多层壳模型和层合壳模型的计算结... 针对机匣包容性问题,提出Kevlar平纹织物本构模型的拟合方法,分别采用单层壳、多层壳、层合壳三种有限元建模方式对Kevlar织物软壁包容环弹道冲击过程进行模拟,发展了机匣包容性仿真分析模型。结果表明,多层壳模型和层合壳模型的计算结果更准确,并且可以通过调节摩擦因子使仿真结果与试验结果更接近。在此基础上研究了撞击点位置和弹体入射姿态对弹体剩余速度的影响。结果表明:在较小偏移距离内,撞击点的位置对剩余速度的影响可以忽略不计;滚转角和俯仰角对剩余速度影响较小,而对于偏航角,当角度大于30°时,剩余速度会随着角度的增大明显呈下降趋势,且弹体出射姿态也会发生明显变化。 展开更多
关键词 kevlar织物 软壁包容 有限元分析 剩余速度
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Virtual ballistic impact testing of Kevlar soft armor:Predictive and validated finite element modeling of the V0-V100 probabilistic penetration response 被引量:4
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作者 Gaurav Nilakantan Suzanne Horner +1 位作者 Virginia Halls James Zheng 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2018年第3期213-225,共13页
This works presents the first fully validated and predictive capability to model the V_0-V_(100) probabilistic penetration response of a woven fabric using a yarn-level fabric finite element model. The V_0-V_(100) cur... This works presents the first fully validated and predictive capability to model the V_0-V_(100) probabilistic penetration response of a woven fabric using a yarn-level fabric finite element model. The V_0-V_(100) curve describes the probability of complete fabric penetration as a function of projectile impact velocity. The exemplar case considered in this paper comprises of a single-layer, fully-clamped, plain-weave Kevlar fabric impacted at the center by a 17-gr, 0.22 cal FSP or fragment-simulating projectile. Each warp and fill yarn in the fabric is individually modeled using 3 D finite elements and the virtual fabric microstructure is validated in detail against the experimental fabric microstructure. Material and testing sources of statistical variability including yarn strength and modulus, inter-yarn friction, precise projectile impact location, and projectile rotation are mapped into the finite element model. A series of impact simulations at varying projectile impact velocities is executed using LS-DYNA on the fabric models, with each model comprising unique mappings. The impact velocities together with the outcomes(penetration, nonpenetration) are used to generate the numerical V_0-V_(100) curve which is then validated against the experimental V_0-V_(100) curve. The numerical Vi-Vrdata(impact, residual velocities) is also validated against the experimental Vi-Vrdata. For completeness, this paper also reports the experimental characterization data and its statistical analysis used for model input, viz. the Kevlar yarn tensile strengths, moduli, and inter-yarn friction, and the experimental ballistic test data used for model validation. 展开更多
关键词 kevlar 有限元素 测试数据 验证 概率 预兆 弹道 虚拟
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Effects of ply orientation and material on the ballistic impact behavior of multilayer plain-weave aramid fabric targets 被引量:4
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作者 Gaurav Nilakantan Steven Nutt 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2018年第3期165-178,共14页
Virtual testing of fabric armor provides an efficient and inexpensive means of systematically studying the influence of various architectural and material parameters on the ballistic impact behavior of woven fabrics, ... Virtual testing of fabric armor provides an efficient and inexpensive means of systematically studying the influence of various architectural and material parameters on the ballistic impact behavior of woven fabrics, before actual laboratory prototypes are woven and destructively tested. In this finite element study, the combined effects of individual ply orientations and material properties on the impact performance of multi-layered, non-stitched woven aramid fabrics are studied using 2-and 4-sided clamping configurations. Individual ply orientations of 0°, ±15°, ±30°, and ±45° are considered along with three levels of inter-yarn friction coefficient. Functionally graded fabric targets are also considered wherein the yarn stiffness progressively increases or decreases through the target thickness while keeping the yarn strain energy density constant and with all other material and architectural parameters unchanged for consistency. For each target configuration, one non-penetrating and one penetrating impact velocity is chosen. The impact performance is evaluated by the time taken to arrest the projectile and the backface deformation for the non-penetrating impacts, and by the residual velocity for the penetrating impact tests. All deterministic impact simulations are performed using LS-DYNA. 2-sided clamped targets and lower inter-yarn frictional levels generally resulted in better impact performance.The functionally graded targets generally showed either similar or inferior impact performance than the baseline fabric target configurations for the non-penetrating shots. Some performance improvements were observed for the penetrating shots when the yarn stiffness was progressively decreased through the layers in a direction away from the strike face, with additional performance enhancements achieved by simultaneously reducing the inter-yarn friction. 展开更多
关键词 材料参数 线织物 芳香族 厚度 编织 取向 行为 弹道
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芳纶(Kevlar)纤维浸胶织物的研究及应用 被引量:2
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作者 任忠海 王琳琳 《黑龙江纺织》 2001年第4期11-12,共2页
介绍了芳纶 (Kevlar)纤维浸胶织物的性能、加工过程。
关键词 应用 芳纶纤维 浸胶织物 性能 加工工艺
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PTFE/Kevlar接结双层织物的织造研究 被引量:2
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作者 许家骅 赵敏 张继红 《产业用纺织品》 北大核心 2008年第10期9-11,共3页
介绍一种用于航天装备的外防护层产品的织物组织设计和织造工艺,该产品为分别用PTFE和Kevlar两种纱线构成织物正反面的接结双层织物。
关键词 聚四氟乙烯纤维 凯夫拉 组织结构设计 接结双层织物 织造工艺
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